Code of Federal Regulations, 2012 CFR
2012-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1735 Section 60.1735... Combustion Units Constructed on or Before August 30, 1999 Model Rule-Continuous Emission Monitoring § 60.1735... to also evaluate your oxygen (or carbon dioxide) continuous emission monitoring system. Therefore...
40 CFR Appendix A to Subpart A of... - State Regulation of Nonroad Internal Combustion Engines
Code of Federal Regulations, 2012 CFR
2012-07-01
... 40 Protection of Environment 21 2012-07-01 2012-07-01 false State Regulation of Nonroad Internal Combustion Engines A Appendix A to Subpart A of Part 89 Protection of Environment ENVIRONMENTAL PROTECTION... Nonroad Internal Combustion Engines This appendix sets forth the Environmental Protection Agency's (EPA's...
40 CFR Appendix A to Subpart A of... - State Regulation of Nonroad Internal Combustion Engines
Code of Federal Regulations, 2010 CFR
2010-07-01
... 40 Protection of Environment 20 2010-07-01 2010-07-01 false State Regulation of Nonroad Internal Combustion Engines A Appendix A to Subpart A of Part 89 Protection of Environment ENVIRONMENTAL PROTECTION... Nonroad Internal Combustion Engines This appendix sets forth the Environmental Protection Agency's (EPA's...
40 CFR Appendix A to Subpart A of... - State Regulation of Nonroad Internal Combustion Engines
Code of Federal Regulations, 2011 CFR
2011-07-01
... 40 Protection of Environment 20 2011-07-01 2011-07-01 false State Regulation of Nonroad Internal Combustion Engines A Appendix A to Subpart A of Part 89 Protection of Environment ENVIRONMENTAL PROTECTION... Nonroad Internal Combustion Engines This appendix sets forth the Environmental Protection Agency's (EPA's...
40 CFR Appendix A to Subpart A of... - State Regulation of Nonroad Internal Combustion Engines
Code of Federal Regulations, 2013 CFR
2013-07-01
... 40 Protection of Environment 21 2013-07-01 2013-07-01 false State Regulation of Nonroad Internal Combustion Engines A Appendix A to Subpart A of Part 89 Protection of Environment ENVIRONMENTAL PROTECTION... Nonroad Internal Combustion Engines This appendix sets forth the Environmental Protection Agency's (EPA's...
40 CFR Appendix A to Subpart A of... - State Regulation of Nonroad Internal Combustion Engines
Code of Federal Regulations, 2014 CFR
2014-07-01
... 40 Protection of Environment 20 2014-07-01 2013-07-01 true State Regulation of Nonroad Internal Combustion Engines A Appendix A to Subpart A of Part 89 Protection of Environment ENVIRONMENTAL PROTECTION... Nonroad Internal Combustion Engines This appendix sets forth the Environmental Protection Agency's (EPA's...
49 CFR Appendix H to Part 173 - Method of Testing for Sustained Combustibility
Code of Federal Regulations, 2010 CFR
2010-10-01
... 49 Transportation 2 2010-10-01 2010-10-01 false Method of Testing for Sustained Combustibility H Appendix H to Part 173 Transportation Other Regulations Relating to Transportation PIPELINE AND HAZARDOUS...-GENERAL REQUIREMENTS FOR SHIPMENTS AND PACKAGINGS Pt. 173, App. H Appendix H to Part 173—Method of Testing...
Code of Federal Regulations, 2013 CFR
2013-07-01
... Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) SOLID WASTES (CONTINUED) LAND DISPOSAL RESTRICTIONS Pt. 268, App. XI Appendix XI to Part 268—Metal Bearing Wastes Prohibited From Dilution in a Combustion... 40 Protection of Environment 28 2013-07-01 2013-07-01 false Metal Bearing Wastes Prohibited From...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) SOLID WASTES (CONTINUED) LAND DISPOSAL RESTRICTIONS Pt. 268, App. XI Appendix XI to Part 268—Metal Bearing Wastes Prohibited From Dilution in a Combustion... 40 Protection of Environment 27 2014-07-01 2014-07-01 false Metal Bearing Wastes Prohibited From...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Menzies, K.T.; Randel, M.A.; Quill, A.L.
1989-01-01
The U.S. Army Biomedical Research and Development Laboratory defined an extensive research program to address the generation of potentially toxic propellant combustion products in crew compartments of armored vehicles during weapons firing. The major objectives of the research were (1) to determine the presence and concentration of propellant combustion products, (2) to determine potential crew exposure to these combustion products, and (3) to assess the efficacy of field monitoring in armored vehicles. To achieve these goals, air monitoring was conducted in selected armored vehicle types, i.e., M109, M60, M3, M1, at several Army installations.
Utilizing Near-IR Tunable Laser Absorption Spectroscopy to Study Detonation and Combustion Systems
2014-03-27
debris, such as soot . Velocity curves for the other equivalence ratios studied in this experiment are shown in Appendix A. Some of these curves show a...James R. Gord. “Measurements of OH mole fraction and temperature up to 20 kHz by using a diode-laser based UV absorption sensor ”. Applied Optics, 44...Davidson, and R.K. Hanson. “CO concentration and temperature sensor for combustion gases using quantum-cascade laser absorption near 4.7µm”. Applied
General Aviation Avionics Statistics: 1977.
1980-06-01
combustion of fuel, the gases of combustion (or the heated air) being used both to rotate the turbine and to create a thrust-producing engine. Turboprop...cc 0 4) 0 ) cu z 4) 0 a$. .- MCI 1001 APPENDIX D AIRSPACE STRUCTURE 101 APPENDIX D. AIRSPACE STRUCTURE -t FLIO* - -FL450 I ContinentalI Control...Compass 9. Landing gear 4. Tachometer 10. Belts 5. Oil temperature 11. Special equipment for 6. Emergency locator over water flights transmitter
General Conformity Training Modules: Appendix A Sample Emissions Calculations
Appendix A of the training modules gives example calculations for external and internal combustion sources, construction, fuel storage and transfer, on-road vehicles, aircraft operations, storage piles, and paved roads.
40 CFR Appendix F to Part 75 - Conversion Procedures
Code of Federal Regulations, 2010 CFR
2010-07-01
...-00, Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter, or ASTM D4809-00, Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb...
Code of Federal Regulations, 2010 CFR
2010-07-01
... ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) AIR PROGRAMS (CONTINUED) STANDARDS OF PERFORMANCE FOR NEW STATIONARY SOURCES Standards of Performance for Small Municipal Waste Combustion Units for Which Construction is... Performance Specification 1 in appendix B of this part. Complete the evaluation within 60 days after your...
40 CFR 75.53 - Monitoring plan.
Code of Federal Regulations, 2012 CFR
2012-07-01
... are pre-combustion, post-combustion, or integral to the combustion process; control equipment code... fuel flow-to-load test in section 2.1.7 of appendix D to this part is used: (A) The upper and lower... and applied to the hourly flow rate data: (A) Stack or duct width at the test location, ft; (B) Stack...
40 CFR Appendix G to Part 75 - Determination of CO2 Emissions
Code of Federal Regulations, 2014 CFR
2014-07-01
... following procedures to estimate daily CO2 mass emissions from the combustion of fossil fuels. The optional... tons/day) from the combustion of fossil fuels. Where fuel flow is measured in a common pipe header (i.e... discharged to the atmosphere (in tons/day) as the sum of CO2 emissions from combustion and, if applicable...
40 CFR Appendix G to Part 75 - Determination of CO2 Emissions
Code of Federal Regulations, 2011 CFR
2011-07-01
... following procedures to estimate daily CO2 mass emissions from the combustion of fossil fuels. The optional... tons/day) from the combustion of fossil fuels. Where fuel flow is measured in a common pipe header (i.e... discharged to the atmosphere (in tons/day) as the sum of CO2 emissions from combustion and, if applicable...
40 CFR Appendix G to Part 75 - Determination of CO2 Emissions
Code of Federal Regulations, 2013 CFR
2013-07-01
... following procedures to estimate daily CO2 mass emissions from the combustion of fossil fuels. The optional... tons/day) from the combustion of fossil fuels. Where fuel flow is measured in a common pipe header (i.e... discharged to the atmosphere (in tons/day) as the sum of CO2 emissions from combustion and, if applicable...
40 CFR Appendix G to Part 75 - Determination of CO2 Emissions
Code of Federal Regulations, 2012 CFR
2012-07-01
... following procedures to estimate daily CO2 mass emissions from the combustion of fossil fuels. The optional... tons/day) from the combustion of fossil fuels. Where fuel flow is measured in a common pipe header (i.e... discharged to the atmosphere (in tons/day) as the sum of CO2 emissions from combustion and, if applicable...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Menzies, K.T.; Randel, M.A.; Quill, A.L.
1989-01-01
The U.S. Army Biomedical Research and Development Laboratory defined an extensive research program to address the generation of potentially toxic propellant combustion products in crew compartments of armored vehicles during weapons firing. The major objectives of the research were (1) to determine the presence and concentration of propellant combustion products, (2) to determine potential crew exposure to these combustion products, and (3) to assess the efficacy of field monitoring in armored vehicles. To achieve these goals, air monitoring was conducted in selected armored vehicle types, i.e., M109, M60, M3, M1, at several Army installations. Auxiliary information concerning the specific munitionsmore » fired and the Training and Doctrine Command (TRADOC) or Forces Command (FORSCOM) firing scenarios was collected so that a comparison of pollutant concentrations generated by specific weapons both within vehicle types and between vehicle types could be made.« less
Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors
NASA Technical Reports Server (NTRS)
Priem, R. J.; Jefferson, Y. S. Y.
1973-01-01
A technique for predicting the stability characteristics of a gaseous-propellant rocket combustion system is developed based on a model that assumes coupling between the flow through the injector and the oscillating chamber pressure. The theoretical model uses a lumped parameter approach for the flow elements in the injection system plus wave dynamics in the combustion chamber. The injector flow oscillations are coupled to the chamber pressure oscillations with a delay time. Frequency and decay (or growth) rates are calculated for various combustor design and operating parameters to demonstrate the influence of various parameters on stability. Changes in oxidizer design parameters had a much larger influence on stability than a similar change in fuel parameters. A complete description of the computer program used to make these calculations is given in an appendix.
40 CFR Table 3 to Subpart Lllll of... - Requirements for Performance Tests a,b
Code of Federal Regulations, 2011 CFR
2011-07-01
..., THC destruction efficiency, THC outlet concentration, or combustion efficiency standards, the sampling... combustion efficiency or THC standards a. Measure the concentration of carbon dioxideb. Measure the... method 25A in appendix A to part 60 of this chapter 10. Each control device used to comply with the THC...
40 CFR Table 3 to Subpart Lllll of... - Requirements for Performance Tests a,b
Code of Federal Regulations, 2012 CFR
2012-07-01
..., THC destruction efficiency, THC outlet concentration, or combustion efficiency standards, the sampling... combustion efficiency or THC standards a. Measure the concentration of carbon dioxideb. Measure the... method 25A in appendix A to part 60 of this chapter 10. Each control device used to comply with the THC...
40 CFR Table 3 to Subpart Lllll of... - Requirements for Performance Tests a,b
Code of Federal Regulations, 2010 CFR
2010-07-01
..., THC destruction efficiency, THC outlet concentration, or combustion efficiency standards, the sampling... combustion efficiency or THC standards a. Measure the concentration of carbon dioxideb. Measure the... method 25A in appendix A to part 60 of this chapter 10. Each control device used to comply with the THC...
40 CFR Table 3 to Subpart Lllll of... - Requirements for Performance Tests a b
Code of Federal Regulations, 2014 CFR
2014-07-01
..., THC destruction efficiency, THC outlet concentration, or combustion efficiency standards, the sampling... combustion efficiency or THC standards a. Measure the concentration of carbon dioxideb. Measure the... method 25A in appendix A to part 60 of this chapter 10. Each control device used to comply with the THC...
40 CFR Table 3 to Subpart Lllll of... - Requirements for Performance Tests a,b
Code of Federal Regulations, 2013 CFR
2013-07-01
..., THC destruction efficiency, THC outlet concentration, or combustion efficiency standards, the sampling... combustion efficiency or THC standards a. Measure the concentration of carbon dioxideb. Measure the... method 25A in appendix A to part 60 of this chapter 10. Each control device used to comply with the THC...
Characterization of Horizontally-Issuing Reacting Buoyant Jets
2011-03-01
125 Appendix B : Unfiltered High Speed Imaging Results ....................................................139 Appendix C: CH* Filtered High...and ( b ) Negative Buoyancy (16) ... 15 Figure 4. (a) Flame and ( b ) Nonflame Combustion in a Spark-Ignition Engine (26) ...... 27 Figure 5. Laminar...a) Fluorescent absorption and emission b ) Emission spectra (30) .................... 41 Figure 9. The X and A Energy States (29
Fire Fighter Trainer Environmental Considerations. Phase II. Appendixes.
1981-07-31
presented in Table A-i. These quidelines ref lect the original materials to be used in the 19F1, as well as the various decomposition and combustion products...15 minutes in any 8-hour period. 1New fuel combustion sources with actual heat input > 250 million Btu/hr. 2 Al other sources. A- 8 Pollutants other...generating chemicals, combustion byproducts, and materials used in t.he construction of the trainer itself. Incompatibility of these materials could
NASA Technical Reports Server (NTRS)
Piccolo, R.
1979-01-01
The methodology used for vehicle layout and component definition is described as well as techniques for system optimization and energy evaluation. The preliminary design is examined with particular attention given to body and structure; propulsion system; crash analysis and handling; internal combustion engine; DC motor separately excited; Ni-Zn battery; transmission; control system; vehicle auxiliarries; weight breakdown, and life cycle costs. Formulas are given for the quantification of energy consumption and results are compared with the reference vehicle.
Combustion Science to Reduce PM Emissions for Military Platforms
2012-01-01
355 7.0 References 356 Appendix: List of Archival Publications and Conference Papers 376 vi List...carbonaddition HITRAN Database of infra-red spectra HP High Pressure HW Harris and Weiner ICCD Intensified charge coupled device ID internal diameter IR ...archival publication based on this work received a distinguished outstanding paper award at the 32nd International Combustion Symposium
Thermodynamic data for biomass conversion and waste incineration
DOE Office of Scientific and Technical Information (OSTI.GOV)
Domalski, E.S.; Jobe, T.L. Jr; Milne, T.A.
1986-09-01
The general purpose of this collection of thermodynamic data of selected materials is to make property information available to the engineering community on chemical mixtures, polymers, composite materials, solid wastes, biomass, and materials not easily identifiable by a single stoichiometric formula. More than 700 materials have been compiled covering properties such as specific heat, gross heat of combustion, heat of fusion, heat of vaporization, and vapor pressure. The information was obtained from the master files of the NBS Chemical Thermodynamics Data Center, the annual issues of the Bulletin of Chemical Thermodynamics, intermittent examinations of the Chemical Abstracts subject indexes, individualmore » articles by various authors, and other general reference sources. The compilation is organized into several broad categories; materials are listed alphabetically within each category. For each material, the physical state, information as to the composition or character of the material, the kind of thermodynamic property reported, the specific property values for the material, and citations to the reference list are given. In addition, appendix A gives an empirical formula that allows heats of combustion of carbonaceous materials to be predicted with surprising accuracy when the elemental composition is known. A spread sheet illustrates this predictability with examples from this report and elsewhere. Appendix B lists some reports containing heats of combustion not included in this publication. Appendix C contains symbols, units, conversion factors, and atomic weights used in evaluating and compiling the thermodynamic data.« less
Stability Analysis of a Liquid Fuel Annular Combustion Chamber
1979-11-01
FOREWORD This report summarizes a portion of the work done for NASA Grant NCR 4I3-0oU3-oj5. It Is thus masters research of the first author, Gary H... Flandro , G. A., "Resonant Combustion in Rockets," Scientific American, December 1960, pp. 95-103. 11 -0 Io U\\ U t APPENDICES 11 117 APPENDIX A ’,4
Code of Federal Regulations, 2011 CFR
2011-01-01
... 10 Energy 3 2011-01-01 2011-01-01 false Uniform Test Method for Measuring the Energy Consumption..., App. O Appendix O to Subpart B of Part 430—Uniform Test Method for Measuring the Energy Consumption of... condition. 1.9“Flue gases” means reaction products resulting from the combustion of a fuel with the oxygen...
Code of Federal Regulations, 2013 CFR
2013-01-01
... 10 Energy 3 2013-01-01 2013-01-01 false Uniform Test Method for Measuring the Energy Consumption..., App. O Appendix O to Subpart B of Part 430—Uniform Test Method for Measuring the Energy Consumption of... products resulting from the combustion of a fuel with the oxygen of the air, including the inerts and any...
Code of Federal Regulations, 2012 CFR
2012-01-01
... 10 Energy 3 2012-01-01 2012-01-01 false Uniform Test Method for Measuring the Energy Consumption..., App. O Appendix O to Subpart B of Part 430—Uniform Test Method for Measuring the Energy Consumption of... condition. 1.9“Flue gases” means reaction products resulting from the combustion of a fuel with the oxygen...
Code of Federal Regulations, 2010 CFR
2010-01-01
... 10 Energy 3 2010-01-01 2010-01-01 false Uniform Test Method for Measuring the Energy Consumption..., App. O Appendix O to Subpart B of Part 430—Uniform Test Method for Measuring the Energy Consumption of... condition. 1.9“Flue gases” means reaction products resulting from the combustion of a fuel with the oxygen...
Geotechnical Properties of Oil Shale Retorted by the PARAHO and TOSCO Processes.
1979-11-01
literature search was restricted to the Green River formation of oil shale in the tri-state area of Colorado (Piceance Basin ), Utah ( Uinta Basin ), and...it is preheated by combustion gases as it travels downward by gravity. Air and recycling gas are injected at midheight and are burned, bringing the oil ...REFERENCES..................................38 TABLES 1-5 APPENDIX A: OIL SHALE RETORTING PROCESSES................Al Tosco Process Gas Combustion
1989-01-01
25 wt % Solid Sorbent Collection solution in water 1. Glass tubing (6.0 mm OD, (Aldrich G400-y or equivalent) 4.0 mm ID) 2. 2,4- Dinitrophenylhydrazine ... dinitrophenylhydrazine in boiling 4M HCI. When the DNPH has dissolved completely, cool the Folution in an ice bath. Collect the yellow crystalline precipitate... dinitrophenylhydrazine . Add the aldehyde in excess to assure that no underivatized DNPH remains. Extract the derivative with dichloromethane. Remove the
40 CFR Appendix Viii to Part 266 - Organic Compounds for Which Residues Must Be Analyzed
Code of Federal Regulations, 2011 CFR
2011-07-01
... residues collected from areas downstream of the combustion chamber (e.g., ductwork, boiler tubes, heat exchange surfaces, air pollution control devices, etc.). Note to the table: Analysis is not required for...
40 CFR Appendix Viii to Part 266 - Organic Compounds for Which Residues Must Be Analyzed
Code of Federal Regulations, 2010 CFR
2010-07-01
... residues collected from areas downstream of the combustion chamber (e.g., ductwork, boiler tubes, heat exchange surfaces, air pollution control devices, etc.). Note to the table: Analysis is not required for...
40 CFR Appendix Viii to Part 266 - Organic Compounds for Which Residues Must Be Analyzed
Code of Federal Regulations, 2012 CFR
2012-07-01
... residues collected from areas downstream of the combustion chamber (e.g., ductwork, boiler tubes, heat exchange surfaces, air pollution control devices, etc.). Note to the table: Analysis is not required for...
40 CFR Appendix Viii to Part 266 - Organic Compounds for Which Residues Must Be Analyzed
Code of Federal Regulations, 2013 CFR
2013-07-01
... residues collected from areas downstream of the combustion chamber (e.g., ductwork, boiler tubes, heat exchange surfaces, air pollution control devices, etc.). Note to the table: Analysis is not required for...
40 CFR Appendix Viii to Part 266 - Organic Compounds for Which Residues Must Be Analyzed
Code of Federal Regulations, 2014 CFR
2014-07-01
... residues collected from areas downstream of the combustion chamber (e.g., ductwork, boiler tubes, heat exchange surfaces, air pollution control devices, etc.). Note to the table: Analysis is not required for...
Summary of Part 75 Administrative Processes: Table 6
Learn how to submit information for a new unit, new stack or new FGD; unit shutdown and restart, long term cold storage (LTCS), expected restart date, postponement of Appendix E testing, backup fuel used, and notice of combustion of emergency fuel.
Code of Federal Regulations, 2011 CFR
2011-01-01
.... Emergency lighting. Emergency lighting units with at least an 8-hour battery power supply shall be provided..., combustible and flammable gases and liquids, high efficiency particulate air and charcoal filters, dry ion...
Code of Federal Regulations, 2014 CFR
2014-01-01
.... Emergency lighting. Emergency lighting units with at least an 8-hour battery power supply shall be provided..., combustible and flammable gases and liquids, high efficiency particulate air and charcoal filters, dry ion...
Code of Federal Regulations, 2012 CFR
2012-01-01
.... Emergency lighting. Emergency lighting units with at least an 8-hour battery power supply shall be provided..., combustible and flammable gases and liquids, high efficiency particulate air and charcoal filters, dry ion...
Code of Federal Regulations, 2013 CFR
2013-01-01
.... Emergency lighting. Emergency lighting units with at least an 8-hour battery power supply shall be provided..., combustible and flammable gases and liquids, high efficiency particulate air and charcoal filters, dry ion...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Roberts, A. G.; Barker, S. N.; Phillips, R. N.
1981-09-01
Volume IV of the report on the 1000 hour programme consists of three appendices giving details of the enginmering/construction aspects of the plant and reports from Stal-Laval Turbin A.B. Appendix N has been entered individually. (LTN)
Code of Federal Regulations, 2012 CFR
2012-07-01
... phosphating in aluminum car washing when such phosphating is an exclusive conversion coating process. K002... primary production of steel in electric furnaces. K069 Emission control dust/sludge from secondary lead...
Code of Federal Regulations, 2011 CFR
2011-07-01
... phosphating in aluminum car washing when such phosphating is an exclusive conversion coating process. K002... primary production of steel in electric furnaces. K069 Emission control dust/sludge from secondary lead...
Code of Federal Regulations, 2010 CFR
2010-07-01
... phosphating in aluminum car washing when such phosphating is an exclusive conversion coating process. K002... primary production of steel in electric furnaces. K069 Emission control dust/sludge from secondary lead...
NASA Technical Reports Server (NTRS)
Fragola, Joseph R.; Maggio, Gaspare; Frank, Michael V.; Gerez, Luis; Mcfadden, Richard H.; Collins, Erin P.; Ballesio, Jorge; Appignani, Peter L.; Karns, James J.
1995-01-01
Volume 5 is Appendix C, Auxiliary Shuttle Risk Analyses, and contains the following reports: Probabilistic Risk Assessment of Space Shuttle Phase 1 - Space Shuttle Catastrophic Failure Frequency Final Report; Risk Analysis Applied to the Space Shuttle Main Engine - Demonstration Project for the Main Combustion Chamber Risk Assessment; An Investigation of the Risk Implications of Space Shuttle Solid Rocket Booster Chamber Pressure Excursions; Safety of the Thermal Protection System of the Space Shuttle Orbiter - Quantitative Analysis and Organizational Factors; Space Shuttle Main Propulsion Pressurization System Probabilistic Risk Assessment, Final Report; and Space Shuttle Probabilistic Risk Assessment Proof-of-Concept Study - Auxiliary Power Unit and Hydraulic Power Unit Analysis Report.
40 CFR Appendix A-4 to Part 60 - Test Methods 6 through 10B
Code of Federal Regulations, 2010 CFR
2010-07-01
... sources Method 6A—Determination of sulfur dioxide, moisture, and carbon dioxide emissions from fossil fuel... fossil fuel combustion sources Method 6C—Determination of Sulfur Dioxide Emissions From Stationary... with SO2 to form particulate sulfite and by reacting with the indicator. If free ammonia is present...
40 CFR Appendix A-4 to Part 60 - Test Methods 6 through 10B
Code of Federal Regulations, 2011 CFR
2011-07-01
... sources Method 6A—Determination of sulfur dioxide, moisture, and carbon dioxide emissions from fossil fuel... fossil fuel combustion sources Method 6C—Determination of Sulfur Dioxide Emissions From Stationary... with SO2 to form particulate sulfite and by reacting with the indicator. If free ammonia is present...
40 CFR Appendix A-4 to Part 60 - Test Methods 6 through 10B
Code of Federal Regulations, 2013 CFR
2013-07-01
... sources Method 6A—Determination of sulfur dioxide, moisture, and carbon dioxide emissions from fossil fuel... fossil fuel combustion sources Method 6C—Determination of Sulfur Dioxide Emissions From Stationary... with SO2 to form particulate sulfite and by reacting with the indicator. If free ammonia is present...
40 CFR Appendix A-4 to Part 60 - Test Methods 6 through 10B
Code of Federal Regulations, 2014 CFR
2014-07-01
... sources Method 6A—Determination of sulfur dioxide, moisture, and carbon dioxide emissions from fossil fuel... fossil fuel combustion sources Method 6C—Determination of Sulfur Dioxide Emissions From Stationary... reacting with SO2 to form particulate sulfite and by reacting with the indicator. If free ammonia is...
40 CFR Appendix A-4 to Part 60 - Test Methods 6 through 10B
Code of Federal Regulations, 2012 CFR
2012-07-01
... sources Method 6A—Determination of sulfur dioxide, moisture, and carbon dioxide emissions from fossil fuel... fossil fuel combustion sources Method 6C—Determination of Sulfur Dioxide Emissions From Stationary... with SO2 to form particulate sulfite and by reacting with the indicator. If free ammonia is present...
40 CFR 62.15330 - What must I include in the initial report?
Code of Federal Regulations, 2014 CFR
2014-07-01
... emissions. (3) The 4-hour block or 24-hour daily arithmetic average concentration of carbon monoxide... specifications in appendix B of 40 CFR part 60 in conducting the evaluation. (e) The maximum demonstrated load of... combustion unit uses activated carbon to control dioxins/furans or mercury emissions, the average carbon feed...
DOE Office of Scientific and Technical Information (OSTI.GOV)
None
This appendix on Mass Burn Technologies is the first in a series designed to identify, describe and assess the suitability of several currently or potentially available generic technologies for the management of municipal solid waste (MSW). These appendices, which cover eight core thermoconversion, bioconversion and recycling technologies, reflect public domain information gathered from many sources. Representative sources include: professional journal articles, conference proceedings, selected municipality solid waste management plans and subscription technology data bases. The information presented is intended to serve as background information that will facilitate the preparation of the technoeconomic and life cycle mass, energy and environmental analysesmore » that are being developed for each of the technologies. Mass burn has been and continues to be the predominant technology in Europe for the management of MSW. In the United States, the majority of the existing waste-to-energy projects utilize this technology and nearly 90 percent of all currently planned facilities have selected mass burn systems. Mass burning generally refers to the direct feeding and combustion of municipal solid waste in a furnace without any significant waste preprocessing. The only materials typically removed from the waste stream prior to combustion are large bulky objects and potentially hazardous or undesirable wastes. The technology has evolved over the last 100 or so years from simple incineration to the most highly developed and commercially proven process available for both reducing the volume of MSW and for recovering energy in the forms of steam and electricity. In general, mass burn plants are considered to operate reliably with high availability.« less
DOE Office of Scientific and Technical Information (OSTI.GOV)
None
1992-10-01
This appendix contains the numerically indexed bibliography for the complete group of reports on municipal solid waste management alternatives. The list references information on the following topics: mass burn technologies, RDF technologies, fluidized bed combustion, pyrolysis and gasification of MSW, materials recovery- recycling technologies, sanitary landfills, composting and anaerobic digestion of MSW.
DOE Office of Scientific and Technical Information (OSTI.GOV)
None
1992-10-01
This appendix contains the alphabetically indexed bibliography for the complete group of reports on municipal waste management alternatives. The references are listed for each of the following topics: mass burn technologies, RDF technologies, fluidized-bed combustion, pyrolysis and gasification of MSW, materials recovery- recycling technologies, sanitary landfills, composting, and anaerobic digestion of MSW.
Ultrafine Condensation Particle Counter Instrument Handbook
DOE Office of Scientific and Technical Information (OSTI.GOV)
Kuang, C.
2016-02-01
The Model 3776 Ultrafine Condensation Particle Counter (UCPC; pictured in Appendix A) is designed for researchers interested in airborne particles smaller than 20 nm. With sensitivity to particles down to 2.5 nm in diameter, this UCPC is ideally suited for atmospheric and climate research, particle formation and growth studies, combustion and engine exhaust research, and nanotechnology research.
Code of Federal Regulations, 2013 CFR
2013-07-01
... communicated effectively using handwritten notes. One major advocacy organization, for example, noted that the... example, blood work for routine lab tests or regular allergy shots. Video Interpreting Services... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there...
Code of Federal Regulations, 2011 CFR
2011-07-01
... communicated effectively using handwritten notes. One major advocacy organization, for example, noted that the... example, blood work for routine lab tests or regular allergy shots. Video Interpreting Services... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there...
Code of Federal Regulations, 2012 CFR
2012-07-01
... communicated effectively using handwritten notes. One major advocacy organization, for example, noted that the... example, blood work for routine lab tests or regular allergy shots. Video Interpreting Services... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there...
Code of Federal Regulations, 2014 CFR
2014-07-01
... communicated effectively using handwritten notes. One major advocacy organization, for example, noted that the... example, blood work for routine lab tests or regular allergy shots. Video Interpreting Services... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there...
29 CFR Appendix A to Subpart S of... - References for Further Information
Code of Federal Regulations, 2014 CFR
2014-07-01
... Safety, Health, and Environmental Training. ANSI/IEEE C2-2002 National Electrical Safety Code. ANSI K61.1.... NFPA 59-2004 Utility LP-Gas Plant Code. NFPA 70-2002 National Electrical Code. (See also NFPA 70-2005.... NMAB 353-3-1980 Classification of Combustible Dust in Accordance with the National Electrical Code. [72...
29 CFR Appendix A to Subpart S of... - References for Further Information
Code of Federal Regulations, 2011 CFR
2011-07-01
... Safety, Health, and Environmental Training. ANSI/IEEE C2-2002 National Electrical Safety Code. ANSI K61.1.... NFPA 59-2004 Utility LP-Gas Plant Code. NFPA 70-2002 National Electrical Code. (See also NFPA 70-2005.... NMAB 353-3-1980 Classification of Combustible Dust in Accordance with the National Electrical Code. [72...
29 CFR Appendix A to Subpart S of... - References for Further Information
Code of Federal Regulations, 2012 CFR
2012-07-01
... Safety, Health, and Environmental Training. ANSI/IEEE C2-2002 National Electrical Safety Code. ANSI K61.1.... NFPA 59-2004 Utility LP-Gas Plant Code. NFPA 70-2002 National Electrical Code. (See also NFPA 70-2005.... NMAB 353-3-1980 Classification of Combustible Dust in Accordance with the National Electrical Code. [72...
29 CFR Appendix A to Subpart S of... - References for Further Information
Code of Federal Regulations, 2013 CFR
2013-07-01
... Safety, Health, and Environmental Training. ANSI/IEEE C2-2002 National Electrical Safety Code. ANSI K61.1.... NFPA 59-2004 Utility LP-Gas Plant Code. NFPA 70-2002 National Electrical Code. (See also NFPA 70-2005.... NMAB 353-3-1980 Classification of Combustible Dust in Accordance with the National Electrical Code. [72...
NASA Technical Reports Server (NTRS)
Borg, Stephen E.; Harper, Samuel E.
2001-01-01
This paper documents the design and development of the fiber-optic probes utilized in the flame detection systems used in NASA Langley Research Center's 8-Foot High Temperature Tunnel (8-ft HTT). Two independent flame detection systems are utilized to monitor the presence and stability of the main-burner and pilot-level flames during facility operation. Due to the harsh environment within the combustor, the successful development of a rugged and efficient fiber-optic probe was a critical milestone in the development of these flame detection systems. The final optical probe design for the two flame detection systems resulted from research that was conducted in Langley's 7-in High Temperature Pilot Tunnel (7-in HTT). A detailed description of the manufacturing process behind the optical probes used in the 8-ft HTT is provided in Appendix A of this report.
Code of Federal Regulations, 2014 CFR
2014-07-01
... Petitions Petitioning state Named source categories Connecticut Fossil fuel-fired boilers or other indirect.... New Hampshire Fossil fuel-fired indirect heat exchange combustion units and fossil fuel-fired electric generating facilities which emit ten tons of NOX or more per day. New York Fossil fuel-fired boilers or...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Petitions Petitioning state Named source categories Connecticut Fossil fuel-fired boilers or other indirect.... New Hampshire Fossil fuel-fired indirect heat exchange combustion units and fossil fuel-fired electric generating facilities which emit ten tons of NOX or more per day. New York Fossil fuel-fired boilers or...
Code of Federal Regulations, 2011 CFR
2011-07-01
... Petitions Petitioning state Named source categories Connecticut Fossil fuel-fired boilers or other indirect.... New Hampshire Fossil fuel-fired indirect heat exchange combustion units and fossil fuel-fired electric generating facilities which emit ten tons of NOX or more per day. New York Fossil fuel-fired boilers or...
Code of Federal Regulations, 2010 CFR
2010-07-01
... Petitions Petitioning state Named source categories Connecticut Fossil fuel-fired boilers or other indirect.... New Hampshire Fossil fuel-fired indirect heat exchange combustion units and fossil fuel-fired electric generating facilities which emit ten tons of NOX or more per day. New York Fossil fuel-fired boilers or...
Code of Federal Regulations, 2013 CFR
2013-07-01
... Petitions Petitioning state Named source categories Connecticut Fossil fuel-fired boilers or other indirect.... New Hampshire Fossil fuel-fired indirect heat exchange combustion units and fossil fuel-fired electric generating facilities which emit ten tons of NOX or more per day. New York Fossil fuel-fired boilers or...
Improved Kinetic Models for High-Speed Combustion Simulation
2008-06-01
142 Appendix F1: USC_Skeletal_Ethylene_chem.inp ....................................................................... 143 ...to form a strong carbonyl double bond ( keto -Q) gaining 80 kcal mol-1, which is sufficient to immediately cleave the weak RO—OH bond (45 kcal mol-1...in the hydroperoxide. Relative to the stabilized adduct this reaction to ( keto -Q+OH), product set is 65.9 kcal mol-1 below the entrance channel
Code of Federal Regulations, 2011 CFR
2011-07-01
... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there... for the definition of “wheelchair” in section 508(c)(2) of the ADA. One commenter indicated a...-operated wheelchairs of 6 miles per hour. In a study of trail and other non-motorized transportation users...
Code of Federal Regulations, 2013 CFR
2013-07-01
... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there... for the definition of “wheelchair” in section 508(c)(2) of the ADA. One commenter indicated a...-operated wheelchairs of 6 miles per hour. In a study of trail and other non-motorized transportation users...
Code of Federal Regulations, 2014 CFR
2014-07-01
... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there... for the definition of “wheelchair” in section 508(c)(2) of the ADA. One commenter indicated a...-operated wheelchairs of 6 miles per hour. In a study of trail and other non-motorized transportation users...
Code of Federal Regulations, 2012 CFR
2012-07-01
... or combustion engines. One commenter suggested using exhaust level as the determinant. Although there... for the definition of “wheelchair” in section 508(c)(2) of the ADA. One commenter indicated a...-operated wheelchairs of 6 miles per hour. In a study of trail and other non-motorized transportation users...
49 CFR Appendix H to Part 173 - Method of Testing for Sustained Combustibility
Code of Federal Regulations, 2013 CFR
2013-10-01
... the well when in the test position. (c) Light the butane test fuel with the jet away from the test... used. The block has a concave well and a pocket drilled to take a thermometer. A small gas jet assembly on a swivel is attached to the block. The handle and gas inlet for the gas jet may be fitted at any...
49 CFR Appendix H to Part 173 - Method of Testing for Sustained Combustibility
Code of Federal Regulations, 2012 CFR
2012-10-01
... the well when in the test position. (c) Light the butane test fuel with the jet away from the test... used. The block has a concave well and a pocket drilled to take a thermometer. A small gas jet assembly on a swivel is attached to the block. The handle and gas inlet for the gas jet may be fitted at any...
49 CFR Appendix H to Part 173 - Method of Testing for Sustained Combustibility
Code of Federal Regulations, 2014 CFR
2014-10-01
... the well when in the test position. (c) Light the butane test fuel with the jet away from the test... used. The block has a concave well and a pocket drilled to take a thermometer. A small gas jet assembly on a swivel is attached to the block. The handle and gas inlet for the gas jet may be fitted at any...
49 CFR Appendix H to Part 173 - Method of Testing for Sustained Combustibility
Code of Federal Regulations, 2011 CFR
2011-10-01
... the well when in the test position. (c) Light the butane test fuel with the jet away from the test... used. The block has a concave well and a pocket drilled to take a thermometer. A small gas jet assembly on a swivel is attached to the block. The handle and gas inlet for the gas jet may be fitted at any...
Tidd hot gas clean up program. Final report
DOE Office of Scientific and Technical Information (OSTI.GOV)
NONE
This Final Report on the Tidd Hot Gas Clean Up Program covers the period from initial Proof-of-Concept testing in August, 1990, through final equipment inspections in May, 1995. The Tidd Hot Gas Clean Up (HGCU) system was installed in the Tidd Pressurized Fluidized Bed Combustion (PFBC) Demonstration Plant, which is the first utility-scale PFBC plant in the United States. Detailed design work on the project began in July, 1990, and site construction began in December, 1991. Initial operation of the system occurred in May, 1992, and the hot gas filter was commissioned in October, 1992. The test program ended inmore » March, 1995, when the Tidd Plant was shut down following its four-year test program. Section 1.0 of this report is an executive summary of the project covering the project background, system description, test results and conclusions. Section 2.0 is an introduction covering the program objectives and schedule. Section 3.0 provides detailed descriptions of the system and its major components. Section 4.0 provides detailed results of all testing including observations and posttest inspection results. Sections 5.0 and 6.0 list the program conclusions and recommendations, respectively. Appendix I is a report prepared by Southern Research Institute on the properties of Tidd PFBC ash sampled during the test program. Appendix II is a report prepared by Westinghouse STC on the performance of candle filter fail-safe regenerator devices.« less
Computed Potential Energy Surfaces for Chemical Reactions
NASA Technical Reports Server (NTRS)
Heinemann, K.; Walch, Stephen P.; Levin, Eugene
1993-01-01
A manuscript describing the calculations on the (1)CH2 + H2O, H2 + HCOH, and H2 + H2CO product channels in the CH3 + OH reaction, which were described in the last progress report, has been accepted for publication in J. Chem. Phys., and a copy of the manuscript is included in the appendix. The production of (1)CH2 in this reaction is important in hydrocarbon combustion since (1)CH2 is highly reactive and would be expected to insert into N2, possibly leading to a new source for prompt NO(x) (vide infra). During the last six months new calculations have been carried out for the NH2 + NO system, which is important in the thermal de-NO(x) process.
Code of Federal Regulations, 2012 CFR
2012-07-01
... Pollutants for Stationary Combustion Turbines Pt. 63, Subpt. YYYY, Table 3 Table 3 to Subpart YYYY of Part 63... points AND Method 1 or 1A of 40 CFR part 60, appendix A § 63.7(d)(1)(i) if using an air pollution control device, the sampling site must be located at the outlet of the air pollution control device. c. determine...
1988-06-01
petroleum and combustion products. Consequently, the PSDDA list of chemicals of concern includes 16 polynuclear aromatic hydrocarbons (PAHs). Measurement...This material usually includes slurry water. Hydrocarbon . An organic compound composed of carbon and hydrogen. Petroleum and its derived compounds... Hydrocarbons Phthalates Pesticides Miscellaneous Compounds Biological Testing --Amphipod Bioassay Microtox Bioassay Macoma Bioaccumulation Costs for
DOE Office of Scientific and Technical Information (OSTI.GOV)
Not Available
1977-12-01
An NOx control technology assessment study was conducted to examine the effectiveness of low-excess-air firing, staged combustion, flue gas recirculation, and current burner/boiler designs as applied to coal-fired utility boilers. Significant variations in NOx emissions exist with boiler type, firing method, and coal type, but a relative comparison of emissions control performance, cost, and operational considerations is presented for each method. The study emphasized the numerous operational factors that are of major importance to the user in selecting and implementing a combustion modification technique. Staged combustion and low-excess-air operation were identified as the most cost-effective methods for existing units. Closemore » control of local air/fuel ratios and rigorous combustion equipment maintenance are essential to the success of both methods. Flue gas recirculation is relatively ineffective and has the added concern of tube erosion. More research is needed to resolve potential corrosion concerns with low-NOx operating modes. Low-NOx burners in conjunction with a compartmentalized windbox are capable of meeting a 0.6-lb/million Btu emission level on new units. Advanced burner designs are being developed to meet research emission goals of approximately 0.25 lb/MBtu.« less
NASA Technical Reports Server (NTRS)
1979-01-01
Results of a study leading to the preliminary design of a five passenger hybrid vehicle utilizing two energy sources (electricity and gasoline/diesel fuel) to minimize petroleum usage on a fleet basis are presented. The study methodology is described. Vehicle characterizations, the mission description, characterization, and impact on potential sales, and the rationale for the selection of the reference internal combustion engine vehicle are presented. Conclusions and recommendations of the mission analysis and performance specification report are included.
DOT National Transportation Integrated Search
1973-12-01
The contents are: Appendix B - Detailed flow diagrams - new systems cost program; Appendix C and D - Typical input and output data - new system cost program; Appendix E - Compiled listings - highway transit cost program; Appendix F and G - Typical in...
Code of Federal Regulations, 2011 CFR
2011-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1245 Section 60.1245... appendix F requirements to evaluate continuous emission monitoring systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or...
Code of Federal Regulations, 2010 CFR
2010-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1245 Section 60.1245... appendix F requirements to evaluate continuous emission monitoring systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or...
Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle
Zuo, Baifang; Johnson, Thomas; Ziminsky, Willy; Khan, Abdul
2013-12-17
A combustion system includes a first combustion chamber and a second combustion chamber. The second combustion chamber is positioned downstream of the first combustion chamber. The combustion system also includes a pre-mixed, direct-injection secondary fuel nozzle. The pre-mixed, direct-injection secondary fuel nozzle extends through the first combustion chamber into the second combustion chamber.
Code of Federal Regulations, 2010 CFR
2010-07-01
... appendix B or appendix F requirements to evaluate continuous emission monitoring systems? 62.15190 Section... evaluate continuous emission monitoring systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission...
Code of Federal Regulations, 2011 CFR
2011-07-01
... appendix B or appendix F requirements to evaluate continuous emission monitoring systems? 62.15190 Section... evaluate continuous emission monitoring systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission...
Atoms and Molecules Interacting with Light
NASA Astrophysics Data System (ADS)
van der Straten, Peter; Metcalf, Harold
2016-02-01
Part I. Atom-Light Interaction: 1. The classical physics pathway; Appendix 1.A. Damping force on an accelerating charge; Appendix 1.B. Hanle effect; Appendix 1.C. Optical tweezers; 2. Interaction of two-level atoms and light; Appendix 2.A. Pauli matrices for motion of the bloch vector; Appendix 2.B. The Ramsey method; Appendix 2.C. Echoes and interferometry; Appendix 2.D. Adiabatic rapid passage; Appendix 2.E Superposition and entanglement; 3. The atom-light interaction; Appendix 3.A. Proof of the oscillator strength theorem; Appendix 3.B. Electromagnetic fields; Appendix 3.C. The dipole approximation; Appendix 3.D. Time resolved fluorescence from multi-level atoms; 4. 'Forbidden' transitions; Appendix 4.A. Higher order approximations; 5. Spontaneous emission; Appendix 5.A. The quantum mechanical harmonic oscillator; Appendix 5.B. Field quantization; Appendix 5.C. Alternative theories to QED; 6. The density matrix; Appendix 6.A. The Liouville-von Neumann equation; Part II. Internal Structure: 7. The hydrogen atom; Appendix 7.A. Center-of-mass motion; Appendix 7.B. Coordinate systems; Appendix 7.C. Commuting operators; Appendix 7.D. Matrix elements of the radial wavefunctions; 8. Fine structure; Appendix 8.A. The Sommerfeld fine-structure constant; Appendix 8.B. Measurements of the fine structure 9. Effects of the nucleus; Appendix 9.A. Interacting magnetic dipoles; Appendix 9.B. Hyperfine structure for two spin =2 particles; Appendix 9.C. The hydrogen maser; 10. The alkali-metal atoms; Appendix 10.A. Quantum defects for the alkalis; Appendix 10.B. Numerov method; 11. Atoms in magnetic fields; Appendix 11.A. The ground state of atomic hydrogen; Appendix 11.B. Positronium; Appendix 11.C. The non-crossing theorem; Appendix 11.D. Passage through an anticrossing: Landau-Zener transitions; 12. Atoms in electric fields; 13. Rydberg atoms; 14. The helium atom; Appendix 14.A. Variational calculations; Appendix 14.B. Detail on the variational calculations of the ground state; 15. The periodic system of the elements; Appendix 15. A paramagnetism; Appendix 15.B. The color of gold; 16. Molecules; Appendix 16.A. Morse potential; 17. Binding in the hydrogen molecule; Appendix 17.A. Confocal elliptical coordinates; Appendix 17.B. One-electron two-center integrals; Appendix 17.C. Electron-electron interaction in molecular hydrogen; 18. Ultra-cold chemistry; Part III. Applications: 19. Optical forces and laser cooling; 20. Confinement of neutral atoms; 21. Bose-Einstein condensation; Appendix 21.A. Distribution functions; Appendix 21.B. Density of states; 22. Cold molecules; 23. Three level systems; Appendix 23.A. General Case for _1 , _2; 24. Fundamental physics; Part IV. Appendices: Appendix A. Notation and definitions; Appendix B. Units and notation; Appendix C. Angular momentum in quantum mechanics; Appendix D. Transition strengths; References; Index.
48 CFR Appendix G to Chapter 2 - [Reserved
Code of Federal Regulations, 2013 CFR
2013-10-01
... 48 Federal Acquisition Regulations System 3 2013-10-01 2013-10-01 false [Reserved] G Appendix G to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendix G to Chapter 2 [Reserved] ...
48 CFR Appendix G to Chapter 2 - [Reserved
Code of Federal Regulations, 2011 CFR
2011-10-01
... 48 Federal Acquisition Regulations System 3 2011-10-01 2011-10-01 false [Reserved] G Appendix G to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendix G to Chapter 2 [Reserved] ...
48 CFR Appendix G to Chapter 2 - [Reserved
Code of Federal Regulations, 2010 CFR
2010-10-01
... 48 Federal Acquisition Regulations System 3 2010-10-01 2010-10-01 false [Reserved] G Appendix G to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendix G to Chapter 2 [Reserved] ...
48 CFR Appendix G to Chapter 2 - [Reserved
Code of Federal Regulations, 2012 CFR
2012-10-01
... 48 Federal Acquisition Regulations System 3 2012-10-01 2012-10-01 false [Reserved] G Appendix G to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendix G to Chapter 2 [Reserved] ...
48 CFR Appendix G to Chapter 2 - [Reserved
Code of Federal Regulations, 2014 CFR
2014-10-01
... 48 Federal Acquisition Regulations System 3 2014-10-01 2014-10-01 false [Reserved] G Appendix G to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendix G to Chapter 2 [Reserved] ...
CO-FIRING COAL: FEEDLOT AND LITTER BIOMASS FUELS
DOE Office of Scientific and Technical Information (OSTI.GOV)
Dr. Kalyan Annamalai; Dr. John Sweeten; Dr. Sayeed Mukhtar
2000-10-24
The following are proposed activities for quarter 1 (6/15/00-9/14/00): (1) Finalize the allocation of funds within TAMU to co-principal investigators and the final task lists; (2) Acquire 3 D computer code for coal combustion and modify for cofiring Coal:Feedlot biomass and Coal:Litter biomass fuels; (3) Develop a simple one dimensional model for fixed bed gasifier cofired with coal:biomass fuels; and (4) Prepare the boiler burner for reburn tests with feedlot biomass fuels. The following were achieved During Quarter 5 (6/15/00-9/14/00): (1) Funds are being allocated to co-principal investigators; task list from Prof. Mukhtar has been received (Appendix A); (2) Ordermore » has been placed to acquire Pulverized Coal gasification and Combustion 3 D (PCGC-3) computer code for coal combustion and modify for cofiring Coal: Feedlot biomass and Coal: Litter biomass fuels. Reason for selecting this code is the availability of source code for modification to include biomass fuels; (3) A simplified one-dimensional model has been developed; however convergence had not yet been achieved; and (4) The length of the boiler burner has been increased to increase the residence time. A premixed propane burner has been installed to simulate coal combustion gases. First coal, as a reburn fuel will be used to generate base line data followed by methane, feedlot and litter biomass fuels.« less
48 CFR Appendixes B-E to Chapter 2 - [Reserved
Code of Federal Regulations, 2012 CFR
2012-10-01
... 48 Federal Acquisition Regulations System 3 2012-10-01 2012-10-01 false [Reserved] B Appendixes B-E to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendixes B-E to Chapter 2 [Reserved] ...
48 CFR Appendixes B-E to Chapter 2 - [Reserved
Code of Federal Regulations, 2014 CFR
2014-10-01
... 48 Federal Acquisition Regulations System 3 2014-10-01 2014-10-01 false [Reserved] B Appendixes B-E to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendixes B-E to Chapter 2 [Reserved] ...
48 CFR Appendixes B-E to Chapter 2 - [Reserved
Code of Federal Regulations, 2011 CFR
2011-10-01
... 48 Federal Acquisition Regulations System 3 2011-10-01 2011-10-01 false [Reserved] B Appendixes B-E to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendixes B-E to Chapter 2 [Reserved] ...
48 CFR Appendixes B-E to Chapter 2 - [Reserved
Code of Federal Regulations, 2010 CFR
2010-10-01
... 48 Federal Acquisition Regulations System 3 2010-10-01 2010-10-01 false [Reserved] B Appendixes B-E to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Appendixes B-E to Chapter 2 [Reserved] ...
AAPSilver System Performance Validation
2012-12-01
10 APPENDIX A. NATIONAL GEODETIC SURVEY FORWARD OUTPUT FOR BPP ALPHA ... A-1...APPENDIX B. NATIONAL GEODETIC SURVEY FORWARD OUTPUT FOR BPP BRAVO ...B-1 APPENDIX C. NATIONAL GEODETIC SURVEY FORWARD OUTPUT FOR BPP CHARLIE...SURVEY FORWARD OUTPUT FOR BPP DELTA ... D-1 APPENDIX E. NATIONAL GEODETIC SURVEY FORWARD OUTPUT FOR BPP ECHO ......E-1 AAPSilver System Performance
Combustor nozzle for a fuel-flexible combustion system
Haynes, Joel Meier [Niskayuna, NY; Mosbacher, David Matthew [Cohoes, NY; Janssen, Jonathan Sebastian [Troy, NY; Iyer, Venkatraman Ananthakrishnan [Mason, OH
2011-03-22
A combustor nozzle is provided. The combustor nozzle includes a first fuel system configured to introduce a syngas fuel into a combustion chamber to enable lean premixed combustion within the combustion chamber and a second fuel system configured to introduce the syngas fuel, or a hydrocarbon fuel, or diluents, or combinations thereof into the combustion chamber to enable diffusion combustion within the combustion chamber.
Command Flight Path Display. Phase I and II. Appendix F.
1983-09-01
AD -R145 858 COMMAND FLIGHT PATH DISPLAY PHASE I AND 11 APPENDIX F / (U) SYSTEMS ASSOCIATES INC LONG BEACH CA RESOURCE MANAGEMENT SYSTEMS DIY SEP...34- (Appendix F) .ś. SYSTEMS ASSOCIATES INC* of CALIFORNIA t. Resource Management Systems Division DTICL it~~~ll ELECTE 1 o..-- , ~SEP 2 4 1984...Availability Codos Avail and/or Dist Special "i j L i 7 7 .... Contained in this appendix are the various plots generated dur- ing data reduction. Parameters
Dry low combustion system with means for eliminating combustion noise
Verdouw, Albert J.; Smith, Duane; McCormick, Keith; Razdan, Mohan K.
2004-02-17
A combustion system including a plurality of axially staged tubular premixers to control emissions and minimize combustion noise. The combustion system includes a radial inflow premixer that delivers the combustion mixture across a contoured dome into the combustion chamber. The axially staged premixers having a twist mixing apparatus to rotate the fluid flow and cause improved mixing without causing flow recirculation that could lead to pre-ignition or flashback.
Code of Federal Regulations, 2012 CFR
2012-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1245 Section 60.1245... Commenced After June 6, 2001 Continuous Emission Monitoring § 60.1245 Am I exempt from any appendix B or... carbon dioxide) continuous emission monitoring system. Therefore, your oxygen (or carbon dioxide...
High efficiency vapor-fed AMTEC system for direct conversion. Appendices for final report
DOE Office of Scientific and Technical Information (OSTI.GOV)
Anderson, W.G.; Bland, J.J.
1997-05-23
This report consists of four appendices for the final report. They are: Appendix A: 700 C Vapor-Fed AMTEC Cell Calculations; Appendix B: 700 C Vapor-Fed AMTEC Cell Parts Drawings; Appendix C: 800 C Vapor-Fed AMTEC Cell Calculations; and Appendix D: 800 C Wick-Pumped AMTEC Cell System Design.
Statistical Mechanics and Applications in Condensed Matter
NASA Astrophysics Data System (ADS)
Di Castro, Carlo; Raimondi, Roberto
2015-08-01
Preface; 1. Thermodynamics: a brief overview; 2. Kinetics; 3. From Boltzmann to Gibbs; 4. More ensembles; 5. The thermodynamic limit and its thermodynamic stability; 6. Density matrix and quantum statistical mechanics; 7. The quantum gases; 8. Mean-field theories and critical phenomena; 9. Second quantization and Hartree-Fock approximation; 10. Linear response and fluctuation-dissipation theorem in quantum systems: equilibrium and small deviations; 11. Brownian motion and transport in disordered systems; 12. Fermi liquids; 13. The Landau theory of the second order phase transitions; 14. The Landau-Wilson model for critical phenomena; 15. Superfluidity and superconductivity; 16. The scaling theory; 17. The renormalization group approach; 18. Thermal Green functions; 19. The microscopic foundations of Fermi liquids; 20. The Luttinger liquid; 21. Quantum interference effects in disordered electron systems; Appendix A. The central limit theorem; Appendix B. Some useful properties of the Euler Gamma function; Appendix C. Proof of the second theorem of Yang and Lee; Appendix D. The most probable distribution for the quantum gases; Appendix E. Fermi-Dirac and Bose-Einstein integrals; Appendix F. The Fermi gas in a uniform magnetic field: Landau diamagnetism; Appendix G. Ising and gas-lattice models; Appendix H. Sum over discrete Matsubara frequencies; Appendix I. Hydrodynamics of the two-fluid model of superfluidity; Appendix J. The Cooper problem in the theory of superconductivity; Appendix K. Superconductive fluctuations phenomena; Appendix L. Diagrammatic aspects of the exact solution of the Tomonaga Luttinger model; Appendix M. Details on the theory of the disordered Fermi liquid; References; Author index; Index.
Code of Federal Regulations, 2011 CFR
2011-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1735 Section 60.1735... systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission monitoring system. Therefore...
Code of Federal Regulations, 2010 CFR
2010-07-01
... appendix F requirements to evaluate continuous emission monitoring systems? 60.1735 Section 60.1735... systems? Yes, the accuracy tests for your sulfur dioxide continuous emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission monitoring system. Therefore...
48 CFR Appendix E to Chapter 7 - [Reserved
Code of Federal Regulations, 2010 CFR
2010-10-01
... 48 Federal Acquisition Regulations System 5 2010-10-01 2010-10-01 false [Reserved] E Appendix E to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendix E to Chapter 7 [Reserved] ...
Energy Efficient Engine (E3) combustion system component technology performance report
NASA Technical Reports Server (NTRS)
Burrus, D. L.; Chahrour, C. A.; Foltz, H. L.; Sabla, P. E.; Seto, S. P.; Taylor, J. R.
1984-01-01
The Energy Efficient Engine (E3) combustor effort was conducted as part of the overall NASA/GE E3 Program. This effort included the selection of an advanced double-annular combustion system design. The primary intent of this effort was to evolve a design that meets the stringent emissions and life goals of the E3, as well as all of the usual performance requirements of combustion systems for modern turbofan engines. Numerous detailed design studies were conducted to define the features of the combustion system design. Development test hardware was fabricated, and an extensive testing effort was undertaken to evaluate the combustion system subcomponents in order to verify and refine the design. Technology derived from this effort was incorporated into the engine combustion hardware design. The advanced engine combustion system was then evaluated in component testing to verify the design intent. What evolved from this effort was an advanced combustion system capable of satisfying all of the combustion system design objectives and requirements of the E3.
Weightless Environment Training Facility (WETF) materials coating evaluation, volume 3
NASA Technical Reports Server (NTRS)
1995-01-01
This volume consists of Appendices C, D, E, and F to the report on the Weightless Environment Training Facility Materials Coating Evaluation project. The project selected 10 coating systems to be evaluated in six separate exposure environments, and subject to three tests for physical properties. Appendix C is the photographic appendix of the test panels. Appendix D details methods and procedures. Appendix E lists application equipment costs. Appendix F is a compilation of the solicitation of the candidate coating systems.
48 CFR Appendixes G-H to Chapter 7 - [Reserved
Code of Federal Regulations, 2014 CFR
2014-10-01
... 48 Federal Acquisition Regulations System 5 2014-10-01 2014-10-01 false [Reserved] G Appendixes G-H to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendixes G-H to Chapter 7 [Reserved] ...
48 CFR Appendixes G-H to Chapter 7 - [Reserved
Code of Federal Regulations, 2011 CFR
2011-10-01
... 48 Federal Acquisition Regulations System 5 2011-10-01 2011-10-01 false [Reserved] G Appendixes G-H to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendixes G-H to Chapter 7 [Reserved] ...
48 CFR Appendixes G-H to Chapter 7 - [Reserved
Code of Federal Regulations, 2012 CFR
2012-10-01
... 48 Federal Acquisition Regulations System 5 2012-10-01 2012-10-01 false [Reserved] G Appendixes G-H to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendixes G-H to Chapter 7 [Reserved] ...
48 CFR Appendixes G-H to Chapter 7 - [Reserved
Code of Federal Regulations, 2013 CFR
2013-10-01
... 48 Federal Acquisition Regulations System 5 2013-10-01 2013-10-01 false [Reserved] G Appendixes G-H to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendixes G-H to Chapter 7 [Reserved] ...
48 CFR Appendixes G-H to Chapter 7 - [Reserved
Code of Federal Regulations, 2010 CFR
2010-10-01
... 48 Federal Acquisition Regulations System 5 2010-10-01 2010-10-01 false [Reserved] G Appendixes G-H to Chapter 7 Federal Acquisition Regulations System AGENCY FOR INTERNATIONAL DEVELOPMENT Appendixes G-H to Chapter 7 [Reserved] ...
29 CFR Appendix C to Subpart M of... - Personal Fall Arrest Systems
Code of Federal Regulations, 2010 CFR
2010-07-01
... with the requirements in § 1926.502(d). Paragraphs (b), (c), (d) and (e) of this Appendix describe test... Appendix D of this subpart, the test methods listed here in Appendix C can also be used to assist employers... operation. (c) Strength test. (1) During the testing of all systems, a test weight of 300 pounds plus or...
29 CFR Appendix C to Subpart M of... - Personal Fall Arrest Systems
Code of Federal Regulations, 2011 CFR
2011-07-01
... with the requirements in § 1926.502(d). Paragraphs (b), (c), (d) and (e) of this appendix describe test... appendix D of this subpart, the test methods listed here in appendix C can also be used to assist employers... operation. (c) Strength test. (1) During the testing of all systems, a test weight of 300 pounds plus or...
29 CFR Appendix B to Subpart M of... - Guardrail Systems
Code of Federal Regulations, 2011 CFR
2011-07-01
... information necessary to build a complete system, and the employer is still responsible for designing and... 29 Labor 8 2011-07-01 2011-07-01 false Guardrail Systems B Appendix B to Subpart M of Part 1926..., Subpt. M, App. B Appendix B to Subpart M of Part 1926—Guardrail Systems Non-Mandatory Guidelines for...
29 CFR Appendix B to Subpart M of... - Guardrail Systems
Code of Federal Regulations, 2010 CFR
2010-07-01
... information necessary to build a complete system, and the employer is still responsible for designing and... 29 Labor 8 2010-07-01 2010-07-01 false Guardrail Systems B Appendix B to Subpart M of Part 1926..., Subpt. M, App. B Appendix B to Subpart M of Part 1926—Guardrail Systems Non-Mandatory Guidelines for...
The Environmental Technology Verification report discusses the technology and performance of the Xonon Cool Combustion System manufactured by Catalytica Energy Systems, Inc., formerly Catalytica Combustion Systems, Inc., to control NOx emissions from gas turbines that operate wit...
36th International Symposium on Combustion (ISOC2016)
2016-12-01
GREENHOUSE GASES / IC ENGINE COMBUSTION I GAS TURBINE COMBUSTION I NOVEL COMBUSTION CONCEPTS, TECHNOLOGIES AND SYSTEMS 15. SUBJECT TERMS Reaction...pollutants and greenhouse gases; IC engine combustion; Gas turbine combustion; Novel combustion concepts, technologies and systems 16. SECURITY...PLENARY LECTURE TRANSFER (15 min) am Turbulent Flames IC Engines Laminar Flames Reaction Kinetics Gas Turbines Soot Solid Fuels/Pollutants
Technology Transfer Program (TTP). Quality Assurance System. Volume 2. Appendices
1980-03-03
LSCo Report No. - 2X23-5.1-4-I TECHNOLOGY TRANSFER PROGRAM (TTP) FINAL REPORT QUALITY ASSURANCE SYSTEM Appendix A Accuracy Control System QUALITY...4-1 TECHNOLOGY TRANSFER PROGRAM (TTP) FINAL REPORT QUALITY ASSURANCE SYSTEM Appendix A Accuracy Control System QUALITY ASSURANCE VOLUME 2 APPENDICES...prepared by: Livingston Shipbuilding Company Orange, Texas March 3, 1980 APPENDIX A ACCURACY CONTROL SYSTEM . IIII MARINE TECHNOLOGY. INC. HP-121
Code of Federal Regulations, 2014 CFR
2014-01-01
... Banks: Tier 1 Leverage Measure B Appendix B to Part 208 Banks and Banking FEDERAL RESERVE SYSTEM BOARD... RESERVE SYSTEM (REGULATION H) Pt. 208, App. B Appendix B to Part 208—Capital Adequacy Guidelines for State... state member banks are outlined in Appendix A to this part. b. The guidelines apply to all state member...
14 CFR Appendix E to Part 417 - Flight Termination System Testing and Analysis
Code of Federal Regulations, 2012 CFR
2012-01-01
... contains requirements for tests and analyses that apply to all flight termination systems and the... termination system components that satisfy the requirements of this appendix. (b) Component tests and analyses. A component must satisfy each test or analysis required by any table of this appendix to demonstrate...
14 CFR Appendix E to Part 417 - Flight Termination System Testing and Analysis
Code of Federal Regulations, 2010 CFR
2010-01-01
... contains requirements for tests and analyses that apply to all flight termination systems and the... termination system components that satisfy the requirements of this appendix. (b) Component tests and analyses. A component must satisfy each test or analysis required by any table of this appendix to demonstrate...
14 CFR Appendix E to Part 417 - Flight Termination System Testing and Analysis
Code of Federal Regulations, 2013 CFR
2013-01-01
... contains requirements for tests and analyses that apply to all flight termination systems and the... termination system components that satisfy the requirements of this appendix. (b) Component tests and analyses. A component must satisfy each test or analysis required by any table of this appendix to demonstrate...
14 CFR Appendix E to Part 417 - Flight Termination System Testing and Analysis
Code of Federal Regulations, 2014 CFR
2014-01-01
... contains requirements for tests and analyses that apply to all flight termination systems and the... termination system components that satisfy the requirements of this appendix. (b) Component tests and analyses. A component must satisfy each test or analysis required by any table of this appendix to demonstrate...
14 CFR Appendix E to Part 417 - Flight Termination System Testing and Analysis
Code of Federal Regulations, 2011 CFR
2011-01-01
... contains requirements for tests and analyses that apply to all flight termination systems and the... termination system components that satisfy the requirements of this appendix. (b) Component tests and analyses. A component must satisfy each test or analysis required by any table of this appendix to demonstrate...
A prototype Knowledge-Based System to Aid Space System Restoration Management.
1986-12-01
Systems. ......... 122 Appendix B: Computation of Weights With AHP . . .. 132 Appendix C: ART Code .. ............... 138 Appendix D: Test Outputs...45 5.1 Earth Coverage With Geosynchronous Satellites 49 5.2 Space System Configurations ... ........... . 50 5.3 AHP Hierarchy...67 5.4 AHP Hierarchy With Weights .... ............ 68 6.1 TALK Schema Structure ..... .............. 75 6.2 ART Code for TALK Satellite C
14 CFR Appendix I to Part 25 - Installation of an Automatic Takeoff Thrust Control System (ATTCS)
Code of Federal Regulations, 2011 CFR
2011-01-01
... Appendix I to Part 25—Installation of an Automatic Takeoff Thrust Control System (ATTCS) I25.1General. (a... crew to increase thrust or power. I25.2Definitions. (a) Automatic Takeoff Thrust Control System (ATTCS... Control System (ATTCS) I Appendix I to Part 25 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION...
32 CFR Appendix C to Part 323 - Instructions for Preparation of Reports to New or Altered Systems
Code of Federal Regulations, 2010 CFR
2010-07-01
... or Altered Systems C Appendix C to Part 323 National Defense Department of Defense (Continued) OFFICE.... 323, App. C Appendix C to Part 323—Instructions for Preparation of Reports to New or Altered Systems... activities that are the sources, recipients, or users of the information in the system. C. Supporting...
NASA Technical Reports Server (NTRS)
1977-01-01
Aspects of combustion technology in power systems are considered, taking into account a combustion in large boilers, the control of over-all thermal efficiency of combustion heating systems, a comparison of mathematical models of the radiative behavior of a large-scale experimental furnace, a concentric multiannular swirl burner, and the effects of water introduction on diesel engine combustion and emissions. Attention is also given to combustion and related processes in energy production from coal, spray and droplet combustion, soot formation and growth, the kinetics of elementary reactions, flame structure and chemistry, propellant ignition and combustion, fire and explosion research, mathematical modeling, high output combustion systems, turbulent flames and combustion, and ignition, optical, and electrical properties.
NASA Technical Reports Server (NTRS)
Muss, J. A.; Nguyen, T. V.; Johnson, C. W.
1991-01-01
The appendices A-K to the user's manual for the rocket combustor interactive design (ROCCID) computer program are presented. This includes installation instructions, flow charts, subroutine model documentation, and sample output files. The ROCCID program, written in Fortran 77, provides a standardized methodology using state of the art codes and procedures for the analysis of a liquid rocket engine combustor's steady state combustion performance and combustion stability. The ROCCID is currently capable of analyzing mixed element injector patterns containing impinging like doublet or unlike triplet, showerhead, shear coaxial and swirl coaxial elements as long as only one element type exists in each injector core, baffle, or barrier zone. Real propellant properties of oxygen, hydrogen, methane, propane, and RP-1 are included in ROCCID. The properties of other propellants can be easily added. The analysis models in ROCCID can account for the influences of acoustic cavities, helmholtz resonators, and radial thrust chamber baffles on combustion stability. ROCCID also contains the logic to interactively create a combustor design which meets input performance and stability goals. A preliminary design results from the application of historical correlations to the input design requirements. The steady state performance and combustion stability of this design is evaluated using the analysis models, and ROCCID guides the user as to the design changes required to satisfy the user's performance and stability goals, including the design of stability aids. Output from ROCCID includes a formatted input file for the standardized JANNAF engine performance prediction procedure.
Real-time combustion controls and diagnostics sensors (CCADS)
Thornton, Jimmy D.; Richards, George A.; Dodrill, Keith A.; Nutter, Jr., Roy S.; Straub, Douglas
2005-05-03
The present invention is directed to an apparatus for the monitoring of the combustion process within a combustion system. The apparatus comprises; a combustion system, a means for supplying fuel and an oxidizer, a device for igniting the fuel and oxidizer in order to initiate combustion, and a sensor for determining the current conducted by the combustion process. The combustion system comprises a fuel nozzle and an outer shell attached to the combustion nozzle. The outer shell defines a combustion chamber. Preferably the nozzle is a lean premix fuel nozzle (LPN). Fuel and an oxidizer are provided to the fuel nozzle at separate rates. The fuel and oxidizer are ignited. A sensor positioned within the combustion system comprising at least two electrodes in spaced-apart relationship from one another. At least a portion of the combustion process or flame is between the first and second electrodes. A voltage is applied between the first and second electrodes and the magnitude of resulting current between the first and second electrodes is determined.
Code of Federal Regulations, 2010 CFR
2010-10-01
... 46 Shipping 1 2010-10-01 2010-10-01 false [Reserved] A Appendix A Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY MERCHANT MARINE OFFICERS AND SEAMEN CHEMICAL TESTING Management Information System Management Information System requirements. Appendix A [Reserved] 46 CFR Ch. I (10-1-10 Edition...
Code of Federal Regulations, 2012 CFR
2012-10-01
... Third-Party Assessment of PTC System Safety Verification and Validation F Appendix F to Part 236... Safety Verification and Validation (a) This appendix provides minimum requirements for mandatory independent third-party assessment of PTC system safety verification and validation pursuant to subpart H or I...
Code of Federal Regulations, 2014 CFR
2014-10-01
... Third-Party Assessment of PTC System Safety Verification and Validation F Appendix F to Part 236... Safety Verification and Validation (a) This appendix provides minimum requirements for mandatory independent third-party assessment of PTC system safety verification and validation pursuant to subpart H or I...
Code of Federal Regulations, 2011 CFR
2011-10-01
... Third-Party Assessment of PTC System Safety Verification and Validation F Appendix F to Part 236... Safety Verification and Validation (a) This appendix provides minimum requirements for mandatory independent third-party assessment of PTC system safety verification and validation pursuant to subpart H or I...
Code of Federal Regulations, 2013 CFR
2013-10-01
... Third-Party Assessment of PTC System Safety Verification and Validation F Appendix F to Part 236... Safety Verification and Validation (a) This appendix provides minimum requirements for mandatory independent third-party assessment of PTC system safety verification and validation pursuant to subpart H or I...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Thayer, G.R.; Williamson, K.D. Jr.; Ramirez, O.
The authors compare the competitive position of peat for energy with coal, oil, and cogenerative systems in gasifiers and solid-fuel boilers. They also explore the possibility for peat use in industry. To identify the major factors, they analyze costs using a Los Alamos levelized cost code, and they study parametric costs, comparing peat production in constant dollars with interest rates and return on investment. They consider costs of processing plant construction, sizes and kinds of boilers, retrofitting, peat drying, and mining methods. They examine mining requirements for Moin, Changuinola, and El Cairo and review wet mining and dewatering methods. Peatmore » can, indeed, be competitive with other energy sources, but this depends on the ratio of fuel costs to boiler costs. This ratio is nearly constant in comparison with cogeneration in a steam-only production system. For grate boilers using Costa Rican high-ash peat, and for small nonautomatic boilers now used in Costa Rica, the authors recommend combustion tests. An appendix contains a preliminary mining plan and cost estimate for the El Cairo peat deposit. 8 refs., 43 figs., 19 tabs.« less
Complementary and Alternative Medicine in the Military Health System: Appendixes
2017-01-01
report. Appendixes F through H supply other supplementary material. Appendixes F and G contain the CAM survey instrument and a glossary of CAM services...respectively. Appendix H contains tables of detailed results from the CAM survey and the MHS administrative data analyses. Individual tables in...this appendix are referenced in Chapters Three through Seven of the main report. 2 Table of Contents Appendix F: CAM Survey Instrument
DOT National Transportation Integrated Search
1996-06-01
This volume expands on the presentations in the main manual by presenting further discussions and examples. Contents: Appendix A: The Costs of Travel Surveys; Appendix B: Census Data for Travel Surveys; Appendix C: An Example of the Systems Capabilit...
NASA Technical Reports Server (NTRS)
1972-01-01
An analysis of the combustion products resulting from the solid propellant rocket engines of the space shuttle booster is presented. Calculation of the degree of pollution indicates that the only potentially harmful pollutants, carbon monoxide and hydrochloric acid, will be too diluted to constitute a hazard. The mass of products ejected during a launch within the troposphere is insignificant in terms of similar materials that enter the atmosphere from other sources. Noise pollution will not exceed that obtained from the Saturn 5 launch vehicle.
U. S. Army Land Warfare Laboratory. Volume II Appendix B. Task Sheets
1974-06-01
Free-Drop Water Container B-256 *06-S-64 Riot Shield 01-S-65 Cl Mob Control Equipment Studies 3-257 02-S-65 Compass - Fog and Fungus Proof B-258 03-S-65...Combustion Engine B-360 05-C-69 Mini-Grenade Munitions 3-36. 06-C-69 Explosive Detector - Plasma Chromatography -chnique B1-362 07-C-69 Grenade, Smoke...Mechanical Earth Waves B-406 05-P-63 Non-Electric Projector B-407 06-P-63 Communication by Earth Currents B-408 07-P-63 Ultrasonics B-409 08-P-63 Acoustic
Energy Efficient Engine combustor test hardware detailed design report
NASA Technical Reports Server (NTRS)
Burrus, D. L.; Chahrour, C. A.; Foltz, H. L.; Sabla, P. E.; Seto, S. P.; Taylor, J. R.
1984-01-01
The Energy Efficient Engine (E3) Combustor Development effort was conducted as part of the overall NASA/GE E3 Program. This effort included the selection of an advanced double-annular combustion system design. The primary intent was to evolve a design which meets the stringent emissions and life goals of the E3 as well as all of the usual performance requirements of combustion systems for modern turbofan engines. Numerous detailed design studies were conducted to define the features of the combustion system design. Development test hardware was fabricated, and an extensive testing effort was undertaken to evaluate the combustion system subcomponents in order to verify and refine the design. Technology derived from this development effort will be incorporated into the engine combustion system hardware design. This advanced engine combustion system will then be evaluated in component testing to verify the design intent. What is evolving from this development effort is an advanced combustion system capable of satisfying all of the combustion system design objectives and requirements of the E3. Fuel nozzle, diffuser, starting, and emissions design studies are discussed.
Code of Federal Regulations, 2010 CFR
2010-10-01
..., App. H Appendix H to Part 40—DOT Drug and Alcohol Testing Management Information System (MIS) Data... 49 Transportation 1 2010-10-01 2010-10-01 false DOT Drug and Alcohol Testing Management Information System (MIS) Data Collection Form H Appendix H to Part 40 Transportation Office of the Secretary...
29 CFR Appendix C to Subpart M of... - Personal Fall Arrest Systems
Code of Federal Regulations, 2014 CFR
2014-07-01
... appendix D of this subpart, the test methods listed here in appendix C can also be used to assist employers... about the system based on its performance during testing so that the employer can know if the system... deceleration device of the self-retracting type since this can result in additional free fall for which the...
29 CFR Appendix C to Subpart M of... - Personal Fall Arrest Systems
Code of Federal Regulations, 2013 CFR
2013-07-01
... appendix D of this subpart, the test methods listed here in appendix C can also be used to assist employers... about the system based on its performance during testing so that the employer can know if the system... deceleration device of the self-retracting type since this can result in additional free fall for which the...
29 CFR Appendix C to Subpart M of... - Personal Fall Arrest Systems
Code of Federal Regulations, 2012 CFR
2012-07-01
... appendix D of this subpart, the test methods listed here in appendix C can also be used to assist employers... about the system based on its performance during testing so that the employer can know if the system... deceleration device of the self-retracting type since this can result in additional free fall for which the...
29 CFR Appendix F to Subpart P of... - Selection of Protective Systems
Code of Federal Regulations, 2012 CFR
2012-07-01
... 29 Labor 8 2012-07-01 2012-07-01 false Selection of Protective Systems F Appendix F to Subpart P.... 1926, Subpt. P, App. F Appendix F to Subpart P of Part 1926—Selection of Protective Systems The following figures are a graphic summary of the requirements contained in subpart P for excavations 20 feet...
29 CFR Appendix F to Subpart P of... - Selection of Protective Systems
Code of Federal Regulations, 2014 CFR
2014-07-01
... 29 Labor 8 2014-07-01 2014-07-01 false Selection of Protective Systems F Appendix F to Subpart P.... 1926, Subpt. P, App. F Appendix F to Subpart P of Part 1926—Selection of Protective Systems The following figures are a graphic summary of the requirements contained in subpart P for excavations 20 feet...
29 CFR Appendix F to Subpart P of... - Selection of Protective Systems
Code of Federal Regulations, 2013 CFR
2013-07-01
... 29 Labor 8 2013-07-01 2013-07-01 false Selection of Protective Systems F Appendix F to Subpart P.... 1926, Subpt. P, App. F Appendix F to Subpart P of Part 1926—Selection of Protective Systems The following figures are a graphic summary of the requirements contained in subpart P for excavations 20 feet...
29 CFR Appendix F to Subpart P of... - Selection of Protective Systems
Code of Federal Regulations, 2011 CFR
2011-07-01
... 29 Labor 8 2011-07-01 2011-07-01 false Selection of Protective Systems F Appendix F to Subpart P.... 1926, Subpt. P, App. F Appendix F to Subpart P of Part 1926—Selection of Protective Systems The following figures are a graphic summary of the requirements contained in subpart P for excavations 20 feet...
Code of Federal Regulations, 2013 CFR
2013-10-01
..., App. H Appendix H to Part 40—DOT Drug and Alcohol Testing Management Information System (MIS) Data... 49 Transportation 1 2013-10-01 2013-10-01 false DOT Drug and Alcohol Testing Management Information System (MIS) Data Collection Form H Appendix H to Part 40 Transportation Office of the Secretary...
Code of Federal Regulations, 2014 CFR
2014-10-01
..., App. H Appendix H to Part 40—DOT Drug and Alcohol Testing Management Information System (MIS) Data... 49 Transportation 1 2014-10-01 2014-10-01 false DOT Drug and Alcohol Testing Management Information System (MIS) Data Collection Form H Appendix H to Part 40 Transportation Office of the Secretary...
Code of Federal Regulations, 2012 CFR
2012-10-01
..., App. H Appendix H to Part 40—DOT Drug and Alcohol Testing Management Information System (MIS) Data... 49 Transportation 1 2012-10-01 2012-10-01 false DOT Drug and Alcohol Testing Management Information System (MIS) Data Collection Form H Appendix H to Part 40 Transportation Office of the Secretary...
Code of Federal Regulations, 2011 CFR
2011-10-01
..., App. H Appendix H to Part 40—DOT Drug and Alcohol Testing Management Information System (MIS) Data... 49 Transportation 1 2011-10-01 2011-10-01 false DOT Drug and Alcohol Testing Management Information System (MIS) Data Collection Form H Appendix H to Part 40 Transportation Office of the Secretary...
14 CFR Appendix H to Part 23 - Installation of An Automatic Power Reserve (APR) System
Code of Federal Regulations, 2010 CFR
2010-01-01
... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Installation of An Automatic Power Reserve (APR) System H Appendix H to Part 23 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT... AIRPLANES Pt. 23, App. H Appendix H to Part 23—Installation of An Automatic Power Reserve (APR) System H23.1...
12 CFR Appendix G to Part 225 - [Reserved
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 3 2014-01-01 2014-01-01 false [Reserved] G Appendix G to Part 225 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) BANK HOLDING COMPANIES AND CHANGE IN BANK CONTROL (REGULATION Y) Appendix G to Part 225 [Reserved] ...
14 CFR Appendix E to Part 43 - Altimeter System Test and Inspection
Code of Federal Regulations, 2010 CFR
2010-01-01
... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Altimeter System Test and Inspection E Appendix E to Part 43 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION Pt. 43, App. E Appendix E to Part...
48 CFR Appendix to Part 1252 - Tar Matrix
Code of Federal Regulations, 2010 CFR
2010-10-01
... 48 Federal Acquisition Regulations System 5 2010-10-01 2010-10-01 false Tar Matrix Appendix to Part 1252 Federal Acquisition Regulations System DEPARTMENT OF TRANSPORTATION CLAUSES AND FORMS SOLICITATION PROVISIONS AND CONTRACT CLAUSES Pt. 1252, App. Appendix to Part 1252—Tar Matrix ER27DE05.000...
14 CFR 25.833 - Combustion heating systems.
Code of Federal Regulations, 2013 CFR
2013-01-01
... 14 Aeronautics and Space 1 2013-01-01 2013-01-01 false Combustion heating systems. 25.833 Section 25.833 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT... Combustion heating systems. Combustion heaters must be approved. [Amdt. 25-72, 55 FR 29783, July 20, 1990...
14 CFR 25.833 - Combustion heating systems.
Code of Federal Regulations, 2010 CFR
2010-01-01
... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Combustion heating systems. 25.833 Section 25.833 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT... Combustion heating systems. Combustion heaters must be approved. [Amdt. 25-72, 55 FR 29783, July 20, 1990...
14 CFR 25.833 - Combustion heating systems.
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 1 2011-01-01 2011-01-01 false Combustion heating systems. 25.833 Section 25.833 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT... Combustion heating systems. Combustion heaters must be approved. [Amdt. 25-72, 55 FR 29783, July 20, 1990...
14 CFR 25.833 - Combustion heating systems.
Code of Federal Regulations, 2012 CFR
2012-01-01
... 14 Aeronautics and Space 1 2012-01-01 2012-01-01 false Combustion heating systems. 25.833 Section 25.833 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT... Combustion heating systems. Combustion heaters must be approved. [Amdt. 25-72, 55 FR 29783, July 20, 1990...
14 CFR 25.833 - Combustion heating systems.
Code of Federal Regulations, 2014 CFR
2014-01-01
... 14 Aeronautics and Space 1 2014-01-01 2014-01-01 false Combustion heating systems. 25.833 Section 25.833 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT... Combustion heating systems. Combustion heaters must be approved. [Amdt. 25-72, 55 FR 29783, July 20, 1990...
The American Combustion Pyretron Thermal Destruction System at the U.S. EPA's Combustion Research Facility. Under the auspices of the Superfund Innovative Technology Evaluation, or SITE, program, a critical assessment was made of the American Combustion Pyretron™ oxygen enha...
1990-09-01
Oil Combustion/Fuel System 59 Derivation of HTHW Plant Condition Indices ...... ................. .. 65 Distribution System . ........ .. 66 HTHW...with Load ..... ............... .. 54 3. Boiler Efficiency Curve for Gas Combustion . 61 4. Boiler Efficiency Curve for Oil Combustion . 62 v List of...147 6. Round One Relative Responses for Gas and Oil Combustion/Fue System .... ............ . 147 7. Round One Relative Responses for Coal - Combustion
Theoretical Investigations on the Efficiency and the Conditions for the Realization of Jet Engines
NASA Technical Reports Server (NTRS)
Roy, Maurice
1950-01-01
Contents: Preliminary notes on the efficiency of propulsion systems; Part I: Propulsion systems with direct axial reaction rockets and rockets with thrust augmentation; Part II: Helicoidal reaction propulsion systems; Appendix I: Steady flow of viscous gases; Appendix II: On the theory of viscous fluids in nozzles; and Appendix III: On the thrusts augmenters, and particularly of gas augmenters
Slag processing system for direct coal-fired gas turbines
Pillsbury, Paul W.
1990-01-01
Direct coal-fired gas turbine systems and methods for their operation are provided by this invention. The gas turbine system includes a primary zone for burning coal in the presence of compressed air to produce hot combustion gases and debris, such as molten slag. The turbine system further includes a secondary combustion zone for the lean combustion of the hot combustion gases. The operation of the system is improved by the addition of a cyclone separator for removing debris from the hot combustion gases. The cyclone separator is disposed between the primary and secondary combustion zones and is in pressurized communication with these zones. In a novel aspect of the invention, the cyclone separator includes an integrally disposed impact separator for at least separating a portion of the molten slag from the hot combustion gases.
12 CFR Appendix B to Part 205 - Federal Enforcement Agencies
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 2 2014-01-01 2014-01-01 false Federal Enforcement Agencies B Appendix B to Part 205 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM ELECTRONIC FUND TRANSFERS (REGULATION E) Pt. 205, App. B Appendix B to Part 205—Federal Enforcement Agencies...
12 CFR Appendix B to Part 213 - Federal Enforcement Agencies
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 2 2014-01-01 2014-01-01 false Federal Enforcement Agencies B Appendix B to Part 213 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM CONSUMER LEASING (REGULATION M) Pt. 213, App. B Appendix B to Part 213—Federal Enforcement Agencies The...
12 CFR Appendix B to Part 205 - Federal Enforcement Agencies
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 2 2011-01-01 2011-01-01 false Federal Enforcement Agencies B Appendix B to Part 205 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM ELECTRONIC FUND TRANSFERS (REGULATION E) Pt. 205, App. B Appendix B to Part 205—Federal Enforcement Agencies...
14 CFR Appendix M to Part 25 - Fuel Tank System Flammability Reduction Means
Code of Federal Regulations, 2010 CFR
2010-01-01
... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Fuel Tank System Flammability Reduction Means M Appendix M to Part 25 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES Pt. 25, App. M Appendix M to Part...
14 CFR Appendix M to Part 25 - Fuel Tank System Flammability Reduction Means
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 1 2011-01-01 2011-01-01 false Fuel Tank System Flammability Reduction Means M Appendix M to Part 25 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION AIRCRAFT AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES Pt. 25, App. M Appendix M to Part...
12 CFR >appendix A to Part 239 - Mutual Holding Company Model Charter
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 4 2013-01-01 2013-01-01 false Mutual Holding Company Model Charter A >Appendix A to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. A >Appendix A to...
48 CFR Appendix H to Chapter 2 - Debarment and Suspension Procedures
Code of Federal Regulations, 2010 CFR
2010-10-01
... Procedures H Appendix H to Chapter 2 Federal Acquisition Regulations System DEFENSE ACQUISITION REGULATIONS SYSTEM, DEPARTMENT OF DEFENSE Ch. 2, App. H Appendix H to Chapter 2—Debarment and Suspension Procedures Sec. H-100Scope. H-101Notification. H-102Nature of proceeding. H-103Presentation of matters in...
DOE Office of Scientific and Technical Information (OSTI.GOV)
None
1978-01-31
This appendix is a part of the interim report documentation for the Global Spent Fuel Logistics System (GSFLS) study. This appendix provides the legal/regulatory reference material, supportive of Volume 2 - GSFLS Visit Finding and Evaluations; and certain background material on British Nuclear Fuel Limited (BNFL).
A Brief Study on Toxic Combustion Products of the Polymers Used in High-Pressure Oxygen Systems
NASA Technical Reports Server (NTRS)
Hshieh, Fu-Yu; Beeson, Harold D.
2005-01-01
One likely cause of polymer ignition in a high-pressure oxygen system is the adiabatic-compression heating of polymers caused by pneumatic impact. Oxidative pyrolysis or combustion of polymers in a high-pressure oxygen system could generate toxic gases. This paper investigates the feasibility of using the NASA pneumatic-impact system to conduct adiabatic-compression combustion tests and determines the toxic combustion products produced from the burning of five selected polymers. Five polymers commonly used in high-pressure oxygen systems, Zytel(Registered TradeMark) 42 (Nylon 6/6), Buna N (nitrile rubber), Witon(Registered TradeMark) A (copolymer of vinylidene fluoride and hexafluoropropylene), Neoflon(Registered TradeMark) (polychlorotrifluoroethylene), and Teflon(Registered TradeMark) (polytetrafluoroethylene), were tested in the NASA pneumatic-impact test system at 17.2-MPa oxygen pressure. The polymers were ignited and burned; combustion products were collected in a stainless-steel sample bottle and analyzed using various methods. The results show that the NASA pneumatic-impact system is an appropriate test system to conduct adiabatic-compression combustion tests and to collect combustion products for further chemical analysis. The composition of the combustion product gas generated from burning the five selected polymers are presented and discussed.
Wijmans, Johannes G [Menlo Park, CA; Merkel, Timothy C [Menlo Park, CA; Baker, Richard W [Palo Alto, CA
2011-10-11
Disclosed herein are combustion systems and power plants that incorporate sweep-based membrane separation units to remove carbon dioxide from combustion gases. In its most basic embodiment, the invention is a combustion system that includes three discrete units: a combustion unit, a carbon dioxide capture unit, and a sweep-based membrane separation unit. In a preferred embodiment, the invention is a power plant including a combustion unit, a power generation system, a carbon dioxide capture unit, and a sweep-based membrane separation unit. In both of these embodiments, the carbon dioxide capture unit and the sweep-based membrane separation unit are configured to be operated in parallel, by which we mean that each unit is adapted to receive exhaust gases from the combustion unit without such gases first passing through the other unit.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Peterson, D.; Haase, S.
2009-07-01
This report provides a market assessment of gasification and direct combustion technologies that use wood and agricultural resources to generate heat, power, or combined heat and power (CHP) for small- to medium-scale applications. It contains a brief overview of wood and agricultural resources in the U.S.; a description and discussion of gasification and combustion conversion technologies that utilize solid biomass to generate heat, power, and CHP; an assessment of the commercial status of gasification and combustion technologies; a summary of gasification and combustion system economics; a discussion of the market potential for small- to medium-scale gasification and combustion systems; andmore » an inventory of direct combustion system suppliers and gasification technology companies. The report indicates that while direct combustion and close-coupled gasification boiler systems used to generate heat, power, or CHP are commercially available from a number of manufacturers, two-stage gasification systems are largely in development, with a number of technologies currently in demonstration. The report also cites the need for a searchable, comprehensive database of operating combustion and gasification systems that generate heat, power, or CHP built in the U.S., as well as a national assessment of the market potential for the systems.« less
ERIC Educational Resources Information Center
National Endowment for the Arts, 2012
2012-01-01
This paper presents two appendices supporting the "How Art Works: The National Endowment for the Arts' Five-Year Research Agenda, with a System Map and Measurement Model" report. In Appendix A, brief descriptions of relevant studies and datasets for each node in the "How Art Works" system map are presented. This appendix is meant to supply…
Code of Federal Regulations, 2014 CFR
2014-07-01
... 33 Navigation and Navigable Waters 2 2014-07-01 2014-07-01 false Specifications for the Design, Installation and Operation of a Part Flow System for Control of Overboard Discharges E Appendix E to Part 157... Appendix E to Part 157—Specifications for the Design, Installation and Operation of a Part Flow System for...
Code of Federal Regulations, 2012 CFR
2012-07-01
... 33 Navigation and Navigable Waters 2 2012-07-01 2012-07-01 false Specifications for the Design, Installation and Operation of a Part Flow System for Control of Overboard Discharges E Appendix E to Part 157... Appendix E to Part 157—Specifications for the Design, Installation and Operation of a Part Flow System for...
Code of Federal Regulations, 2011 CFR
2011-07-01
... 33 Navigation and Navigable Waters 2 2011-07-01 2011-07-01 false Specifications for the Design, Installation and Operation of a Part Flow System for Control of Overboard Discharges E Appendix E to Part 157... Appendix E to Part 157—Specifications for the Design, Installation and Operation of a Part Flow System for...
Code of Federal Regulations, 2013 CFR
2013-07-01
... 33 Navigation and Navigable Waters 2 2013-07-01 2013-07-01 false Specifications for the Design, Installation and Operation of a Part Flow System for Control of Overboard Discharges E Appendix E to Part 157... Appendix E to Part 157—Specifications for the Design, Installation and Operation of a Part Flow System for...
NASA Technical Reports Server (NTRS)
Varma, Arvind; Mukasyan, Alexander; Pelekh, Aleksey
1997-01-01
There have been relatively few publications examining the role of gravity during combustion synthesis (CS), mostly involving thermite systems. The main goal of this research was to study the influence of gravity on the combustion characteristics of heterogeneous gasless systems. In addition, some aspects of microstructure formation processes which occur during gasless CS were also studied. Four directions for experimental investigation have been explored: (1) the influence of gravity force on the characteristic features of heterogeneous combustion wave propagation (average velocity, instantaneous velocities, shape of combustion front); (2) the combustion of highly porous mixtures (with porosity greater than that for loose powders), which cannot be obtained in normal gravity; (3) the effect of gravity on sample expansion during combustion, in order to produce highly porous materials under microgravity conditions; and (4) the effect of gravity on the structure formation mechanism during the combustion synthesis of poreless composite materials.
Code of Federal Regulations, 2011 CFR
2011-01-01
... Reverse Mortgage Transactions K Appendix K to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. K Appendix K to Part 226—Total Annual Loan Cost Rate Computations for Reverse Mortgage Transactions (a...
Code of Federal Regulations, 2012 CFR
2012-01-01
... Reverse Mortgage Transactions K Appendix K to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. K Appendix K to Part 226—Total Annual Loan Cost Rate Computations for Reverse Mortgage Transactions (a...
Code of Federal Regulations, 2010 CFR
2010-01-01
... Reverse Mortgage Transactions K Appendix K to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. K Appendix K to Part 226—Total Annual Loan Cost Rate Computations for Reverse Mortgage Transactions (a...
40 CFR Appendix A to Part 300 - The Hazard Ranking System
Code of Federal Regulations, 2014 CFR
2014-07-01
... 40 Protection of Environment 28 2014-07-01 2014-07-01 false The Hazard Ranking System A Appendix A to Part 300 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) SUPERFUND, EMERGENCY PLANNING, AND COMMUNITY RIGHT-TO-KNOW PROGRAMS NATIONAL OIL AND HAZARDOUS SUBSTANCES POLLUTION CONTINGENCY PLAN Pt. 300, App. A Appendix A to Par...
40 CFR Appendix A to Part 300 - The Hazard Ranking System
Code of Federal Regulations, 2013 CFR
2013-07-01
... 40 Protection of Environment 29 2013-07-01 2013-07-01 false The Hazard Ranking System A Appendix A to Part 300 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) SUPERFUND, EMERGENCY PLANNING, AND COMMUNITY RIGHT-TO-KNOW PROGRAMS NATIONAL OIL AND HAZARDOUS SUBSTANCES POLLUTION CONTINGENCY PLAN Pt. 300, App. A Appendix A to Par...
12 CFR Appendix C to Part 239 - Mutual Holding Company Model Bylaws
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 4 2013-01-01 2013-01-01 false Mutual Holding Company Model Bylaws C Appendix C to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. C Appendix C to Part 239...
12 CFR Appendix C to Part 239 - Mutual Holding Company Model Bylaws
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 4 2012-01-01 2012-01-01 false Mutual Holding Company Model Bylaws C Appendix C to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. C Appendix C to Part 239...
12 CFR Appendix A to Part 239 - Mutual Holding Company Model Charter
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 4 2012-01-01 2012-01-01 false Mutual Holding Company Model Charter A Appendix A to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. A Appendix A to Part 239...
12 CFR Appendix C to Part 239 - Mutual Holding Company Model Bylaws
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 4 2014-01-01 2014-01-01 false Mutual Holding Company Model Bylaws C Appendix C to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. C Appendix C to Part 239...
12 CFR Appendix A to Part 239 - Mutual Holding Company Model Charter
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 4 2014-01-01 2014-01-01 false Mutual Holding Company Model Charter A Appendix A to Part 239 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM (CONTINUED) MUTUAL HOLDING COMPANIES (REGULATION MM) Pt. 239, App. A Appendix A to Part 239...
2006-06-01
Appendix A. Demographic Questionnaire 25 Appendix B. Attentional Control Survey 27 Appendix C. NASA - TLX Questionnaire 29 Appendix D. Simulator...the National Aeronautics and Space Administration task load index ( NASA - TLX ) questionnaire (appendix C) (Hart & Staveland, 1988). The NASA - TLX is a...There were 2-minute breaks between experimental sessions. Participants assessed their workload using the NASA - TLX after they completed each
Federal Register 2010, 2011, 2012, 2013, 2014
2011-03-24
.... (n/k/a Clean Energy Combustion Systems, Inc.), Collectible Concepts Group, Inc., Communitronics of America, Inc. (n/k/a RPM Advantage, Inc.), and ConSyGen, Inc., Order of Suspension of Trading March 22..., Inc. (n/k/a Clean Energy Combustion Systems, Inc.) because it has not filed any periodic reports since...
20 CFR 404.1525 - Listing of Impairments in appendix 1.
Code of Federal Regulations, 2010 CFR
2010-04-01
... Impairments (the listings) is in appendix 1 of this subpart. It describes for each of the major body systems..., regardless of his or her age, education, or work experience. (b) How is appendix 1 organized? There are two... relationship with their counterparts in part A. (c) How do we use the listings? (1) Each body system section in...
12 CFR Appendix C to Part 230 - Effect on State Laws
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 3 2010-01-01 2010-01-01 false Effect on State Laws C Appendix C to Part 230 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM TRUTH IN SAVINGS (REGULATION DD) Pt. 230, App. C Appendix C to Part 230—Effect on State Laws (a...
Code of Federal Regulations, 2010 CFR
2010-01-01
... Annual Loan Cost Rates L Appendix L to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED) BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. L Appendix L to Part 226—Assumed Loan Periods for Computations of Total Annual Loan Cost Rates (a) Required...
12 CFR Appendix A to Part 213 - Model Forms
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 2 2010-01-01 2010-01-01 false Model Forms A Appendix A to Part 213 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM CONSUMER LEASING (REGULATION M) Pt. 213, App. A Appendix A to Part 213—Model Forms A-1Model Open-End or Finance Vehicle Lease...
12 CFR Appendix A to Part 213 - Model Forms
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 2 2011-01-01 2011-01-01 false Model Forms A Appendix A to Part 213 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM CONSUMER LEASING (REGULATION M) Pt. 213, App. A Appendix A to Part 213—Model Forms A-1Model Open-End or Finance Vehicle Lease...
NASA Technical Reports Server (NTRS)
Hanley, G. M.
1979-01-01
Appendixes for Volume 2 (Part 2) of a seven volume Satellite (SPS) report are presented. The document contains two appendixes. The first is a SPS work breakdown structure dictionary. The second gives SPS cost estimating relationships and contains the cost analyses and a description of cost elements that comprise the SPS program.
Code of Federal Regulations, 2012 CFR
2012-01-01
... 10 Energy 4 2012-01-01 2012-01-01 false Application of the System and Technical Guidelines During the Siting Process III Appendix III to Part 960 Energy DEPARTMENT OF ENERGY GENERAL GUIDELINES FOR THE PRELIMINARY SCREENING OF POTENTIAL SITES FOR A NUCLEAR WASTE REPOSITORY Pt. 960, App. III Appendix III to Part...
Code of Federal Regulations, 2014 CFR
2014-01-01
... 10 Energy 4 2014-01-01 2014-01-01 false Application of the System and Technical Guidelines During the Siting Process III Appendix III to Part 960 Energy DEPARTMENT OF ENERGY GENERAL GUIDELINES FOR THE PRELIMINARY SCREENING OF POTENTIAL SITES FOR A NUCLEAR WASTE REPOSITORY Pt. 960, App. III Appendix III to Part...
Code of Federal Regulations, 2013 CFR
2013-01-01
... 10 Energy 4 2013-01-01 2013-01-01 false Application of the System and Technical Guidelines During the Siting Process III Appendix III to Part 960 Energy DEPARTMENT OF ENERGY GENERAL GUIDELINES FOR THE PRELIMINARY SCREENING OF POTENTIAL SITES FOR A NUCLEAR WASTE REPOSITORY Pt. 960, App. III Appendix III to Part...
Code of Federal Regulations, 2010 CFR
2010-01-01
... 10 Energy 4 2010-01-01 2010-01-01 false Application of the System and Technical Guidelines During the Siting Process III Appendix III to Part 960 Energy DEPARTMENT OF ENERGY GENERAL GUIDELINES FOR THE PRELIMINARY SCREENING OF POTENTIAL SITES FOR A NUCLEAR WASTE REPOSITORY Pt. 960, App. III Appendix III to Part...
Database interfaces on NASA's heterogeneous distributed database system
NASA Technical Reports Server (NTRS)
Huang, Shou-Hsuan Stephen
1989-01-01
The syntax and semantics of all commands used in the template are described. Template builders should consult this document for proper commands in the template. Previous documents (Semiannual reports) described other aspects of this project. Appendix 1 contains all substituting commands used in the system. Appendix 2 includes all repeating commands. Appendix 3 is a collection of DEFINE templates from eight different DBMS's.
Shock-tunnel combustor testing for hypersonic vehicles
NASA Technical Reports Server (NTRS)
Loomis, Mark P.
1994-01-01
Proposed configurations for the next generation of transatmospheric vehicles will rely on air breathing propulsion systems during all or part of their mission. At flight Mach numbers greater than about 7 these engines will operate in the supersonic combustion ramjet mode (scramjet). Ground testing of these engine concepts above Mach 8 requires high pressure, high enthalpy facilities such as shock tunnels and expansion tubes. These impulse, or short duration facilities have test times on the order of a millisecond, requiring high speed instrumentation and data systems. One such facility ideally suited for scramjet testing is the NASA-Ames 16-Inch shock tunnel, which over the last two years has completed a series of tests for the NASP (National Aero-Space Plane) program at simulated flight Mach numbers ranging from 12-16. The focus of the experimental programs consisted of a series of classified tests involving a near-full scale hydrogen fueled scramjet combustor model in the semi-free jet method of engine testing whereby the compressed forebody flow ahead of the cowl inlet is reproduced (see appendix A). The AIMHYE-1 (Ames Integrated Modular Hypersonic Engine) test entry for the NASP program was completed in April 1993, while AIMHYE-2 was completed in May 1994. The test entries were regarded as successful, resulting in some of the first data of its kind on the performance of a near full scale scramjet engine at Mach 12-16. The data was distributed to NASP team members for use in design system verification and development. Due to the classified nature of the hardware and data, the data reports resulting from this work are classified and have been published as part of the NASP literature. However, an unclassified AIAA paper resulted from the work and has been included as appendix A. It contains an overview of the test program and a description of some of the important issues.
The Physical Effects of Detonation in a Closed Cylindrical Chamber
NASA Technical Reports Server (NTRS)
Draper, C S
1935-01-01
Detonation in the internal-combustion engine is studied as a physical process. It is shown that detonation is accompanied by pressure waves within the cylinder charge. Sound theory is applied to the calculation of resonant pressure-wave frequencies. Apparatus is described for direct measurement of pressure-wave frequencies. Frequencies determined from two engines of different cylinder sizes are shown to agree with the values calculated from sound theory. An outline of the theoretically possible modes of vibration in a right circular cylinder with flat ends is included. An appendix by John P. Elting gives a method of calculating pressure in the sound wave following detonation.
40 CFR 52.1281 - Original identification of plan section.
Code of Federal Regulations, 2011 CFR
2011-07-01
... prior to July 1, 1997. (b) The plan was officially submitted on February 4, 1972. (c) The plan revisions..., Appendix C; addition of testing methods, section 8, Appendix C; addition of Permit System, Appendix G and deletion of SO2 regulation, section 4, Appendix C submitted on May 4, 1972, by the Mississippi Air and...
40 CFR 52.1281 - Original identification of plan section.
Code of Federal Regulations, 2012 CFR
2012-07-01
... prior to July 1, 1997. (b) The plan was officially submitted on February 4, 1972. (c) The plan revisions..., Appendix C; addition of testing methods, section 8, Appendix C; addition of Permit System, Appendix G and deletion of SO2 regulation, section 4, Appendix C submitted on May 4, 1972, by the Mississippi Air and...
40 CFR 52.1281 - Original identification of plan section.
Code of Federal Regulations, 2013 CFR
2013-07-01
... prior to July 1, 1997. (b) The plan was officially submitted on February 4, 1972. (c) The plan revisions..., Appendix C; addition of testing methods, section 8, Appendix C; addition of Permit System, Appendix G and deletion of SO2 regulation, section 4, Appendix C submitted on May 4, 1972, by the Mississippi Air and...
NASA Technical Reports Server (NTRS)
Hanley, G.
1978-01-01
Three appendixes in support of Volume 7 are contained in this document. The three appendixes are: (1) Satellite Power System Work Breakdown Structure Dictionary; (2) SPS cost Estimating Relationships; and (3) Financial and Operational Concept. Other volumes of the final report that provide additional detail are: Executive Summary; SPS Systems Requirements; SPS Concept Evolution; SPS Point Design Definition; Transportation and Operations Analysis; and SPS Technology Requirements and Verification.
NASA Technical Reports Server (NTRS)
Hshieh, Fu-Yu; Beeson, Harold D.
2004-01-01
One likely cause of polymer ignition in a high-pressure oxygen system is adiabatic-compression heating of polymers caused by pneumatic impact. Oxidative _ pyrolysis or combustion of polymers in a high-pressure oxygen system could generate toxic gases. This paper reports the preliminary results of toxic combustion product testing of selected polymers in a pneumatic-impact test system. Five polymers commonly used in high-pressure oxygen systems, Nylon 6/6, polychlorotrifluoroethylene (CTFE), polytetrafluoroethylene (PTFE), fluoroelastomer (Viton(TradeMark) A), and nitrile rubber (Buna N), were tested in a pneumatic-impact test system at 2500- or 3500-psia oxygen pressure. The polymers were ignited and burned, then combustion products were collected in a stainless-steel sample bottle and analyzed by GC/MS/IRD, GC/FID, and GC/Methanizer/FID. The results of adiabatic-compression tests show that combustion of hydrocarbon polymers, nitrogen-containing polymers, and halogenated polymers in high-pressure oxygen systems are relatively complete. Toxicity of the combustion product gas is presumably much lower than the combustion product gas generated from ambient-pressure oxygen (or air) environments. The NASA-Lewis equilibrium code was used to determine the composition of combustion product gas generated from a simulated, adiabatic-compression test of nine polymers. The results are presented and discussed.
Real-time combustion control and diagnostics sensor-pressure oscillation monitor
Chorpening, Benjamin T [Morgantown, WV; Thornton, Jimmy [Morgantown, WV; Huckaby, E David [Morgantown, WV; Richards, George A [Morgantown, WV
2009-07-14
An apparatus and method for monitoring and controlling the combustion process in a combustion system to determine the amplitude and/or frequencies of dynamic pressure oscillations during combustion. An electrode in communication with the combustion system senses hydrocarbon ions and/or electrons produced by the combustion process and calibration apparatus calibrates the relationship between the standard deviation of the current in the electrode and the amplitudes of the dynamic pressure oscillations by applying a substantially constant voltage between the electrode and ground resulting in a current in the electrode and by varying one or more of (1) the flow rate of the fuel, (2) the flow rate of the oxidant, (3) the equivalence ratio, (4) the acoustic tuning of the combustion system, and (5) the fuel distribution in the combustion chamber such that the amplitudes of the dynamic pressure oscillations in the combustion chamber are calculated as a function of the standard deviation of the electrode current. Thereafter, the supply of fuel and/or oxidant is varied to modify the dynamic pressure oscillations.
Doherty, Brian J.
1984-07-10
A burner system particularly useful for downhole deployment includes a tubular combustion chamber unit housed within a tubular coolant jacket assembly. The combustion chamber unit includes a monolithic tube of refractory material whose inner surface defines the combustion zone. A metal reinforcing sleeve surrounds and extends the length of the refractory tube. The inner surface of the coolant jacket assembly and outer surface of the combustion chamber unit are dimensioned so that those surfaces are close to one another in standby condition so that the combustion chamber unit has limited freedom to expand with that expansion being stabilized by the coolant jacket assembly so that compression forces in the refractory tube do not exceed about one-half the safe compressive stress of the material; and the materials of the combustion chamber unit are selected to establish thermal gradient parameters across the combustion chamber unit to maintain the refractory tube in compression during combustion system start up and cool down sequences.
24 CFR 3280.710 - Venting, ventilation and combustion air.
Code of Federal Regulations, 2010 CFR
2010-04-01
... 24 Housing and Urban Development 5 2010-04-01 2010-04-01 false Venting, ventilation and combustion... Fuel Burning Systems § 3280.710 Venting, ventilation and combustion air. (a) The venting as required by... appliance listing and the appliance manufacturer's instructions. (b) Venting and combustion air systems...
24 CFR 3280.710 - Venting, ventilation and combustion air.
Code of Federal Regulations, 2014 CFR
2014-04-01
... 24 Housing and Urban Development 5 2014-04-01 2014-04-01 false Venting, ventilation and combustion... Fuel Burning Systems § 3280.710 Venting, ventilation and combustion air. (a) The venting as required by... appliance listing and the appliance manufacturer's instructions. (b) Venting and combustion air systems...
24 CFR 3280.710 - Venting, ventilation and combustion air.
Code of Federal Regulations, 2012 CFR
2012-04-01
... 24 Housing and Urban Development 5 2012-04-01 2012-04-01 false Venting, ventilation and combustion... Fuel Burning Systems § 3280.710 Venting, ventilation and combustion air. (a) The venting as required by... appliance listing and the appliance manufacturer's instructions. (b) Venting and combustion air systems...
24 CFR 3280.710 - Venting, ventilation and combustion air.
Code of Federal Regulations, 2011 CFR
2011-04-01
... 24 Housing and Urban Development 5 2011-04-01 2011-04-01 false Venting, ventilation and combustion... Fuel Burning Systems § 3280.710 Venting, ventilation and combustion air. (a) The venting as required by... appliance listing and the appliance manufacturer's instructions. (b) Venting and combustion air systems...
2009-01-05
ISS018-E-017796 (5 Jan. 2009) --- Astronaut Sandra Magnus, Expedition 18 flight engineer, works on the Fluids and Combustion Facility (FCF) Combustion Integration Rack (CIR) Passive Rack Isolation System (PaRIS) in the Destiny laboratory of the International Space Station.
24 CFR 3280.710 - Venting, ventilation and combustion air.
Code of Federal Regulations, 2013 CFR
2013-04-01
... 24 Housing and Urban Development 5 2013-04-01 2013-04-01 false Venting, ventilation and combustion... Fuel Burning Systems § 3280.710 Venting, ventilation and combustion air. (a) The venting as required by... appliance listing and the appliance manufacturer's instructions. (b) Venting and combustion air systems...
40 CFR 60.4219 - What definitions apply to this subpart?
Code of Federal Regulations, 2010 CFR
2010-07-01
... given them in the CAA and in subpart A of this part. Combustion turbine means all equipment, including but not limited to the turbine, the fuel, air, lubrication and exhaust gas systems, control systems... simple cycle combustion turbine, any regenerative/recuperative cycle combustion turbine, the combustion...
Automotive Stirling engine system component review
NASA Technical Reports Server (NTRS)
Hindes, Chip; Stotts, Robert
1987-01-01
The design and testing of the power and combustion control system for the basic Stirling engine, Mod II, are examined. The power control system is concerned with transparent operation, and the Mod II uses engine working gas pressure variation to control the power output of the engine. The main components of the power control system, the power control valve, the pump-down system, and the hydrogen stable system, are described. The combustion control system consists of a combustion air supply system and an air/fuel ratio control system, and the system is to maintain constant heater head temperature, and to maximize combustion efficiency and to minimize exhaust emissions.
32 CFR Appendix F to Part 505 - Example of a System of Records Notice
Code of Federal Regulations, 2010 CFR
2010-07-01
... 32 National Defense 3 2010-07-01 2010-07-01 true Example of a System of Records Notice F Appendix F to Part 505 National Defense Department of Defense (Continued) DEPARTMENT OF THE ARMY AID OF CIVIL AUTHORITIES AND PUBLIC RELATIONS ARMY PRIVACY ACT PROGRAM Pt. 505, App. F Appendix F to Part 505—Example of a...
Code of Federal Regulations, 2012 CFR
2012-04-01
... Development Highway System and Local Access Roads Contracts Other Than Construction Contracts C Appendix C to.... 633, Subpt. B, App. C Appendix C to Subpart B of Part 633—Additional Required Contract Provisions.... Compliance with regulations. The contractor will comply with the provisions of 23 U.S.C. 324 and with the...
Code of Federal Regulations, 2010 CFR
2010-04-01
... 23 Highways 1 2010-04-01 2010-04-01 false Guidance Criteria for Evaluating Requests for Modifications to the National Highway System D Appendix D to Subpart A of Part 470 Highways FEDERAL HIGHWAY.... 470, Subpt. A, App. D Appendix D to Subpart A of Part 470—Guidance Criteria for Evaluating Requests...
NASA Technical Reports Server (NTRS)
Strahle, W. C.
1977-01-01
A review of the subject of combustion generated noise is presented. Combustion noise is an important noise source in industrial furnaces and process heaters, turbopropulsion and gas turbine systems, flaring operations, Diesel engines, and rocket engines. The state-of-the-art in combustion noise importance, understanding, prediction and scaling is presented for these systems. The fundamentals and available theories of combustion noise are given. Controversies in the field are discussed and recommendations for future research are made.
Staged combustion with piston engine and turbine engine supercharger
Fischer, Larry E [Los Gatos, CA; Anderson, Brian L [Lodi, CA; O'Brien, Kevin C [San Ramon, CA
2006-05-09
A combustion engine method and system provides increased fuel efficiency and reduces polluting exhaust emissions by burning fuel in a two-stage combustion system. Fuel is combusted in a piston engine in a first stage producing piston engine exhaust gases. Fuel contained in the piston engine exhaust gases is combusted in a second stage turbine engine. Turbine engine exhaust gases are used to supercharge the piston engine.
Staged combustion with piston engine and turbine engine supercharger
Fischer, Larry E [Los Gatos, CA; Anderson, Brian L [Lodi, CA; O'Brien, Kevin C [San Ramon, CA
2011-11-01
A combustion engine method and system provides increased fuel efficiency and reduces polluting exhaust emissions by burning fuel in a two-stage combustion system. Fuel is combusted in a piston engine in a first stage producing piston engine exhaust gases. Fuel contained in the piston engine exhaust gases is combusted in a second stage turbine engine. Turbine engine exhaust gases are used to supercharge the piston engine.
13 CFR Appendix A to Subpart A of... - Appendix A to Subpart A of Part 113
Code of Federal Regulations, 2010 CFR
2010-01-01
... innovation and research Small Business Act, sec. 9. Procurement automated source system. Small Business Act... 13 Business Credit and Assistance 1 2010-01-01 2010-01-01 false Appendix A to Subpart A of Part 113 A Appendix A to Subpart A of Part 113 Business Credit and Assistance SMALL BUSINESS ADMINISTRATION...
40 CFR Appendix I to Subparts D... - Motorcycle Noise Emission Test Procedures
Code of Federal Regulations, 2011 CFR
2011-07-01
... Procedures I Appendix I to Subparts D and E of Part 205 Protection of Environment ENVIRONMENTAL PROTECTION... Exhaust Systems Remedial orders. Pt. 205, Subpts. D-E, App. I Appendix I to Subparts D and E of Part 205—Motorcycle Noise Emission Test Procedures Appendix I-1 to Subparts D and E—Test Procedure for Street and off...
40 CFR Appendix I to Subparts D... - Motorcycle Noise Emission Test Procedures
Code of Federal Regulations, 2010 CFR
2010-07-01
... Procedures I Appendix I to Subparts D and E of Part 205 Protection of Environment ENVIRONMENTAL PROTECTION... Exhaust Systems Remedial orders. Pt. 205, Subpts. D-E, App. I Appendix I to Subparts D and E of Part 205—Motorcycle Noise Emission Test Procedures Appendix I-1 to Subparts D and E—Test Procedure for Street and off...
1967-03-01
is restricted only by the practical range of its organic aerial vehicles which provide its high degree of mobility; a form of warfare that not only... ORGANIC AIRCRAFT RADIOS 1* Chapter and Appendix. APPENDIX 4 ARMY AIRCRAFT WEAPONS SYSTEMS APPENDIX 5 ARMY AVIATION ORGANIZATIONS IL. APPENDIX 6 AIRMOBILE...helicopters, fix,:d wing aircraft, and organizations and equipment associatetd with Army aviation. It provides basic and general information, and
46 CFR 62.35-35 - Starting systems for internal-combustion engines.
Code of Federal Regulations, 2013 CFR
2013-10-01
... 46 Shipping 2 2013-10-01 2013-10-01 false Starting systems for internal-combustion engines. 62.35-35 Section 62.35-35 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE... Starting systems for internal-combustion engines. The starting systems for propulsion engines and for prime...
46 CFR 62.35-35 - Starting systems for internal-combustion engines.
Code of Federal Regulations, 2014 CFR
2014-10-01
... 46 Shipping 2 2014-10-01 2014-10-01 false Starting systems for internal-combustion engines. 62.35-35 Section 62.35-35 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE... Starting systems for internal-combustion engines. The starting systems for propulsion engines and for prime...
46 CFR 62.35-35 - Starting systems for internal-combustion engines.
Code of Federal Regulations, 2010 CFR
2010-10-01
... 46 Shipping 2 2010-10-01 2010-10-01 false Starting systems for internal-combustion engines. 62.35-35 Section 62.35-35 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE... Starting systems for internal-combustion engines. The starting systems for propulsion engines and for prime...
46 CFR 62.35-35 - Starting systems for internal-combustion engines.
Code of Federal Regulations, 2011 CFR
2011-10-01
... 46 Shipping 2 2011-10-01 2011-10-01 false Starting systems for internal-combustion engines. 62.35-35 Section 62.35-35 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE... Starting systems for internal-combustion engines. The starting systems for propulsion engines and for prime...
46 CFR 62.35-35 - Starting systems for internal-combustion engines.
Code of Federal Regulations, 2012 CFR
2012-10-01
... 46 Shipping 2 2012-10-01 2012-10-01 false Starting systems for internal-combustion engines. 62.35-35 Section 62.35-35 Shipping COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) MARINE... Starting systems for internal-combustion engines. The starting systems for propulsion engines and for prime...
Carbon deposition model for oxygen-hydrocarbon combustion, volume 1
NASA Technical Reports Server (NTRS)
Hernandez, R.; Ito, J. I.; Niiya, K. Y.
1987-01-01
Presented are details of the design, fabrication, and testing of subscale hardware used in the evaluation of carbon deposition characteristics of liquid oxygen and three hydrocarbon fuels for both main chamber and preburner/gas generator operating conditions. In main chamber conditions, the deposition of carbon on the combustion chamber wall was investigated at mixture ratios of 2.0 to 4.0 and at pressures of 1000 to 1500 psia. No carbon deposition on the chamber walls was detected at these main chamber mixture ratios. In preburner/gas generator operating conditions, the deposition of carbon on the turbine simulator tubes was evaluated at mixture ratios of 0.20 to 0.60 and at chamber pressures of 720 to 1650 psia. The results of the tests showed carbon deposition rate to be a strong function of mixture ratio and a weak function of chamber pressure. Further analyses evaluated the operational consequences of carbon deposition on preburner/gas generator performance. The report is in two volumes, of which this is Volume 1 covering the main body of the report plus Appendixes A through D.
Assessment of Literature Related to Combustion Appliance Venting Systems
DOE Office of Scientific and Technical Information (OSTI.GOV)
Rapp, V. H.; Less, B. D.; Singer, B. C.
In many residential building retrofit programs, air tightening to increase energy efficiency is often constrained by safety concerns with naturally vented combustion appliances. Tighter residential buildings more readily depressurize when exhaust equipment is operated, making combustion appliances more prone to backdraft or spill combustion exhaust into the living space. Several measures, such as installation guidelines, vent sizing codes, and combustion safety diagnostics, are in place with the intent to prevent backdrafting and combustion spillage, but the diagnostics conflict and the risk mitigation objective is inconsistent. This literature review summarizes the metrics and diagnostics used to assess combustion safety, documents theirmore » technical basis, and investigates their risk mitigations. It compiles information from the following: codes for combustion appliance venting and installation; standards and guidelines for combustion safety diagnostics; research evaluating combustion safety diagnostics; research investigating wind effects on building depressurization and venting; and software for simulating vent system performance.« less
Evaluation of Commercial Off-the-Shelf and Government Off-the-Shelf Microclimate Cooling Systems
2005-08-01
Appendix A - Request for Information (RFI) 23 Appendix B - Memorandum from Natick Soldier Center’s International Office 25 Appendix C - Cooling Power...Data Entry Forms 7 Figure 3. Evaporative Cooling Products 9 Figure 4. Passive Phase Change Product 10 Figure 5. Liquid Circulating...Microclimate Cooling System 13 Figure 6. Compressed Air Cooling Product 15 Figure 7. Vortex Tube 15 Figure 8. Active Phase
DEMONSTRATION BULLETIN: CELLO PULSE COMBUSTION BURNER SYSTEM/SONOTECH INC.
Sonotech, Inc. (Sonotech), of Atlanta, GA, the developer of the Cello® pulse combustion burner, claims that its burner system can be beneficial to a variety of combustion processes. The system incorporates a combustor that can be tuned to induce large amplitude sonic pulsation...
A practical approach in porous medium combustion for domestic application: A review
NASA Astrophysics Data System (ADS)
Ismail, A. K.; Ibrahim, N. H.; Shamsuddin, K. A.; Abdullah, M. Z.; Zubair, M.
2018-05-01
Combustion in porous media has been widely studied. Many application involving the combustion of porous media has been reported in various way with most consider on numerical works and industrial application. Besides, recent application of porous medium combustion for domestic is the topic of interest among researchers. In this paper, a review was conducted on the combustion of porous media in term of practical application for domestic consumers. Details on the type of fuel used including bio fuel and their system have been search thoroughly. Most of the system have utilized compressed air system to provide lean combustion in domestic application. Some self-aspirating system of porous medium burner was also reported. The application of new technology such as cogeneration by using thermoelectric cells in tandem with porous medium combustion is also revised according to recent work which have already been published. Besides, the recent advances which include coating of porous material is also considered at the end of this paper.
Tripropellant combustion process
NASA Technical Reports Server (NTRS)
Kmiec, T. D.; Carroll, R. G.
1988-01-01
The addition of small amounts of hydrogen to the combustion of LOX/hydrocarbon propellants in large rocket booster engines has the potential to enhance the system stability. Programs being conducted to evaluate the effects of hydrogen on the combustion of LOX/hydrocarbon propellants at supercritical pressures are described. Combustion instability has been a problem during the development of large hydrocarbon fueled rocket engines. At the higher combustion chamber pressures expected for the next generation of booster engines, the effect of unstable combustion could be even more destructive. The tripropellant engine cycle takes advantage of the superior cooling characteristics of hydrogen to cool the combustion chamber and a small amount of the hydrogen coolant can be used in the combustion process to enhance the system stability. Three aspects of work that will be accomplished to evaluate tripropellant combustion are described. The first is laboratory demonstration of the benefits through the evaluation of drop size, ignition delay and burning rate. The second is analytical modeling of the combustion process using the empirical relationship determined in the laboratory. The third is a subscale demonstration in which the system stability will be evaluated. The approach for each aspect is described and the analytical models that will be used are presented.
Detection and control of combustion instability based on the concept of dynamical system theory.
Gotoda, Hiroshi; Shinoda, Yuta; Kobayashi, Masaki; Okuno, Yuta; Tachibana, Shigeru
2014-02-01
We propose an online method of detecting combustion instability based on the concept of dynamical system theory, including the characterization of the dynamic behavior of combustion instability. As an important case study relevant to combustion instability encountered in fundamental and practical combustion systems, we deal with the combustion dynamics close to lean blowout (LBO) in a premixed gas-turbine model combustor. The relatively regular pressure fluctuations generated by thermoacoustic oscillations transit to low-dimensional intermittent chaos owing to the intermittent appearance of burst with decreasing equivalence ratio. The translation error, which is characterized by quantifying the degree of parallelism of trajectories in the phase space, can be used as a control variable to prevent LBO.
System and method for reducing combustion dynamics in a combustor
Uhm, Jong Ho; Ziminsky, Willy Steve; Johnson, Thomas Edward; Srinivasan, Shiva; York, William David
2016-11-29
A system for reducing combustion dynamics in a combustor includes an end cap that extends radially across the combustor and includes an upstream surface axially separated from a downstream surface. A combustion chamber is downstream of the end cap, and tubes extend from the upstream surface through the downstream surface. Each tube provides fluid communication through the end cap to the combustion chamber. The system further includes means for reducing combustion dynamics in the combustor. A method for reducing combustion dynamics in a combustor includes flowing a working fluid through tubes that extend axially through an end cap that extends radially across the combustor and obstructing at least a portion of the working fluid flowing through a first set of the tubes.
Combustion process for synthesis of carbon nanomaterials from liquid hydrocarbon
Diener, Michael D.; Alford, J. Michael; Nabity, James; Hitch, Bradley D.
2007-01-02
The present invention provides a combustion apparatus for the production of carbon nanomaterials including fullerenes and fullerenic soot. Most generally the combustion apparatus comprises one or more inlets for introducing an oxygen-containing gas and a hydrocarbon fuel gas in the combustion system such that a flame can be established from the mixed gases, a droplet delivery apparatus for introducing droplets of a liquid hydrocarbon feedstock into the flame, and a collector apparatus for collecting condensable products containing carbon nanomaterials that are generated in the combustion system. The combustion system optionally has a reaction zone downstream of the flame. If this reaction zone is present the hydrocarbon feedstock can be introduced into the flame, the reaction zone or both.
Detection and control of combustion instability based on the concept of dynamical system theory
NASA Astrophysics Data System (ADS)
Gotoda, Hiroshi; Shinoda, Yuta; Kobayashi, Masaki; Okuno, Yuta; Tachibana, Shigeru
2014-02-01
We propose an online method of detecting combustion instability based on the concept of dynamical system theory, including the characterization of the dynamic behavior of combustion instability. As an important case study relevant to combustion instability encountered in fundamental and practical combustion systems, we deal with the combustion dynamics close to lean blowout (LBO) in a premixed gas-turbine model combustor. The relatively regular pressure fluctuations generated by thermoacoustic oscillations transit to low-dimensional intermittent chaos owing to the intermittent appearance of burst with decreasing equivalence ratio. The translation error, which is characterized by quantifying the degree of parallelism of trajectories in the phase space, can be used as a control variable to prevent LBO.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Yang, Li-Ping, E-mail: yangliping302@hrbeu.edu.cn; Ding, Shun-Liang; Song, En-Zhe
The cycling combustion instabilities in a diesel engine have been analyzed based on chaos theory. The objective was to investigate the dynamical characteristics of combustion in diesel engine. In this study, experiments were performed under the entire operating range of a diesel engine (the engine speed was changed from 600 to 1400 rpm and the engine load rate was from 0% to 100%), and acquired real-time series of in-cylinder combustion pressure using a piezoelectric transducer installed on the cylinder head. Several methods were applied to identify and quantitatively analyze the combustion process complexity in the diesel engine including delay-coordinate embedding, recurrencemore » plot (RP), Recurrence Quantification Analysis, correlation dimension (CD), and the largest Lyapunov exponent (LLE) estimation. The results show that the combustion process exhibits some determinism. If LLE is positive, then the combustion system has a fractal dimension and CD is no more than 1.6 and within the diesel engine operating range. We have concluded that the combustion system of diesel engine is a low-dimensional chaotic system and the maximum values of CD and LLE occur at the lowest engine speed and load. This means that combustion system is more complex and sensitive to initial conditions and that poor combustion quality leads to the decrease of fuel economy and the increase of exhaust emissions.« less
Yang, Li-Ping; Ding, Shun-Liang; Litak, Grzegorz; Song, En-Zhe; Ma, Xiu-Zhen
2015-01-01
The cycling combustion instabilities in a diesel engine have been analyzed based on chaos theory. The objective was to investigate the dynamical characteristics of combustion in diesel engine. In this study, experiments were performed under the entire operating range of a diesel engine (the engine speed was changed from 600 to 1400 rpm and the engine load rate was from 0% to 100%), and acquired real-time series of in-cylinder combustion pressure using a piezoelectric transducer installed on the cylinder head. Several methods were applied to identify and quantitatively analyze the combustion process complexity in the diesel engine including delay-coordinate embedding, recurrence plot (RP), Recurrence Quantification Analysis, correlation dimension (CD), and the largest Lyapunov exponent (LLE) estimation. The results show that the combustion process exhibits some determinism. If LLE is positive, then the combustion system has a fractal dimension and CD is no more than 1.6 and within the diesel engine operating range. We have concluded that the combustion system of diesel engine is a low-dimensional chaotic system and the maximum values of CD and LLE occur at the lowest engine speed and load. This means that combustion system is more complex and sensitive to initial conditions and that poor combustion quality leads to the decrease of fuel economy and the increase of exhaust emissions.
A/E/C CAD Standard, Release 5.0
2012-12-01
System Control Panels Halon System Inert Gas Smoke/Pressurization Control Egress Requirements Fire Protection System Appendix A ... System Natural Gas System Miter Gates Makeup Air System Appendix A Model File Level/Layer Assignment Tables A54 Discipline: Mechanical Model...SWITCHES Element type: Symbol Electrical: STP14B SURFACE 1X4 STRIP BATTERY Element type: Symbol Electrical: SUBST A
Study of aircraft in intraurban transportation systems. Volume 4: Appendix
NASA Technical Reports Server (NTRS)
Stout, E. G.; Kesling, P. H.; Matteson, H. C.; Sherwood, D. E.; Tuck, W. R., Jr.; Vaughn, L. A.
1971-01-01
An appendix of the supporting data leading to conclusions and recommendations for an effective intraurban transportation system from volumes 1, 2, and 3 is presented. The data are given in tables and graphs.
Laser-GMA Hybrid Pipe Welding System
2007-11-01
Experimental Results.................................................................................................34 Autogenous Laser Welds...APPENDIX B. Training Manual – Overview of System Components and Software...................... APPENDIX C. NASSCO...17. Autogenous laser welds in different joint configurations (10 mm thick mild steel, 5 mm land
40 CFR Appendix B to Part 122 - [Reserved
Code of Federal Regulations, 2010 CFR
2010-07-01
... 40 Protection of Environment 21 2010-07-01 2010-07-01 false [Reserved] B Appendix B to Part 122 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) WATER PROGRAMS EPA ADMINISTERED PERMIT PROGRAMS: THE NATIONAL POLLUTANT DISCHARGE ELIMINATION SYSTEM Appendix B to Part 122 [Reserved] ...
40 CFR Appendix B to Part 122 - [Reserved
Code of Federal Regulations, 2011 CFR
2011-07-01
... 40 Protection of Environment 22 2011-07-01 2011-07-01 false [Reserved] B Appendix B to Part 122 Protection of Environment ENVIRONMENTAL PROTECTION AGENCY (CONTINUED) WATER PROGRAMS EPA ADMINISTERED PERMIT PROGRAMS: THE NATIONAL POLLUTANT DISCHARGE ELIMINATION SYSTEM Appendix B to Part 122 [Reserved] ...
NASA Astrophysics Data System (ADS)
Mizumoto, Ikuro; Tsunematsu, Junpei; Fujii, Seiya
2016-09-01
In this paper, a design method of an output feedback control system with a simple feedforward input for a combustion model of diesel engine will be proposed based on the almost strictly positive real-ness (ASPR-ness) of the controlled system for a combustion control of diesel engines. A parallel feedforward compensator (PFC) design scheme which renders the resulting augmented controlled system ASPR will also be proposed in order to design a stable output feedback control system for the considered combustion model. The effectiveness of our proposed method will be confirmed through numerical simulations.
Electrically heated particulate filter propagation support methods and systems
Gonze, Eugene V [Pinckney, MI; Ament, Frank [Troy, MI
2011-06-07
A control system that controls regeneration of a particulate filter is provided. The system generally includes a regeneration module that controls current to the particulate filter to initiate combustion of particulate matter in the particulate filter. A propagation module estimates a propagation status of the combustion of the particulate matter based on a combustion temperature. A temperature adjustment module controls the combustion temperature by selectively increasing a temperature of exhaust that passes through the particulate filter.
Code of Federal Regulations, 2012 CFR
2012-07-01
... the system at the base of the main sprinkler riser. l. Fire hydrants must be located within 250 feet... Suppression System(s) 1. General. This Appendix B contains information on the Fire-safety Detection and Suppression System(s) tested by NARA through independent live fire testing that are certified to meet the...
Code of Federal Regulations, 2014 CFR
2014-07-01
... the system at the base of the main sprinkler riser. l. Fire hydrants must be located within 250 feet... Suppression System(s) 1. General. This Appendix B contains information on the Fire-safety Detection and Suppression System(s) tested by NARA through independent live fire testing that are certified to meet the...
Code of Federal Regulations, 2013 CFR
2013-07-01
... the system at the base of the main sprinkler riser. l. Fire hydrants must be located within 250 feet... Suppression System(s) 1. General. This Appendix B contains information on the Fire-safety Detection and Suppression System(s) tested by NARA through independent live fire testing that are certified to meet the...
Code of Federal Regulations, 2013 CFR
2013-07-01
... 40 Protection of Environment 9 2013-07-01 2013-07-01 false Am I exempt from any 40 CFR part 60... Emission Monitoring § 62.15190 Am I exempt from any 40 CFR part 60 appendix B or appendix F requirements to... emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission...
Code of Federal Regulations, 2012 CFR
2012-07-01
... 40 Protection of Environment 9 2012-07-01 2012-07-01 false Am I exempt from any 40 CFR part 60... Emission Monitoring § 62.15190 Am I exempt from any 40 CFR part 60 appendix B or appendix F requirements to... emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission...
Code of Federal Regulations, 2014 CFR
2014-07-01
... 40 Protection of Environment 9 2014-07-01 2014-07-01 false Am I exempt from any 40 CFR part 60... Emission Monitoring § 62.15190 Am I exempt from any 40 CFR part 60 appendix B or appendix F requirements to... emission monitoring system require you to also evaluate your oxygen (or carbon dioxide) continuous emission...
Process Synchronization and Data Communication between Processes in Real Time Local Area Networks.
1985-12-01
52 APPENDIX A: PROCEDURE MAKETABLE .............. 54 APPENDIX B: PROCEDURE MAKEMESSAGE ............. 56 APPENDIX C: PROCEDURE...item. The relation table is built by the driver during system initialization by the procedure maketable , see Appendix A. This procedure reads the file... MAKETABLE Procedure maketable is the first procedure called by the driver. It sets up the relation table in local RAM of SBC 1 by reading the information
JANNAF 37th Combustion Subcommittee Meeting. Volume 1
NASA Technical Reports Server (NTRS)
Fry, Ronald S. (Editor); Gannaway, Mary T. (Editor)
2000-01-01
This volume, the first of two volumes is a compilation of 59 unclassified/unlimited-distribution technical papers presented at the Joint Army-Navy-NASA-Air Force (JANNAF) 37th Combustion Subcommittee (CS) meeting held jointly with the 25th Airbreathing Propulsion Subcommittee (APS), 19th Propulsion Systems Hazards Subcommittee (PSHS), and 1st Modeling and Simulation Subcommittee (MSS) meetings. The meeting was held 13-17 November 2000 at the Naval Postgraduate School and Hyatt Regency Hotel, Monterey, California. Topics covered at the CS meeting include: a keynote address on the Future Combat Systems, and review of a new JANNAF Modeling and Simulation Subcommittee, and technical papers on gun propellant burning rate, gun tube erosion, advanced gun propulsion concepts, ETC guns, novel gun propellants; liquid, hybrid and novel propellant combustion; solid propellant combustion kinetics, GAP, ADN and RDX combustion, sandwich combustion, metal combustion, combustion instability, and motor combustion instability.
Kraemer, Gilbert Otto; Varatharajan, Balachandar; Evulet, Andrei Tristan; Yilmaz, Ertan; Lacy, Benjamin Paul
2013-12-31
Methods and systems are provided for premixing combustion fuel and air within gas turbines. In one embodiment, a combustor includes an upstream mixing panel configured to direct compressed air and combustion fuel through premixing zone to form a fuel-air mixture. The combustor includes a downstream mixing panel configured to mix additional combustion fuel with the fule-air mixture to form a combustion mixture.
Hybrid lean premixing catalytic combustion system for gas turbines
Critchley, Ian L.
2003-12-09
A system and method of combusting a hydrocarbon fuel is disclosed. The system combines the accuracy and controllability of an air staging system with the ultra-low emissions achieved by catalytic combustion systems without the need for a pre-heater. The result is a system and method that is mechanically simple and offers ultra-low emissions over a wide range of power levels, fuel properties and ambient operating conditions.
Pulsation-based method for reduction of nitrogen oxides content in torch combustion products
NASA Astrophysics Data System (ADS)
Berg, I. A.; Porshnev, S. V.; Oshchepkova, V. Y.; Kit, M.
2018-01-01
Out of all ways to fuel bum the torch combustion systems is used most often. Even though the processes in the steam boiler are stochastic, the system can be controlled rather easily by changing the flowrate of the air pumped into it and - in case of balanced flue units - exhausters load. Advantages offered by torch-based combustion systems are offset by a disadvantage resulted in oxidation of nitrogen contained in the air. This paper provides rationale for an NOx content reduction method that employs pulsation mode of fuel combustion; it also describes combustion control and monitoring system employed for implementation of this method. Described methodology can be used not only for pulsation combustion studies but also for studies of torches formed by conventional burning systems. The outcome of the experimental study supports the assumption that it is possible to create conditions for NOx content reduction in flue gases by means of cycling the fuel supply on/off valve at the rate of 6 Hz.
Oxy-fuel combustion with integrated pollution control
Patrick, Brian R [Chicago, IL; Ochs, Thomas Lilburn [Albany, OR; Summers, Cathy Ann [Albany, OR; Oryshchyn, Danylo B [Philomath, OR; Turner, Paul Chandler [Independence, OR
2012-01-03
An oxygen fueled integrated pollutant removal and combustion system includes a combustion system and an integrated pollutant removal system. The combustion system includes a furnace having at least one burner that is configured to substantially prevent the introduction of air. An oxygen supply supplies oxygen at a predetermine purity greater than 21 percent and a carbon based fuel supply supplies a carbon based fuel. Oxygen and fuel are fed into the furnace in controlled proportion to each other and combustion is controlled to produce a flame temperature in excess of 3000 degrees F. and a flue gas stream containing CO2 and other gases. The flue gas stream is substantially void of non-fuel borne nitrogen containing combustion produced gaseous compounds. The integrated pollutant removal system includes at least one direct contact heat exchanger for bringing the flue gas into intimated contact with a cooling liquid to produce a pollutant-laden liquid stream and a stripped flue gas stream and at least one compressor for receiving and compressing the stripped flue gas stream.
Critical areas: Satellite power systems concepts
NASA Technical Reports Server (NTRS)
1975-01-01
Critical Areas are defined and discussed in the various areas pertinent to satellite power systems. The presentation is grouped into five areas (General, Space Systems, Solar Energy Conversion, Microwave Systems, and Environment/Ecology) with a sixth area (Power Relay) considered separately in an appendix. Areas for Future Consideration as critical areas are discussed in a second appendix.
14 CFR Appendix D to Part 417 - Flight Termination Systems, Components, Installation, and Monitoring
Code of Federal Regulations, 2013 CFR
2013-01-01
... other propulsion system. D417.5Flight termination system design (a) Reliability prediction. A flight... design margin required by this appendix. As an alternative to subjecting the flight termination system to... the component is heated or cooled to achieve the required dwell time at one extreme of the required...
14 CFR Appendix D to Part 417 - Flight Termination Systems, Components, Installation, and Monitoring
Code of Federal Regulations, 2011 CFR
2011-01-01
... other propulsion system. D417.5Flight termination system design (a) Reliability prediction. A flight... design margin required by this appendix. As an alternative to subjecting the flight termination system to... the component is heated or cooled to achieve the required dwell time at one extreme of the required...
14 CFR Appendix D to Part 417 - Flight Termination Systems, Components, Installation, and Monitoring
Code of Federal Regulations, 2012 CFR
2012-01-01
... other propulsion system. D417.5Flight termination system design (a) Reliability prediction. A flight... design margin required by this appendix. As an alternative to subjecting the flight termination system to... the component is heated or cooled to achieve the required dwell time at one extreme of the required...
14 CFR Appendix D to Part 417 - Flight Termination Systems, Components, Installation, and Monitoring
Code of Federal Regulations, 2014 CFR
2014-01-01
... other propulsion system. D417.5Flight termination system design (a) Reliability prediction. A flight... design margin required by this appendix. As an alternative to subjecting the flight termination system to... the component is heated or cooled to achieve the required dwell time at one extreme of the required...
Code of Federal Regulations, 2010 CFR
2010-07-01
... Emission Measurement Systems This appendix describes a series of correlation criteria that EPA considers to... results from each system. (b) Correlation criteria for particulate measurements. (1) The correlation... system (i.e., avgalt/avgspc) should be between 0.97 and 1.05. (c) Correlation criteria for other...
Code of Federal Regulations, 2011 CFR
2011-07-01
... Emission Measurement Systems This appendix describes a series of correlation criteria that EPA considers to... results from each system. (b) Correlation criteria for particulate measurements. (1) The correlation... system (i.e., avgalt/avgspc) should be between 0.97 and 1.05. (c) Correlation criteria for other...
Army Corps of Engineers: Water Resource Authorizations, Appropriations, and Activities
2014-07-01
Assistance Authorities ........................................................................... 11 Appendixes Appendix. Evolution of the Its...projects (e.g., municipal water and wastewater treatment systems) and other nontraditional activities. The Appendix provides more on the evolution of...feasibility by the Secretary of the Army.13 10 General Robert B. Flowers , Army Corps
Pathways for School Finance in California. Technical Appendix
ERIC Educational Resources Information Center
Rose, Heather; Sonstelie, Jon; Weston, Margaret
2010-01-01
This is a technical appendix for the report, "Pathways for School Finance in California" (ED515651). "Pathways for School Finance in California" simulates alternatives to California's current school finance system. This appendix provides more information about the revenues used in those simulations. The first section describes…
Genie Inference Engine Rule Writer’s Guide.
1987-08-01
33 APPENDIX D. Animal Bootstrap File.............................................................. 39...APPENDIX E. Sample Run of Animal Identification Expert System.......................... 43 APPENDIX F. Numeric Test Knowledge Base...and other data s.tructures stored in the knowledge base (KB), queries the user for input, and draws conclusions. Genie (GENeric Inference Engine) is
DOE Office of Scientific and Technical Information (OSTI.GOV)
NONE
This study, conducted by Black & Veatch, was funded by the U.S. Trade and Development Agency. The report presents a technical and commercial analysis for the development of three nearly identical electricity generating facilities (biomass steam power plants) in the towns of Chachoengsao, Suphan Buri, and Pichit in Thailand. The Main Report is divided into the following sections: (1.0) Executive Study; (2.0) Project Objectives; (3.0) Review of Combustion Technology for Biomass Fueled Steam Generator Units; (4.0) Conceptual Design; (5.0) Plant Descriptions; (6.0) Plant Operations Staffing; (7.0) Project Schedule; (8.0) Project Cost Estimate; (9.0) Financial Analysis; Appendix - Financial Analysis.
JANNAF 35th Combustion Subcommittee Meeting. Volume 1
NASA Technical Reports Server (NTRS)
Fry, Ronald S. (Editor); Gannaway, Mary T. (Editor); Rognan, Melanie (Editor)
1998-01-01
Volume 1, the first of two volumes is a compilation of 63 unclassified/unlimited distribution technical papers presented at the 35th meeting of the Joint Army-Navy-NASA-Air Force (JANNAF) Combustion Subcommittee (CS) held jointly with the 17th Propulsion Systems Hazards Subcommittee (PSHS) and Airbreathing Propulsion Subcommittee (APS). The meeting was held on 7-11 December 1998 at Raytheon Systems Company and the Marriott Hotel, Tucson, AZ. Topics covered include solid gun propellant processing, ignition and combustion, charge concepts, barrel erosion and flash, gun interior ballistics, kinetics and molecular modeling, ETC gun modeling, simulation and diagnostics, and liquid gun propellant combustion; solid rocket motor propellant combustion, combustion instability fundamentals, motor instability, and measurement techniques; and liquid and hybrid rocket combustion.
Analysis of pressure spectra measurements in a ducted combustion system. Ph.D. Thesis - Toledo Univ.
NASA Technical Reports Server (NTRS)
Miles, J. H.
1980-01-01
Combustion noise propagation in an operating ducted liquid fuel combustion system is studied in relation to the development of combustion noise prediction and suppression techniques. The presence of combustor emissions in the duct is proposed as the primary mechanism producing the attenuation and dispersion of combustion noise propagating in an operating liquid fuel combustion system. First, a complex mathematical model for calculating attenuation and dispersion taking into account mass transfer, heat transfer, and viscosity effects due to the presence of liquid fuel droplets or solid soot particles is discussed. Next, a simpler single parameter model for calculating pressure auto-spectra and cross-spectra which takes into account dispersion and attenuation due to heat transfer between solid soot particles and air is developed. Then, auto-spectra and cross-spectra obtained from internal pressure measurements in a combustion system consisting of a J-47 combustor can, a spool piece, and a long duct are presented. Last, analytical results obtained with the single parameter model are compared with the experimental measurements. The single parameter model results are shown to be in excellent agreement with the measurements.
Analysis of pressure spectra measurements in a ducted combustion system
NASA Astrophysics Data System (ADS)
Miles, J. H.
1980-11-01
Combustion noise propagation in an operating ducted liquid fuel combustion system is studied in relation to the development of combustion noise prediction and suppression techniques. The presence of combustor emissions in the duct is proposed as the primary mechanism producing the attenuation and dispersion of combustion noise propagating in an operating liquid fuel combustion system. First, a complex mathematical model for calculating attenuation and dispersion taking into account mass transfer, heat transfer, and viscosity effects due to the presence of liquid fuel droplets or solid soot particles is discussed. Next, a simpler single parameter model for calculating pressure auto-spectra and cross-spectra which takes into account dispersion and attenuation due to heat transfer between solid soot particles and air is developed. Then, auto-spectra and cross-spectra obtained from internal pressure measurements in a combustion system consisting of a J-47 combustor can, a spool piece, and a long duct are presented. Last, analytical results obtained with the single parameter model are compared with the experimental measurements. The single parameter model results are shown to be in excellent agreement with the measurements.
NASA Astrophysics Data System (ADS)
Ispas, N.; Cofaru, C.; Aleonte, M.
2017-10-01
Internal combustion engines still play a major role in today transportation but increasing the fuel efficiency and decreasing chemical emissions remain a great goal of the researchers. Direct injection and air assisted injection system can improve combustion and can reduce the concentration of the exhaust gas pollutes. Advanced air-to-fuel and combustion air-to-fuel injection system for mixtures, derivatives and alcohol gasoline blends represent a major asset in reducing pollutant emissions and controlling combustion processes in spark-ignition engines. The use of these biofuel and biofuel blending systems for gasoline results in better control of spark ignition engine processes, making combustion as complete as possible, as well as lower levels of concentrations of pollutants in exhaust gases. The main purpose of this paper was to provide most suitable tools for ensure the proven increase in the efficiency of spark ignition engines, making them more environmentally friendly. The conclusions of the paper allow to highlight the paths leading to a better use of alcohols (biofuels) in internal combustion engines of modern transport units.
14 CFR Appendix B to Part 135 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2013 CFR
2013-01-01
... 14 Aeronautics and Space 3 2013-01-01 2013-01-01 false Airplane Flight Recorder Specifications B Appendix B to Part 135 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION.... B Appendix B to Part 135—Airplane Flight Recorder Specifications Parameters Range Installed system 1...
12 CFR Appendix A to Part 630 - Supplemental Information Disclosure Guidelines
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 7 2013-01-01 2013-01-01 false Supplemental Information Disclosure Guidelines A Appendix A to Part 630 Banks and Banking FARM CREDIT ADMINISTRATION FARM CREDIT SYSTEM DISCLOSURE..., App. A Appendix A to Part 630—Supplemental Information Disclosure Guidelines Supplemental information...
12 CFR Appendix A to Part 630 - Supplemental Information Disclosure Guidelines
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 6 2011-01-01 2011-01-01 false Supplemental Information Disclosure Guidelines A Appendix A to Part 630 Banks and Banking FARM CREDIT ADMINISTRATION FARM CREDIT SYSTEM DISCLOSURE..., App. A Appendix A to Part 630—Supplemental Information Disclosure Guidelines Supplemental information...
12 CFR Appendix A to Part 630 - Supplemental Information Disclosure Guidelines
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 7 2014-01-01 2014-01-01 false Supplemental Information Disclosure Guidelines A Appendix A to Part 630 Banks and Banking FARM CREDIT ADMINISTRATION FARM CREDIT SYSTEM DISCLOSURE..., App. A Appendix A to Part 630—Supplemental Information Disclosure Guidelines Supplemental information...
12 CFR Appendix A to Part 630 - Supplemental Information Disclosure Guidelines
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 7 2012-01-01 2012-01-01 false Supplemental Information Disclosure Guidelines A Appendix A to Part 630 Banks and Banking FARM CREDIT ADMINISTRATION FARM CREDIT SYSTEM DISCLOSURE..., App. A Appendix A to Part 630—Supplemental Information Disclosure Guidelines Supplemental information...
33 CFR Appendix B to Part 187 - Participating and Certified Titling Authorities
Code of Federal Regulations, 2010 CFR
2010-07-01
... 33 Navigation and Navigable Waters 2 2010-07-01 2010-07-01 false Participating and Certified Titling Authorities B Appendix B to Part 187 Navigation and Navigable Waters COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) BOATING SAFETY VESSEL IDENTIFICATION SYSTEM Pt. 187, App. B Appendix B to...
1988-09-01
20 SLIM . . . . .e & . . . . . . . . . . . . 24 SoftCost-R . . . . . . . . . . . . . . . 26 SPQR /20 . . . . . . . . . . .*. . . . . 28...PRICB-8 . . . . . . . . . . .. . 83 softCost-R ............. 84 SPQR /20 . . . . . . . . . . . . 0 . 84 System-3 . . . . . . . . . . . . . . 85 Summry...128 Appendix G: SoftCost-R Input Values . . . . . . . . . . 129 Appendix H: SoftCost-R Resources Estimate . . . . . . . 131 Appendix I: SPQR
14 CFR Appendix B to Part 135 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2014 CFR
2014-01-01
... 14 Aeronautics and Space 3 2014-01-01 2014-01-01 false Airplane Flight Recorder Specifications B Appendix B to Part 135 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION.... B Appendix B to Part 135—Airplane Flight Recorder Specifications Parameters Range Installed system 1...
14 CFR Appendix E to Part 91 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2013 CFR
2013-01-01
... 14 Aeronautics and Space 2 2013-01-01 2013-01-01 false Airplane Flight Recorder Specifications E Appendix E to Part 91 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION... Appendix E to Part 91—Airplane Flight Recorder Specifications Parameters Range Installed system 1 minimum...
14 CFR Appendix E to Part 91 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2014 CFR
2014-01-01
... 14 Aeronautics and Space 2 2014-01-01 2014-01-01 false Airplane Flight Recorder Specifications E Appendix E to Part 91 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION... Appendix E to Part 91—Airplane Flight Recorder Specifications Parameters Range Installed system 1 minimum...
14 CFR Appendix B to Part 135 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 3 2011-01-01 2011-01-01 false Airplane Flight Recorder Specifications B Appendix B to Part 135 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION.... B Appendix B to Part 135—Airplane Flight Recorder Specifications Parameters Range Installed system 1...
14 CFR Appendix E to Part 91 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 2 2011-01-01 2011-01-01 false Airplane Flight Recorder Specifications E Appendix E to Part 91 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION... Appendix E to Part 91—Airplane Flight Recorder Specifications Parameters Range Installed system 1 minimum...
14 CFR Appendix B to Part 135 - Airplane Flight Recorder Specifications
Code of Federal Regulations, 2012 CFR
2012-01-01
... 14 Aeronautics and Space 3 2012-01-01 2012-01-01 false Airplane Flight Recorder Specifications B Appendix B to Part 135 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION.... B Appendix B to Part 135—Airplane Flight Recorder Specifications Parameters Range Installed system 1...
14 CFR Appendix C to Part 135 - Helicopter Flight Recorder Specifications
Code of Federal Regulations, 2014 CFR
2014-01-01
... 14 Aeronautics and Space 3 2014-01-01 2014-01-01 false Helicopter Flight Recorder Specifications C Appendix C to Part 135 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION.... C Appendix C to Part 135—Helicopter Flight Recorder Specifications Parameters Range Installed system...
DOE Office of Scientific and Technical Information (OSTI.GOV)
O'Neil, Lori Ross; Conway, T. J.; Tobey, D. H.
The Secure Power Systems Professional Phase III final report was released last year which an appendix of Job Profiles. This new report is that appendix broken out as a standalone document to assist utilities in recruiting and developing Secure Power Systems Professionals at their site.
32 CFR Appendix H to Part 323 - DLA Exemption Rules
Code of Federal Regulations, 2012 CFR
2012-07-01
... PROGRAM DEFENSE LOGISTICS AGENCY PRIVACY PROGRAM Pt. 323, App. H Appendix H to Part 323—DLA Exemption Rules Exempted Records Systems. All systems of records maintained by the Defense Logistics Agency will.... b. ID: S500.20 (Specific exemption). 1. System name: Defense Logistics Agency Criminal Incident...
Code of Federal Regulations, 2010 CFR
2010-01-01
... Quality Management Systems for Flight Simulation Training Devices E Appendix E to Part 60 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIRMEN FLIGHT SIMULATION...—Qualification Performance Standards for Quality Management Systems for Flight Simulation Training Devices Begin...
40 CFR Appendix Viii to Part 85 - Vehicle and Engine Parameters and Specifications
Code of Federal Regulations, 2014 CFR
2014-07-01
...) AIR PROGRAMS (CONTINUED) CONTROL OF AIR POLLUTION FROM MOBILE SOURCES Pt. 85, App. VIII Appendix VIII.... Air Inlet System. 1. Temperature control system calibration. IV. Fuel System. 1. General. a. Engine idle speed. b. Engine idle mixture. 2. Carburetion. a. Air-fuel flow calibration. b. Transient...
40 CFR Appendix Viii to Part 85 - Vehicle and Engine Parameters and Specifications
Code of Federal Regulations, 2013 CFR
2013-07-01
...) AIR PROGRAMS (CONTINUED) CONTROL OF AIR POLLUTION FROM MOBILE SOURCES Pt. 85, App. VIII Appendix VIII.... Air Inlet System. 1. Temperature control system calibration. IV. Fuel System. 1. General. a. Engine idle speed. b. Engine idle mixture. 2. Carburetion. a. Air-fuel flow calibration. b. Transient...
40 CFR Appendix Viii to Part 85 - Vehicle and Engine Parameters and Specifications
Code of Federal Regulations, 2012 CFR
2012-07-01
...) AIR PROGRAMS (CONTINUED) CONTROL OF AIR POLLUTION FROM MOBILE SOURCES Pt. 85, App. VIII Appendix VIII.... Air Inlet System. 1. Temperature control system calibration. IV. Fuel System. 1. General. a. Engine idle speed. b. Engine idle mixture. 2. Carburetion. a. Air-fuel flow calibration. b. Transient...
Large liquid rocket engine transient performance simulation system
NASA Technical Reports Server (NTRS)
Mason, J. R.; Southwick, R. D.
1989-01-01
Phase 1 of the Rocket Engine Transient Simulation (ROCETS) program consists of seven technical tasks: architecture; system requirements; component and submodel requirements; submodel implementation; component implementation; submodel testing and verification; and subsystem testing and verification. These tasks were completed. Phase 2 of ROCETS consists of two technical tasks: Technology Test Bed Engine (TTBE) model data generation; and system testing verification. During this period specific coding of the system processors was begun and the engineering representations of Phase 1 were expanded to produce a simple model of the TTBE. As the code was completed, some minor modifications to the system architecture centering on the global variable common, GLOBVAR, were necessary to increase processor efficiency. The engineering modules completed during Phase 2 are listed: INJTOO - main injector; MCHBOO - main chamber; NOZLOO - nozzle thrust calculations; PBRNOO - preburner; PIPE02 - compressible flow without inertia; PUMPOO - polytropic pump; ROTROO - rotor torque balance/speed derivative; and TURBOO - turbine. Detailed documentation of these modules is in the Appendix. In addition to the engineering modules, several submodules were also completed. These submodules include combustion properties, component performance characteristics (maps), and specific utilities. Specific coding was begun on the system configuration processor. All functions necessary for multiple module operation were completed but the SOLVER implementation is still under development. This system, the Verification Checkout Facility (VCF) allows interactive comparison of module results to store data as well as provides an intermediate checkout of the processor code. After validation using the VCF, the engineering modules and submodules were used to build a simple TTBE.
Experimental study of combustion in hydrogen peroxide hybrid rockets
NASA Astrophysics Data System (ADS)
Wernimont, Eric John
Combustion behavior in a hydrogen peroxide oxidized hybrid rocket motor is investigated with a series of experiments. Hybrid chemical rocket propulsion is presently of interest due to reduced system complexity compared to classical chemical propulsion systems. Reduced system complexity, by use of a storable oxidizer and a hybrid configuration, is expected to reduce propulsive costs. The fuel in this study is polyethylene which has the potential of continuous manufacture leading to further reduced system costs. The study investigated parameters of interest for nominal design of a full scale hydrogen peroxide oxidized hybrid rocket. Amongst these parameters is the influence of chamber pressure, mass flux, fuel molecular weight and fuel density on fuel regression rate. Effects of chamber pressure and aft combustion length on combustion efficiency and non-acoustic combustion oscillations are also examined. The fuel regression behavior is found to be strongly influenced by both chamber pressure and mass flux. Combustion efficiencies in the upper 90% range are attained by simple changes to the aft combustion chamber length as well as increased combustion pressure. Fuel burning surface is found to be influenced by the density of the polyethylene polymer as well as molecular weight. The combustion is observed to be exceptionally smooth (oscillations less than 5% zero-to-peak of mean) in all motors tested in this program. Tests using both a single port fuel gain and a novel radial flow hybrid are also performed.
Reducing mode circulating fluid bed combustion
Lin, Yung-Yi; Sadhukhan, Pasupati; Fraley, Lowell D.; Hsiao, Keh-Hsien
1986-01-01
A method for combustion of sulfur-containing fuel in a circulating fluid bed combustion system wherein the fuel is burned in a primary combustion zone under reducing conditions and sulfur captured as alkaline sulfide. The reducing gas formed is oxidized to combustion gas which is then separated from solids containing alkaline sulfide. The separated solids are then oxidized and recycled to the primary combustion zone.
Slag processing system for direct coal-fired gas turbines
Pillsbury, Paul W.
1990-01-01
Direct coal-fired gas turbine systems and methods for their operation are provided by this invention. The systems include a primary combustion compartment coupled to an impact separator for removing molten slag from hot combustion gases. Quenching means are provided for solidifying the molten slag removed by the impact separator, and processing means are provided forming a slurry from the solidified slag for facilitating removal of the solidified slag from the system. The released hot combustion gases, substantially free of molten slag, are then ducted to a lean combustion compartment and then to an expander section of a gas turbine.
Combustion-gas recirculation system
Baldwin, Darryl Dean
2007-10-09
A combustion-gas recirculation system has a mixing chamber with a mixing-chamber inlet and a mixing-chamber outlet. The combustion-gas recirculation system may further include a duct connected to the mixing-chamber inlet. Additionally, the combustion-gas recirculation system may include an open inlet channel with a solid outer wall. The open inlet channel may extend into the mixing chamber such that an end of the open inlet channel is disposed between the mixing-chamber inlet and the mixing-chamber outlet. Furthermore, air within the open inlet channel may be at a pressure near or below atmospheric pressure.
Code of Federal Regulations, 2010 CFR
2010-04-01
... as Parts of the Interstate System B Appendix B to Subpart A of Part 470 Highways FEDERAL HIGHWAY ADMINISTRATION, DEPARTMENT OF TRANSPORTATION PLANNING AND RESEARCH HIGHWAY SYSTEMS Federal-aid Highway Systems Pt...) Corridors as Parts of the Interstate System The following guidance is comparable to current procedures for...
20 CFR 404.1525 - Listing of Impairments in appendix 1.
Code of Federal Regulations, 2011 CFR
2011-04-01
... Impairments (the listings) is in appendix 1 of this subpart. It describes for each of the major body systems... relationship with their counterparts in part A. (c) How do we use the listings? (1) Each body system section in... introduction to each body system contains information relevant to the use of the listings in that body system...
49 CFR Appendix I to Part 1201 - Certification of Branch Line Accounting System Records
Code of Federal Regulations, 2010 CFR
2010-10-01
... 49 Transportation 9 2010-10-01 2010-10-01 false Certification of Branch Line Accounting System... RAILROAD COMPANIES Pt. 1201, App. I Appendix I to Part 1201—Certification of Branch Line Accounting System...__ the branch line accounting system data were collected and maintained for each line that met the...
Updating the conceptual model for fine particle mass emissions from combustion systems.
Robinson, Allen L; Grieshop, Andrew P; Donahue, Neil M; Hunt, Sherri W
2010-10-01
Atmospheric transformations determine the contribution of emissions from combustion systems to fine particulate matter (PM) mass. For example, combustion systems emit vapors that condense onto existing particles or form new particles as the emissions are cooled and diluted. Upon entering the atmosphere, emissions are exposed to atmospheric oxidants and sunlight, which causes them to evolve chemically and physically, generating secondary PM. This review discusses these transformations, focusing on organic PM. Organic PM emissions are semi-volatile at atmospheric conditions and thus their partitioning varies continuously with changing temperature and concentration. Because organics contribute a large portion of the PM mass emitted by most combustion sources, these emissions cannot be represented using a traditional, static emission factor. Instead, knowledge of the volatility distribution of emissions is required to explicitly account for changes in gas-particle partitioning. This requires updating how PM emissions from combustion systems are measured and simulated from combustion systems. Secondary PM production often greatly exceeds the direct or primary PM emissions; therefore, secondary PM must be included in any assessment of the contribution of combustion systems to ambient PM concentrations. Low-volatility organic vapors emitted by combustion systems appear to be very important secondary PM precursors that are poorly accounted for in inventories and models. The review concludes by discussing the implications that the dynamic nature of these PM emissions have on source testing for emission inventory development and regulatory purposes. This discussion highlights important linkages between primary and secondary PM, which could lead to simplified certification test procedures while capturing the emission components that contribute most to atmospheric PM mass.
Robinson, Allen L; Grieshop, Andrew P; Donahue, Neil M; Hunt, Sherri W
2010-10-01
Atmospheric transformations determine the contribution of emissions from combustion systems to fine particulate matter (PM) mass. For example, combustion systems emit vapors that condense onto existing particles or form new particles as the emissions are cooled and diluted. Upon entering the atmosphere, emissions are exposed to atmospheric oxidants and sunlight, which causes them to evolve chemically and physically, generating secondary PM. This review discusses these transformations, focusing on organic PM. Organic PM emissions are semi -volatile at atmospheric conditions and thus their partitioning varies continuously with changing temperature and concentration. Because organics contribute a large portion of the PM mass emitted by most combustion sources, these emissions cannot be represented using a traditional, static emission factor. Instead, knowledge of the volatility distribution of emissions is required to explicitly account for changes in gas-particle partitioning. This requires updating how PM emissions from combustion systems are measured and simulated from combustion systems. Secondary PM production often greatly exceeds the direct or primary PM emissions; therefore, secondary PM must be included in any assessment of the contribution of combustion systems to ambient PM concentrations. Low-volatility organic vapors emitted by combustion systems appear to be very important secondary PM precursors that are poorly accounted for in inventories and models. The review concludes by discussing the implications that the dynamic nature of these PM emissions have on source testing for emission inventory development and regulatory purposes. This discussion highlights important linkages between primary and secondary PM, which could lead to simplified certification test procedures while capturing the emission components that contribute most to atmospheric PM mass.
Diagnostics in Japan's microgravity experiments
NASA Technical Reports Server (NTRS)
Kadota, Toshikazu
1995-01-01
The achievement of the combustion research under microgravity depends substantially on the availability of diagnostic systems. The non-intrusive diagnostic systems are potentially applicable for providing the accurate, realistic and detailed information on momentum, mass and energy transport, complex gas phase chemistry, and phase change in the combustion field under microgravity. The non-intrusive nature of optical instruments is essential to the measurement of combustion process under microgravity which is very nervous to any perturbation. However, the implementation of the non-intrusive combustion diagnostic systems under microgravity is accompanied by several constraints. Usually, a very limited space is only available for constructing a highly sophisticated system which is so sensitive that it is easily affected by the magnitude of the gravitational force, vibration and heterogeneous field of temperature and density of the environments. The system should be properly adjusted prior to the experiment. Generally, it is quite difficult to tune the instruments during measurements. The programmed sequence of operation should also be provided. Extensive effort has been toward the development of non-intrusive diagnostic systems available for the combustion experiments under microgravity. This paper aims to describe the current art and the future strategy on the non-intrusive diagnostic systems potentially applicable to the combustion experiments under microgravity in Japan.
Exhaust heated hydrogen and oxygen producing catalytic converter for combustion engine
DOE Office of Scientific and Technical Information (OSTI.GOV)
Schreiber, E.T.
1977-07-26
A steam generator is provided in operative association with a source of water and the exhaust system of a combustion engine including an air induction system provided with primary fuel inlet structure and supplemental fuel inlet structure. The steam generator derives its heat for converting water into steam from the exhaust system of the combustion engine and the steam generator includes a steam outlet communicated with and opening into one end of an elongated tubular housing disposed in good heat transfer relation with the exhaust system of the combustion engine and having a gas outlet at its other end communicatedmore » with the supplemental fuel inlet of the induction system. The tubular housing has iron filings disposed therein and is in such heat transfer relation with the exhaust system of the combustion engine so as to elevate the temperature of steam passing therethrough and to heat the iron filings to the extent that passage of the heated steam over the heated filings will result in hydrogen and oxygen gas being produced in the tubular housing for subsequent passage to the supplemental fuel inlet of the combustion engine induction system.« less
30 CFR 250.1630 - Safety-system testing and records.
Code of Federal Regulations, 2013 CFR
2013-07-01
... conditions warrant. Testing must be in accordance with API RP 14C, Appendix D (as incorporated by reference in § 250.198). For safety system devices other than those listed in API RP 14C, Appendix D, you must...
30 CFR 250.1630 - Safety-system testing and records.
Code of Federal Regulations, 2012 CFR
2012-07-01
... conditions warrant. Testing must be in accordance with API RP 14C, Appendix D (as incorporated by reference in § 250.198). For safety system devices other than those listed in API RP 14C, Appendix D, you must...
30 CFR 250.1630 - Safety-system testing and records.
Code of Federal Regulations, 2014 CFR
2014-07-01
... conditions warrant. Testing must be in accordance with API RP 14C, Appendix D (as incorporated by reference in § 250.198). For safety system devices other than those listed in API RP 14C, Appendix D, you must...
CO-FIRING COAL: FEEDLOT AND LITTER BIOMASS FUELS
DOE Office of Scientific and Technical Information (OSTI.GOV)
Unknown
2002-07-01
Proposed activities for quarter 8 (3/15/2001--6/14/2002), Boiler Burner Simulation and Experiments: (1) Continue the parametric study of cofiring of pulverized coal and LB in the boiler burner, and determining the combustor performance and emissions of NO, CO, CO{sub 2}, PO{sub 2} and P{sub 4}O{sub 10}, etc. The air-fuel ratio, swirl number of the secondary air stream and moisture effects will also be investigated (Task 4). Gasification: (Task 3) (2) Measuring the temperature profile for chicken litter biomass under different operating conditions. (3) Product gas species for different operating conditions for different fuels. (4) Determining the bed ash composition for differentmore » fuels. (5) Determining the gasification efficiency for different operating conditions. Activities Achieved during quarter 8 (3/15/2001--6/14/2002), Boiler Burner Simulation and Experiments: (1) The evaporation and phosphorus combustion models have been incorporated into the PCGC-2 code. Mr. Wei has successfully defended his Ph.D. proposal on Coal: LB modeling studies (Task 4, Appendix C). (2) Reburn experiments with both low and high phosphorus feedlot biomass has been performed (Task 2, Appendix A). (3) Parametric studies on the effect of air-fuel ratio, swirl number of the secondary air stream and moisture effects have been investigated (Task 2, Appendix A). (4) Three abstracts have been submitted to the American Society of Agricultural Engineers Annual International meeting at Chicago in July 2002. Three part paper dealing with fuel properties, cofiring, large scale testing are still under review in the Journal of Fuel. Gasification: (Task 3, Appendix B) (5) Items No. 2, and 3 are 95% complete, with four more experiments yet to be performed with coal and chicken litter biomass blends. (6) Item No. 4, and 5 shall be performed after completion of all the experiments.« less
Tropic Test of Bradley Fighting Vehicle Systems.
1985-05-23
CM-R AMSTE-SG-H AMSTE-PT-MT AMSTE-RM Aberden Proving Ground , MD 21005-5055 Commander U.S. Army Armament Research and Development Command ATTN: AMSMC...Requirements Appendix E -Vision Devices Appendix F - Grounding Circuit Resistance Appendix G - Human Factors Appendix H - Distribution List -" -"" 3...miles of operation o Time-on-Target Baseline Tests o Selected electrical and grounding circuit resistances o Armament Firing (25mm, 7.62mm and TOW) o Fire
Computer presentation of data in science.
NASA Astrophysics Data System (ADS)
Simmonds, D.; Reynolds, L.
Contents: How this book was created. Foreword. 1. Introduction. 2. Choosing your system and software. 3. Working methods. 4. Preparing manuscripts and camera-ready copy. 5. Principles of typography and layout. 6. Using type and space to show the structure of text. 7. Artwork creation and drawing tips. 8. Posters, slides and OHP transparencies. 9. Designing with colour. Glossaries 1 and 2. Appendix 1: Copyfitting. Appendix 2: Signatures and imposition. Appendix 3: Publishing and the law. Appendix 4: Working comfort.
APTI (Air Pollution Training Institute) Course 427: combustion evaluation, student manual
DOE Office of Scientific and Technical Information (OSTI.GOV)
Beard, J.T.; Iachetta, F.A.; Lilleleht, L.U.
1980-02-01
This Student Manual is used in conjunction with Course No. 427, 'Combustion Evaluation' as applied to air pollution control situations. This manual was prepared by the EPA Air Pollution Training Institute (APTI) to supplement the course lecture materials and to present detailed reference information on the following topics: combustion fundamentals, fuel properties, combustion system design, pollutant emission evaluations, combustion control, gas, oil, and coal burning, solid waste and wood burning, incineration of wastes, sewage sludge incineration, waste gas flares, hazardous waste combustion, NOx control, and improved combustion systems. Note: There is also an Instructor's Guide to be used in conductingmore » the training course - (EPA-450/2-80-065) and a Student Workbook to be used for homework and in-class problem solving - (EPA-450/2-80-64).« less
Numerical modelling of biomass combustion: Solid conversion processes in a fixed bed furnace
NASA Astrophysics Data System (ADS)
Karim, Md. Rezwanul; Naser, Jamal
2017-06-01
Increasing demand for energy and rising concerns over global warming has urged the use of renewable energy sources to carry a sustainable development of the world. Bio mass is a renewable energy which has become an important fuel to produce thermal energy or electricity. It is an eco-friendly source of energy as it reduces carbon dioxide emissions. Combustion of solid biomass is a complex phenomenon due to its large varieties and physical structures. Among various systems, fixed bed combustion is the most commonly used technique for thermal conversion of solid biomass. But inadequate knowledge on complex solid conversion processes has limited the development of such combustion system. Numerical modelling of this combustion system has some advantages over experimental analysis. Many important system parameters (e.g. temperature, density, solid fraction) can be estimated inside the entire domain under different working conditions. In this work, a complete numerical model is used for solid conversion processes of biomass combustion in a fixed bed furnace. The combustion system is divided in to solid and gas phase. This model includes several sub models to characterize the solid phase of the combustion with several variables. User defined subroutines are used to introduce solid phase variables in commercial CFD code. Gas phase of combustion is resolved using built-in module of CFD code. Heat transfer model is modified to predict the temperature of solid and gas phases with special radiation heat transfer solution for considering the high absorptivity of the medium. Considering all solid conversion processes the solid phase variables are evaluated. Results obtained are discussed with reference from an experimental burner.
14 CFR Appendix B to Part 1215 - Factors Affecting Standard Charges
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 5 2011-01-01 2010-01-01 true Factors Affecting Standard Charges B Appendix B to Part 1215 Aeronautics and Space NATIONAL AERONAUTICS AND SPACE ADMINISTRATION TRACKING AND DATA RELAY SATELLITE SYSTEM (TDRSS) Pt. 1215, App. B Appendix B to Part 1215—Factors Affecting Standard...
Code of Federal Regulations, 2013 CFR
2013-07-01
... for Federal Travel [Traveler Identification] C Appendix C to Chapter 301 Public Contracts and Property Management Federal Travel Regulation System TEMPORARY DUTY (TDY) TRAVEL ALLOWANCES Ch. 301, App. C Appendix C to Chapter 301—Standard Data Elements for Federal Travel [Traveler Identification] Group name Data...
12 CFR Appendix D to Part 230 - Issuance of Staff Interpretations
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 3 2010-01-01 2010-01-01 false Issuance of Staff Interpretations D Appendix D... RESERVE SYSTEM TRUTH IN SAVINGS (REGULATION DD) Pt. 230, App. D Appendix D to Part 230—Issuance of Staff... official staff interpretations of this part. These interpretations provide the protections afforded under...
12 CFR Appendix D to Part 230 - Issuance of Staff Interpretations
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 3 2011-01-01 2011-01-01 false Issuance of Staff Interpretations D Appendix D... RESERVE SYSTEM TRUTH IN SAVINGS (REGULATION DD) Pt. 230, App. D Appendix D to Part 230—Issuance of Staff... official staff interpretations of this part. These interpretations provide the protections afforded under...
41 CFR Appendix D to Chapter 301 - Glossary of Acronyms
Code of Federal Regulations, 2010 CFR
2010-07-01
... 41 Public Contracts and Property Management 4 2010-07-01 2010-07-01 false Glossary of Acronyms D Appendix D to Chapter 301 Public Contracts and Property Management Federal Travel Regulation System TEMPORARY DUTY (TDY) TRAVEL ALLOWANCES Ch. 301, App. D Appendix D to Chapter 301—Glossary of Acronyms ATM...
40 CFR 51.214 - Continuous emission monitoring.
Code of Federal Regulations, 2010 CFR
2010-07-01
... information as specified in appendix P of this part. (b) The procedures must— (1) Identify the types of... the types of sources set forth in appendix P of this part to meet the applicable requirements set... systems and other reports and records required by appendix P of this part. (e) The procedures must require...
14 CFR Appendix I to Part 25 - Installation of an Automatic Takeoff Thrust Control System (ATTCS)
Code of Federal Regulations, 2010 CFR
2010-01-01
...) This appendix specifies additional requirements for installation of an engine power control system that... crew to increase thrust or power. I25.2Definitions. (a) Automatic Takeoff Thrust Control System (ATTCS... mechanical and electrical, that sense engine failure, transmit signals, actuate fuel controls or power levers...
Code of Federal Regulations, 2010 CFR
2010-04-01
... 23 Highways 1 2010-04-01 2010-04-01 false Additional Required Contract Provisions, Appalachian Development Highway System and Local Access Roads Contracts Other Than Construction Contracts C Appendix C to..., Appalachian Development Highway System and Local Access Roads Contracts Other Than Construction Contracts...
Jiao, Penghao; Li, Zhijun; Li, Qiang; Zhang, Wen; He, Li; Wu, Yue
2018-07-01
In the coupled Diesel Oxidation Catalyst (DOC) and Diesel Particular Filter (DPF) system, soot cannot be completely removed by only using the passive regeneration. And DPF active regeneration is necessary. The research method in this paper is to spray different kinds of combustion-supporting agents to the DOC in the front of the DPF. Therefore, the low temperature combustion mechanism of different kinds of combustion-supporting agents in DOC was studied, in order to grasp the law of combustion in DOC, and the influence of follow-up emission on DPF removal of soot. During the study, CH 4 H 2 mixture and diesel (n-heptane + toluene) were used as combustion-supporting agents respectively. The simplified mechanisms of two kinds of gas mixtures used as the combustion-supporting agents in DPF have been constructed and testified in the paper. In this paper, the combustion and emission conditions of the two combustion-supporting agents were analyzed so as to meet the practical requirements of different working conditions. Copyright © 2017 ISA. Published by Elsevier Ltd. All rights reserved.
NASA Technical Reports Server (NTRS)
Bartrand, Timothy A.
1988-01-01
During the shutdown of the space shuttle main engine, oxygen flow is shut off from the fuel preburner and helium is used to push the residual oxygen into the combustion chamber. During this process a low frequency combustion instability, or chug, occurs. This chug has resulted in damage to the engine's augmented spark igniter due to backflow of the contents of the preburner combustion chamber into the oxidizer feed system. To determine possible causes and fixes for the chug, the fuel preburner was modeled as a heterogeneous stirred tank combustion chamber, a variable mass flow rate oxidizer feed system, a constant mass flow rate fuel feed system and an exit turbine. Within the combustion chamber gases were assumed perfectly mixed. To account for liquid in the combustion chamber, a uniform droplet distribution was assumed to exist in the chamber, with mean droplet diameter determined from an empirical relation. A computer program was written to integrate the resulting differential equations. Because chamber contents were assumed perfectly mixed, the fuel preburner model erroneously predicted that combustion would not take place during shutdown. The combustion rate model was modified to assume that all liquid oxygen that vaporized instantaneously combusted with fuel. Using this combustion model, the effect of engine parameters on chamber pressure oscillations during the SSME shutdown was calculated.
Early distinction system of mine fire in underground by using a neural-network system
DOE Office of Scientific and Technical Information (OSTI.GOV)
Ohga, Kotaro; Higuchi, Kiyoshi
1996-12-31
In our laboratory, a new detection system using smell detectors was developed to detect the spontaneous combustion of coal and the combustion of other materials used underground. The results of experiments clearly the combustion of materials can be detected earlier by this detection system than by conventional detectors for gas and smoke, and there were significant differences between output data from each smell detector for coal, rubber, oil and wood. In order to discern the source of combustion gases, we have been developing a distinction system using a neural-network system. It has shown successful results in laboratory tests. This papermore » describes our detection system using smell detectors and our distinction system which uses a neural-network system, and presents results of experiments using both systems.« less
Fuel injection device and method
Carlson, L.W.
1983-12-21
A fuel injection system and method provide for shaping a combustion plume within a combustion chamber to effectively recirculate hot combustion gases for stable combustion conditions while providing symmetrical combustion conditions. Char and molten slag are passed to the outer boundary layer to complete combustion of char while permitting initial substoichiometric combustion in a reductive atmosphere for reducing discharge of nitrogen oxides. Shaping of the plume is accomplished by an axially adjustable pintle which permits apportionment of driving pressure between elements which contribute tangential and those which contribute radial directional components to oxidant flow entering the combustion chamber.
Fuel injection device and method
Carlson, Larry W.
1986-01-01
A fuel injection system and method provide for shaping a combustion plume within a combustion chamber to effectively recirculate hot combustion gases for stable combustion conditions while providing symmetrical combustion conditions. Char and molten slag are passed to the outer boundary layer to complete combustion of char while permitting initial substoichiometric combustion in a reductive atmosphere for reducing discharge of nitrogen oxides. Shaping of the plume is accomplished by an axially adjustable pintle which permits apportionment of driving pressure between elements which contribute tangential and those which contribute radial directional components to oxidant flow entering the combustion chamber.
Fuel injection device and method
Carlson, Larry W.
1986-02-04
A fuel injection system and method provide for shaping a combustion plume within a combustion chamber to effectively recirculate hot combustion gases for stable combustion conditions while providing symmetrical combustion conditions. Char and molten slag are passed to the outer boundary layer to complete combustion of char while permitting initial substoichiometric combustion in a reductive atmosphere for reducing discharge of nitrogen oxides. Shaping of the plume is accomplished by an axially adjustable pintle which permits apportionment of driving pressure between elements which contribute tangential and those which contribute radial directional components to oxidant flow entering the combustion chamber.
Porteiro, Jacobo; Riveiro, Belén; Granada, Enrique; Armesto, Julia; Eguía, Pablo; Collazo, Joaquín
2011-01-01
This paper describes a prototype instrumentation system for photogrammetric measuring of bed and ash layers, as well as for flying particle detection and pursuit using a single device (CCD) web camera. The system was designed to obtain images of the combustion process in the interior of a domestic boiler. It includes a cooling system, needed because of the high temperatures in the combustion chamber of the boiler. The cooling system was designed using CFD simulations to ensure effectiveness. This method allows more complete and real-time monitoring of the combustion process taking place inside a boiler. The information gained from this system may facilitate the optimisation of boiler processes. PMID:22319349
Porteiro, Jacobo; Riveiro, Belén; Granada, Enrique; Armesto, Julia; Eguía, Pablo; Collazo, Joaquín
2011-01-01
This paper describes a prototype instrumentation system for photogrammetric measuring of bed and ash layers, as well as for flying particle detection and pursuit using a single device (CCD) web camera. The system was designed to obtain images of the combustion process in the interior of a domestic boiler. It includes a cooling system, needed because of the high temperatures in the combustion chamber of the boiler. The cooling system was designed using CFD simulations to ensure effectiveness. This method allows more complete and real-time monitoring of the combustion process taking place inside a boiler. The information gained from this system may facilitate the optimisation of boiler processes.
An innovative system for supplying air and fuel mixture to a combustion chamber of an engine
NASA Astrophysics Data System (ADS)
Saikumar, G. R. Bharath
2018-04-01
Conventional carburetors are being used since decades to ensure that the desired ratio of air and fuel enters the combustion chamber for combustion for the purpose of generating power in an Spark Ignition(SI) internal combustion engine. However to increase the efficiency, the carburetor system is gradually being replaced by fuel injection systems. Fuel injection systems use injectors to supply pressurized fuel into the combustion chamber. Owing to the high initial and maintenance cost, carburetors are still ruling in the low cost vehicle domain. An innovative concept is conceived, which is an alternative method to the carburetor system to supply the air and fuel mixture to a combustion chamber of an engine. This system comprises of an inner hollow cylinder with minute holes drilled along its length with an outer cylinder capable of sliding along its length or its longitudinal axis. This system is placed in the venturi instead of the conventional carburetor system. Fuel enters from the bottom inlet of the inner cylinder and flows out through the holes provided along its length. The fuel flow from the inner cylinder is dependent on the size and the number of holes exposed at that instance by the sliding outer cylinder which in turn is connected to the throttle or accelerator.
Automatic calibration and control system for a combined oxygen and combustibles analyzer
DOE Office of Scientific and Technical Information (OSTI.GOV)
Woolbert, G.D.; Jewett, S.Y.; Robertson, J.W. Jr.
1989-08-01
This patent describes an automatic, periodically calibrating system for continuous output of calibrated signals from a combined oxygen and combustibles analyzer. It comprises: a combined oxygen and combustibles analyzer for sensing a level of oxygen and a level of combustibles in a volatile atmosphere and for producing a first sample signal indicative of the oxygen level and a second sample signal indicative of the combustibles level; means for introducing zero and span calibration test gases into the analyzer; means for periodically calibrating the analyzer. This including: a data control unit; a timer unit; a mechanical unit, means for calculating zeromore » and span values for oxygen and combustibles, means for comparing the calculated zero and span values for oxygen and combustibles to the preset alarm limits for oxygen and combustibles, means for activating an operator alarm, means for calculating oxygen and combustibles drift adjustments, a memory unit; and means for applying the oxygen and combustibles drift adjustments concurrently to the first and second sample signals, according to predetermined mathematical relationship, to obtain calibrated output signals indicative of the oxygen and combustibles level in the volatile atmosphere.« less
DOE Office of Scientific and Technical Information (OSTI.GOV)
Marriott, Craig; Gonzalez, Manual; Russell, Durrett
2011-06-30
This report summarizes activities related to the revised STATEMENT OF PROJECT OBJECTIVES (SOPO) dated June 2010 for the Development of High-Efficiency Clean Combustion engine Designs for Spark-Ignition and Compression-Ignition Internal Combustion Engines (COOPERATIVE AGREEMENT NUMBER DE-FC26-05NT42415) project. In both the spark- (SI) and compression-ignition (CI) development activities covered in this program, the goal was to develop potential production-viable internal combustion engine system technologies that both reduce fuel consumption and simultaneously met exhaust emission targets. To be production-viable, engine technologies were also evaluated to determine if they would meet customer expectations of refinement in terms of noise, vibration, performance, driveability, etc.more » in addition to having an attractive business case and value. Prior to this activity, only proprietary theoretical / laboratory knowledge existed on the combustion technologies explored The research reported here expands and develops this knowledge to determine series-production viability. Significant SI and CI engine development occurred during this program within General Motors, LLC over more than five years. In the SI program, several engines were designed and developed that used both a relatively simple multi-lift valve train system and a Fully Flexible Valve Actuation (FFVA) system to enable a Homogeneous Charge Compression Ignition (HCCI) combustion process. Many technical challenges, which were unknown at the start of this program, were identified and systematically resolved through analysis, test and development. This report documents the challenges and solutions for each SOPO deliverable. As a result of the project activities, the production viability of the developed clean combustion technologies has been determined. At this time, HCCI combustion for SI engines is not considered production-viable for several reasons. HCCI combustion is excessively sensitive to control variables such as internal dilution level and charge temperature. As a result, HCCI combustion has limited robustness when variables exceed the required narrow ranges determined in this program. HCCI combustion is also not available for the entire range of production engine speeds and loads, (i.e., the dynamic range is limited). Thus, regular SI combustion must be employed for a majority of the full dynamic range of the engine. This degrades the potential fuel economy impact of HCCI combustion. Currently-available combustion control actuators for the simple valve train system engine do not have the authority for continuous air - fuel or torque control for managing the combustion mode transitions between SI and HCCI and thus, require further refinement to meet customer refinement expectations. HCCI combustion control sensors require further development to enable robust long-term HCCI combustion control. Finally, the added technologies required to effectively manage HCCI combustion such as electric cam phasers, central direct fuel injection, cylinder pressure sensing, high-flow exhaust gas recirculation system, etc. add excessive on-engine cost and complexity that erodes the production-viability business« less
Code of Federal Regulations, 2014 CFR
2014-07-01
... Notice in Federal Register Format E Appendix E to Part 310 National Defense Department of Defense... Format (See paragraph (f) of § 310.30) New system of records notice DEPARTMENT OF DEFENSE Office of the..., Department of Defense. NSLRB 01 System name: The National Security Labor Relations Board (NSLRB). System...
Code of Federal Regulations, 2014 CFR
2014-07-01
... Personal Fall Protection Systems (Non-Mandatory) B Appendix B to Subpart I of Part 1915 Labor Regulations... Guidelines for Personal Fall Protection Systems (Non-Mandatory) 1. Personal fall arrest systems—(a) General... create the free fall distance should be the one supplied with the system, or in its absence, the least...
Code of Federal Regulations, 2012 CFR
2012-07-01
... Personal Fall Protection Systems (Non-Mandatory) B Appendix B to Subpart I of Part 1915 Labor Regulations... Guidelines for Personal Fall Protection Systems (Non-Mandatory) 1. Personal fall arrest systems—(a) General... create the free fall distance should be the one supplied with the system, or in its absence, the least...
Code of Federal Regulations, 2013 CFR
2013-07-01
... Personal Fall Protection Systems (Non-Mandatory) B Appendix B to Subpart I of Part 1915 Labor Regulations... Guidelines for Personal Fall Protection Systems (Non-Mandatory) 1. Personal fall arrest systems—(a) General... create the free fall distance should be the one supplied with the system, or in its absence, the least...
Code of Federal Regulations, 2012 CFR
2012-04-01
... 23 Highways 1 2012-04-01 2012-04-01 false Guidance Criteria for Evaluating Requests for Modifications to the National Highway System D Appendix D to Subpart A of Part 470 Highways FEDERAL HIGHWAY ADMINISTRATION, DEPARTMENT OF TRANSPORTATION PLANNING AND RESEARCH HIGHWAY SYSTEMS Federal-aid Highway Systems Pt...
Code of Federal Regulations, 2013 CFR
2013-04-01
... 23 Highways 1 2013-04-01 2013-04-01 false Guidance Criteria for Evaluating Requests for Modifications to the National Highway System D Appendix D to Subpart A of Part 470 Highways FEDERAL HIGHWAY ADMINISTRATION, DEPARTMENT OF TRANSPORTATION PLANNING AND RESEARCH HIGHWAY SYSTEMS Federal-aid Highway Systems Pt...
Code of Federal Regulations, 2014 CFR
2014-04-01
... 23 Highways 1 2014-04-01 2014-04-01 false Guidance Criteria for Evaluating Requests for Modifications to the National Highway System D Appendix D to Subpart A of Part 470 Highways FEDERAL HIGHWAY ADMINISTRATION, DEPARTMENT OF TRANSPORTATION PLANNING AND RESEARCH HIGHWAY SYSTEMS Federal-aid Highway Systems Pt...
Lean, Premixed-Prevaporized (LPP) combustor conceptual design study
NASA Technical Reports Server (NTRS)
Dickman, R. A.; Dodds, W. J.; Ekstedt, E. E.
1979-01-01
Four combustion systems were designed and sized for the energy efficient engine. A fifth combustor was designed for the cycle and envelope of the twin-spool, high bypass ratio, high pressure ratio turbofan engine. Emission levels, combustion performance, life, and reliability assessments were made for these five combustion systems. Results of these design studies indicate that cruise NOx emission can be reduced by the use of lean, premixed-prevaporaized combustion and airflow modulation.
Flame Suppression Agent, System and Uses
NASA Technical Reports Server (NTRS)
Parrish, Clyde F. (Inventor)
2013-01-01
Aqueous droplets encapsulated in a flame retardant polymer are useful in suppressing combustion. Upon exposure to a flame, the encapsulated aqueous droplets rupture and vaporize, removing heat and displacing oxygen to retard the combustion process. The polymer encapsulant, through decomposition, may further add free radicals to the combustion atmosphere, thereby further retarding the combustion process. The encapsulated aqueous droplets may be used as a replacement to halon, water mist and dry powder flame suppression systems.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Mays, S.E.; Poloski, J.P.; Sullivan, W.H.
1982-07-01
This report describes a risk study of the Browns Ferry, Unit 1, nuclear plant. The study is one of four such studies sponsored by the NRC Office of Research, Division of Risk Assessment, as part of its Interim Reliability Evaluation Program (IREP), Phase II. This report is contained in four volumes: a main report and three appendixes. Appendix B provides a description of Browns Ferry, Unit 1, plant systems and the failure evaluation of those systems as they apply to accidents at Browns Ferry. Information is presented concerning front-line system fault analysis; support system fault analysis; human error models andmore » probabilities; and generic control circuit analyses.« less
NASA Astrophysics Data System (ADS)
Virgen, Matthew Miguel
Two significant goals in solar plant operation are lower cost and higher efficiencies. To achieve those goals, a combined cycle gas turbine (CCGT) system, which uses the hot gas turbine exhaust to produce superheated steam for a bottoming Rankine cycle by way of a heat recovery steam generator (HRSG), is investigated in this work. Building off of a previous gas turbine model created at the Combustion and Solar Energy Laboratory at SDSU, here are added the HRSG and steam turbine model, which had to handle significant change in the mass flow and temperature of air exiting the gas turbine due to varying solar input. A wide range of cases were run to explore options for maximizing both power and efficiency from the proposed CSP CCGT plant. Variable guide vanes (VGVs) were found in the earlier model to be an effective tool in providing operational flexibility to address the variable nature of solar input. Combined cycle efficiencies in the range of 50% were found to result from this plant configuration. However, a combustor inlet temperature (CIT) limit leads to two distinct Modes of operation, with a sharp drop in both plant efficiency and power occurring when the air flow through the receiver exceeded the CIT limit. This drawback can be partially addressed through strategic use of the VGVs. Since system response is fully established for the relevant range of solar input and variable guide vane angles, the System Advisor Model (SAM) from NREL can be used to find what the actual expected solar input would be over the course of the day, and plan accordingly. While the SAM software is not yet equipped to model a Brayton cycle cavity receiver, appropriate approximations were made in order to produce a suitable heliostat field to fit this system. Since the SPHER uses carbon nano-particles as the solar absorbers, questions of particle longevity and how the particles might affect the flame behavior in the combustor were addressed using the chemical kinetics software ChemkinPro by modeling the combustion characteristics both with and without the particles. This work is presented in the Appendix.
Combustion Fundamentals Research
NASA Technical Reports Server (NTRS)
1983-01-01
Increased emphasis is placed on fundamental and generic research at Lewis Research Center with less systems development efforts. This is especially true in combustion research, where the study of combustion fundamentals has grown significantly in order to better address the perceived long term technical needs of the aerospace industry. The main thrusts for this combustion fundamentals program area are as follows: analytical models of combustion processes, model verification experiments, fundamental combustion experiments, and advanced numeric techniques.
Flashback detection sensor for lean premix fuel nozzles
Thornton, Jimmy Dean [Morgantown, WV; Richards, George Alan [Morgantown, WV; Straub, Douglas L [Morgantown, WV; Liese, Eric Arnold [Morgantown, WV; Trader, Jr., John Lee; Fasching, George Edward [Morgantown, WV
2002-08-06
A sensor for detecting the flame occurring during a flashback condition in the fuel nozzle of a lean premix combustion system is presented. The sensor comprises an electrically isolated flashback detection electrode and a guard electrode, both of which generate electrical fields extending to the walls of the combustion chamber and to the walls of the fuel nozzle. The sensor is positioned on the fuel nozzle center body at a location proximate the entrance to the combustion chamber of the gas turbine combustion system. The sensor provides 360.degree. detection of a flashback inside the fuel nozzle, by detecting the current conducted by the flame within a time frame that will prevent damage to the gas turbine combustion system caused by the flashback condition.
Closed-loop system for growth of aquatic biomass and gasification thereof
Oyler, James R.
2017-09-19
Processes, systems, and methods for producing combustible gas from wet biomass are provided. In one aspect, for example, a process for generating a combustible gas from a wet biomass in a closed system is provided. Such a process may include growing a wet biomass in a growth chamber, moving at least a portion of the wet biomass to a reactor, heating the portion of the wet biomass under high pressure in the reactor to gasify the wet biomass into a total gas component, separating the gasified component into a liquid component, a non-combustible gas component, and a combustible gas component, and introducing the liquid component and non-combustible gas component containing carbon dioxide into the growth chamber to stimulate new wet biomass growth.
14 CFR Appendix D to Part 25 - Appendix D to Part 25
Code of Federal Regulations, 2014 CFR
2014-01-01
..., electronic controls, pressurization system controls, and engine controls. (2) The accessibility and... considered: (1) Flight path control. (2) Collision avoidance. (3) Navigation. (4) Communications. (5) Operation and monitoring of aircraft engines and systems. (6) Command decisions. (b) Workload factors. The...
14 CFR Appendix D to Part 25 - Appendix D to Part 25
Code of Federal Regulations, 2010 CFR
2010-01-01
..., electronic controls, pressurization system controls, and engine controls. (2) The accessibility and... considered: (1) Flight path control. (2) Collision avoidance. (3) Navigation. (4) Communications. (5) Operation and monitoring of aircraft engines and systems. (6) Command decisions. (b) Workload factors. The...
14 CFR Appendix D to Part 25 - Appendix D to Part 25
Code of Federal Regulations, 2011 CFR
2011-01-01
..., electronic controls, pressurization system controls, and engine controls. (2) The accessibility and... considered: (1) Flight path control. (2) Collision avoidance. (3) Navigation. (4) Communications. (5) Operation and monitoring of aircraft engines and systems. (6) Command decisions. (b) Workload factors. The...
14 CFR Appendix D to Part 25 - Appendix D to Part 25
Code of Federal Regulations, 2012 CFR
2012-01-01
..., electronic controls, pressurization system controls, and engine controls. (2) The accessibility and... considered: (1) Flight path control. (2) Collision avoidance. (3) Navigation. (4) Communications. (5) Operation and monitoring of aircraft engines and systems. (6) Command decisions. (b) Workload factors. The...
18 CFR 301.6 - Appendix 1 instructions.
Code of Federal Regulations, 2013 CFR
2013-04-01
..., DEPARTMENT OF ENERGY REGULATIONS FOR FEDERAL POWER MARKETING ADMINISTRATIONS AVERAGE SYSTEM COST METHODOLOGY... 4: Average System Cost (f) The filing Utility must reference and attach work papers, documentation... 18 Conservation of Power and Water Resources 1 2013-04-01 2013-04-01 false Appendix 1 instructions...
18 CFR 301.6 - Appendix 1 instructions.
Code of Federal Regulations, 2011 CFR
2011-04-01
..., DEPARTMENT OF ENERGY REGULATIONS FOR FEDERAL POWER MARKETING ADMINISTRATIONS AVERAGE SYSTEM COST METHODOLOGY... 4: Average System Cost (f) The filing Utility must reference and attach work papers, documentation... 18 Conservation of Power and Water Resources 1 2011-04-01 2011-04-01 false Appendix 1 instructions...
18 CFR 301.6 - Appendix 1 instructions.
Code of Federal Regulations, 2014 CFR
2014-04-01
..., DEPARTMENT OF ENERGY REGULATIONS FOR FEDERAL POWER MARKETING ADMINISTRATIONS AVERAGE SYSTEM COST METHODOLOGY... 4: Average System Cost (f) The filing Utility must reference and attach work papers, documentation... 18 Conservation of Power and Water Resources 1 2014-04-01 2014-04-01 false Appendix 1 instructions...
18 CFR 301.6 - Appendix 1 instructions.
Code of Federal Regulations, 2012 CFR
2012-04-01
..., DEPARTMENT OF ENERGY REGULATIONS FOR FEDERAL POWER MARKETING ADMINISTRATIONS AVERAGE SYSTEM COST METHODOLOGY... 4: Average System Cost (f) The filing Utility must reference and attach work papers, documentation... 18 Conservation of Power and Water Resources 1 2012-04-01 2012-04-01 false Appendix 1 instructions...
Flex Fuel Optimized SI and HCCI Engine
DOE Office of Scientific and Technical Information (OSTI.GOV)
Zhu, Guoming; Schock, Harold; Yang, Xiaojian
The central objective of the proposed work is to demonstrate an HCCI (homogeneous charge compression ignition) capable SI (spark ignited) engine that is capable of fast and smooth mode transition between SI and HCCI combustion modes. The model-based control technique was used to develop and validate the proposed control strategy for the fast and smooth combustion mode transition based upon the developed control-oriented engine; and an HCCI capable SI engine was designed and constructed using production ready two-step valve-train with electrical variable valve timing actuating system. Finally, smooth combustion mode transition was demonstrated on a metal engine within eight enginemore » cycles. The Chrysler turbocharged 2.0L I4 direct injection engine was selected as the base engine for the project and the engine was modified to fit the two-step valve with electrical variable valve timing actuating system. To develop the model-based control strategy for stable HCCI combustion and smooth combustion mode transition between SI and HCCI combustion, a control-oriented real-time engine model was developed and implemented into the MSU HIL (hardware-in-the-loop) simulation environment. The developed model was used to study the engine actuating system requirement for the smooth and fast combustion mode transition and to develop the proposed mode transition control strategy. Finally, a single cylinder optical engine was designed and fabricated for studying the HCCI combustion characteristics. Optical engine combustion tests were conducted in both SI and HCCI combustion modes and the test results were used to calibrate the developed control-oriented engine model. Intensive GT-Power simulations were conducted to determine the optimal valve lift (high and low) and the cam phasing range. Delphi was selected to be the supplier for the two-step valve-train and Denso to be the electrical variable valve timing system supplier. A test bench was constructed to develop control strategies for the electrical variable valve timing (VVT) actuating system and satisfactory electrical VVT responses were obtained. Target engine control system was designed and fabricated at MSU for both single-cylinder optical and multi-cylinder metal engines. Finally, the developed control-oriented engine model was successfully implemented into the HIL simulation environment. The Chrysler 2.0L I4 DI engine was modified to fit the two-step vale with electrical variable valve timing actuating system. A used prototype engine was used as the base engine and the cylinder head was modified for the two-step valve with electrical VVT actuating system. Engine validation tests indicated that cylinder #3 has very high blow-by and it cannot be reduced with new pistons and rings. Due to the time constraint, it was decided to convert the four-cylinder engine into a single cylinder engine by blocking both intake and exhaust ports of the unused cylinders. The model-based combustion mode transition control algorithm was developed in the MSU HIL simulation environment and the Simulink based control strategy was implemented into the target engine controller. With both single-cylinder metal engine and control strategy ready, stable HCCI combustion was achived with COV of 2.1% Motoring tests were conducted to validate the actuator transient operations including valve lift, electrical variable valve timing, electronic throttle, multiple spark and injection controls. After the actuator operations were confirmed, 15-cycle smooth combustion mode transition from SI to HCCI combustion was achieved; and fast 8-cycle smooth combustion mode transition followed. With a fast electrical variable valve timing actuator, the number of engine cycles required for mode transition can be reduced down to five. It was also found that the combustion mode transition is sensitive to the charge air and engine coolant temperatures and regulating the corresponding temperatures to the target levels during the combustion mode transition is the key for a smooth combustion mode transition. As a summary, the proposed combustion mode transition strategy using the hybrid combustion mode that starts with the SI combustion and ends with the HCCI combustion was experimentally validated on a metal engine. The proposed model-based control approach made it possible to complete the SI-HCCI combustion mode transition within eight engine cycles utilizing the well controlled hybrid combustion mode. Without intensive control-oriented engine modeling and HIL simulation study of using the hybrid combustion mode during the mode transition, it would be impossible to validate the proposed combustion mode transition strategy in a very short period.« less
APTI (Air Pollution Training Institute) course 427: combustion evaluation, instructor's guide
DOE Office of Scientific and Technical Information (OSTI.GOV)
Beard, J.T.; Iachetta, F.A.; Lilleleht, L.U.
1980-02-01
This Instructor's Guide is used in conjunction with Course No. 427, 'Combustion Evaluation' as applied to air pollution control situations. The teaching guide was prepared by the EPA Air Pollution Training Institute (APTI) to assist instructors in presenting course No. 427. The guide contains sections on the following topics: combustion fundamentals, fuel properties, combustion system design, pollutant emission calculations, combustion control, gas, oil, and burning, solid waste and wood burning, incineration of wastes, sewage sludge incineration, flame and catalytic incineration, waste gas flares, hazardous waste combustion, NOx control, improved combustion systems. Note: There is also a Student Workbook to bemore » used for homework and in-class problem solving (EPA-450/2-80-064) and a Student Manual for reference and additional subject material (EPA-450/2-80-063).« less
FY2017 Advanced Combustion Systems and Fuels Annual Progress Report
DOE Office of Scientific and Technical Information (OSTI.GOV)
None, None
The Advanced Combustion Systems and Fuels Program supports VTO’s goal and focuses early-stage research and development (R&D) to improve understanding of the combustion processes, fuel properties, and emission control technologies while generating knowledge and insight necessary for industry to develop the next generation of engines.
NETL- High-Pressure Combustion Research Facility
None
2018-02-14
NETL's High-Pressure Combustion Facility is a unique resource within the National Laboratories system. It provides the test capabilities needed to evaluate new combustion concepts for high-pressure, high-temperature hydrogen and natural gas turbines. These concepts will be critical for the next generation of ultra clean, ultra efficient power systems.
40 CFR Appendix Vii to Part 86 - Standard Bench Cycle (SBC)
Code of Federal Regulations, 2012 CFR
2012-07-01
.... VII Appendix VII to Part 86—Standard Bench Cycle (SBC) 1. The standard bench aging durability procedures [Ref. § 86.1823-08(d)] consist of aging a catalyst-oxygen-sensor system on an aging bench which follows the standard bench cycle (SBC) described in this appendix. 2. The SBC requires use of an aging...
40 CFR Appendix Vii to Part 86 - Standard Bench Cycle (SBC)
Code of Federal Regulations, 2013 CFR
2013-07-01
.... VII Appendix VII to Part 86—Standard Bench Cycle (SBC) 1. The standard bench aging durability procedures [Ref. § 86.1823-08(d)] consist of aging a catalyst-oxygen-sensor system on an aging bench which follows the standard bench cycle (SBC) described in this appendix. 2. The SBC requires use of an aging...
40 CFR Appendix A to Subpart Uuuuu - Hg Monitoring Provisions
Code of Federal Regulations, 2012 CFR
2012-07-01
... “cold standby” and may be reinstalled in the event of a primary monitoring system outage. A non... 40 Protection of Environment 15 2012-07-01 2012-07-01 false Hg Monitoring Provisions A Appendix A... Generating Units Pt. 63, Subpt. UUUUU, App. A Appendix A to Subpart UUUUU—Hg Monitoring Provisions 1. General...
14 CFR Appendix J to Part 23 - HIRF Environments and Equipment HIRF Test Levels
Code of Federal Regulations, 2012 CFR
2012-01-01
... 14 Aeronautics and Space 1 2012-01-01 2012-01-01 false HIRF Environments and Equipment HIRF Test.... 23, App. J Appendix J to Part 23—HIRF Environments and Equipment HIRF Test Levels This appendix specifies the HIRF environments and equipment HIRF test levels for electrical and electronic systems under...
14 CFR Appendix J to Part 23 - HIRF Environments and Equipment HIRF Test Levels
Code of Federal Regulations, 2011 CFR
2011-01-01
... 14 Aeronautics and Space 1 2011-01-01 2011-01-01 false HIRF Environments and Equipment HIRF Test.... 23, App. J Appendix J to Part 23—HIRF Environments and Equipment HIRF Test Levels This appendix specifies the HIRF environments and equipment HIRF test levels for electrical and electronic systems under...
14 CFR Appendix J to Part 23 - HIRF Environments and Equipment HIRF Test Levels
Code of Federal Regulations, 2013 CFR
2013-01-01
... 14 Aeronautics and Space 1 2013-01-01 2013-01-01 false HIRF Environments and Equipment HIRF Test.... 23, App. J Appendix J to Part 23—HIRF Environments and Equipment HIRF Test Levels This appendix specifies the HIRF environments and equipment HIRF test levels for electrical and electronic systems under...
14 CFR Appendix J to Part 23 - HIRF Environments and Equipment HIRF Test Levels
Code of Federal Regulations, 2014 CFR
2014-01-01
... 14 Aeronautics and Space 1 2014-01-01 2014-01-01 false HIRF Environments and Equipment HIRF Test.... 23, App. J Appendix J to Part 23—HIRF Environments and Equipment HIRF Test Levels This appendix specifies the HIRF environments and equipment HIRF test levels for electrical and electronic systems under...
40 CFR Appendix A to Part 58 - Quality Assurance Requirements for SLAMS, SPMs and PSD Air Monitoring
Code of Federal Regulations, 2014 CFR
2014-07-01
... monitor. 3.3.4.4Pb Performance Evaluation Program (PEP) Procedures. Each year, one performance evaluation... Information 2. Quality System Requirements 3. Measurement Quality Check Requirements 4. Calculations for Data... 10 of this appendix) and at a national level in references 1, 2, and 3 of this appendix. 1...
40 CFR Appendix A to Part 58 - Quality Assurance Requirements for SLAMS, SPMs and PSD Air Monitoring
Code of Federal Regulations, 2013 CFR
2013-07-01
... monitor. 3.3.4.4Pb Performance Evaluation Program (PEP) Procedures. Each year, one performance evaluation... Information 2. Quality System Requirements 3. Measurement Quality Check Requirements 4. Calculations for Data... 10 of this appendix) and at a national level in references 1, 2, and 3 of this appendix. 1...
12 CFR Appendix C to Part 226 - Issuance of Staff Interpretations
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 3 2012-01-01 2012-01-01 false Issuance of Staff Interpretations C Appendix C... RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. C Appendix C to Part 226—Issuance of Staff Interpretations Official Staff Interpretations Officials in the Board's Division of Consumer and Community Affairs...
12 CFR Appendix C to Part 226 - Issuance of Staff Interpretations
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 3 2011-01-01 2011-01-01 false Issuance of Staff Interpretations C Appendix C... RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. C Appendix C to Part 226—Issuance of Staff Interpretations Official Staff Interpretations Officials in the Board's Division of Consumer and Community Affairs...
12 CFR Appendix C to Part 226 - Issuance of Staff Interpretations
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 3 2010-01-01 2010-01-01 false Issuance of Staff Interpretations C Appendix C... RESERVE SYSTEM TRUTH IN LENDING (REGULATION Z) Pt. 226, App. C Appendix C to Part 226—Issuance of Staff Interpretations Official Staff Interpretations Officials in the Board's Division of Consumer and Community Affairs...
14 CFR Appendix C to Part 1215 - Typical User Activity Timeline
Code of Federal Regulations, 2010 CFR
2010-01-01
... 14 Aeronautics and Space 5 2010-01-01 2010-01-01 false Typical User Activity Timeline C Appendix C... RELAY SATELLITE SYSTEM (TDRSS) Pt. 1215, App. C Appendix C to Part 1215—Typical User Activity Timeline... mission model. 3 years before launch (Ref. § 1215.109(c). Submit general user requirements to permit...
32 CFR Appendix F to Part 310 - Format for New or Altered System Report
Code of Federal Regulations, 2010 CFR
2010-07-01
... DEFENSE (CONTINUED) PRIVACY PROGRAM DOD PRIVACY PROGRAM Pt. 310, App. F Appendix F to Part 310—Format for.... Transmittal Letter The transmittal letter shall be prepared by the Defense Privacy Office and shall contain... maintenance of the System; 5. Probable or potential effects on the privacy of individuals; 6. Is the system...
20 CFR 404.1525 - Listing of Impairments in appendix 1.
Code of Federal Regulations, 2012 CFR
2012-04-01
... Impairments (the listings) is in appendix 1 of this subpart. It describes for each of the major body systems... relationship with their counterparts in part A. (c) How do we use the listings? (1) Most body system sections.... (2) The introduction to each body system contains information relevant to the use of the listings in...
20 CFR 404.1525 - Listing of Impairments in appendix 1.
Code of Federal Regulations, 2014 CFR
2014-04-01
... Impairments (the listings) is in appendix 1 of this subpart. It describes for each of the major body systems... relationship with their counterparts in part A. (c) How do we use the listings? (1) Most body system sections.... (2) The introduction to each body system contains information relevant to the use of the listings in...
20 CFR 404.1525 - Listing of Impairments in appendix 1.
Code of Federal Regulations, 2013 CFR
2013-04-01
... Impairments (the listings) is in appendix 1 of this subpart. It describes for each of the major body systems... relationship with their counterparts in part A. (c) How do we use the listings? (1) Most body system sections.... (2) The introduction to each body system contains information relevant to the use of the listings in...
DOE Office of Scientific and Technical Information (OSTI.GOV)
O'Neil, Lori Ross; Conway, T. J.; Tobey, D. H.
The Secure Power Systems Professional Phase III final report was released last year which an appendix of Behavioral Interview Guidelines by Job Roles. This new report is that appendix broken out as a standalone document to assist utilities in recruiting and developing Secure Power Systems Professionals at their site.
Code of Federal Regulations, 2010 CFR
2010-07-01
...) OCCUPATIONAL SAFETY AND HEALTH STANDARDS FOR SHIPYARD EMPLOYMENT Personal Protective Equipment (PPE) Pt. 1915... Personal Fall Protection Systems (Non-Mandatory) B Appendix B to Subpart I of Part 1915 Labor Regulations... Guidelines for Personal Fall Protection Systems (Non-Mandatory) 1. Personal fall arrest systems—(a) General...
Code of Federal Regulations, 2011 CFR
2011-07-01
...) OCCUPATIONAL SAFETY AND HEALTH STANDARDS FOR SHIPYARD EMPLOYMENT Personal Protective Equipment (PPE) Pt. 1915... Personal Fall Protection Systems (Non-Mandatory) B Appendix B to Subpart I of Part 1915 Labor Regulations... Guidelines for Personal Fall Protection Systems (Non-Mandatory) 1. Personal fall arrest systems—(a) General...
DOE Office of Scientific and Technical Information (OSTI.GOV)
O'Neil, Lori Ross; Conway, T. J.; Tobey, D. H.
The Secure Power Systems Professional Phase III final report was released last year which an appendix of Individual and Team Performance Guidelines. This new report is that appendix broken out as a standalone document to assist utilities in recruiting and developing Secure Power Systems Professionals at their site.
12 CFR Appendix A to Subpart H of... - Consumer Grievance Process
Code of Federal Regulations, 2010 CFR
2010-01-01
... Subpart H of Part 208 Banks and Banking FEDERAL RESERVE SYSTEM BOARD OF GOVERNORS OF THE FEDERAL RESERVE SYSTEM MEMBERSHIP OF STATE BANKING INSTITUTIONS IN THE FEDERAL RESERVE SYSTEM (REGULATION H) Consumer Protection in Sales of Insurance Pt. 208, Subpt. H, App. A Appendix A to Subpart H of Part 208—Consumer...
X-33 Combustion-Wave Ignition System Tested
NASA Technical Reports Server (NTRS)
Liou, Larry C.
1999-01-01
The NASA Lewis Research Center, in cooperation with Rocketdyne, the Boeing Company, tested a novel rocket engine ignition system, called the combustion-wave ignition system, in its Research Combustion Laboratory. This ignition system greatly simplifies ignition in rocket engines that have a large number of combustors. The particular system tested was designed and fabricated by Rocketdyne for the national experimental spacecraft, X-33, which uses Rocketdyne s aerospike rocket engines. The goal of the tests was to verify the system design and define its operational characteristics. Results will contribute to the eventual successful flight of X-33. Furthermore, the combustion-wave ignition system, after it is better understood and refined on the basis of the test results and, later, flight-proven onboard X-33, could become an important candidate engine ignition system for our Nation s next-generation reusable launch vehicle.
High-speed flight propulsion systems. Progress in Astronautics and Aeronautics. Vol. 137
DOE Office of Scientific and Technical Information (OSTI.GOV)
Murthy, S.N.B.; Curran, E.T.
1991-01-01
Various papers on high-speed flight propulsion systems are presented. The topics addressed are: propulsion systems from takeoff to high-speed flight, propulsion system performance and integration for high Mach air-breathing flight, energy analysis of high-speed flight systems, waves and thermodynamics in high Mach number propulsive ducts, turbulent free shear layer mixing and combustion, turbulent mixing in supersonic combustion systems, mixing and mixing enhancement in supersonic reacting flowfields, study of combustion and heat-exchange processes in high-enthalpy short-duration facilities, and facility requirements for hypersonic propulsion system testing.
1979-01-01
OF SMALL INTERNAL COMBUSTION ENGINES AS A MEANS 0-.ETC(U) 1979 DAAK7O-78-C-O031 .hhuuufBuhhhh...Aerodyne Dallas th W__tIP FINAL REPORT CONTRACT* DAAK7-78-C-0031 FTURBOCHARGING OF SMALL INTERNAL COMBUSTION ENGINE AS A MEANS OF IMPROVING ENGINE ...DAAK70-78-C0031 TURBOCHARGING OF SMALL INTERNAL COMBUSTION ENGINES AS A MEANS OF IMPROVING ENGINE /APPLICATION SYSTEM FUEL ECONOMY Prepared by
49 CFR Appendix C to Part 238 - Suspension System Safety Performance Standards
Code of Federal Regulations, 2010 CFR
2010-10-01
... 49 Transportation 4 2010-10-01 2010-10-01 false Suspension System Safety Performance Standards C Appendix C to Part 238 Transportation Other Regulations Relating to Transportation (Continued) FEDERAL RAILROAD ADMINISTRATION, DEPARTMENT OF TRANSPORTATION PASSENGER EQUIPMENT SAFETY STANDARDS Pt. 238, App. C...
Combustion system CFD modeling at GE Aircraft Engines
NASA Technical Reports Server (NTRS)
Burrus, D.; Mongia, H.; Tolpadi, Anil K.; Correa, S.; Braaten, M.
1995-01-01
This viewgraph presentation discusses key features of current combustion system CFD modeling capabilities at GE Aircraft Engines provided by the CONCERT code; CONCERT development history; modeling applied for designing engine combustion systems; modeling applied to improve fundamental understanding; CONCERT3D results for current production combustors; CONCERT3D model of NASA/GE E3 combustor; HYBRID CONCERT CFD/Monte-Carlo modeling approach; and future modeling directions.
Combustion system CFD modeling at GE Aircraft Engines
NASA Astrophysics Data System (ADS)
Burrus, D.; Mongia, H.; Tolpadi, Anil K.; Correa, S.; Braaten, M.
1995-03-01
This viewgraph presentation discusses key features of current combustion system CFD modeling capabilities at GE Aircraft Engines provided by the CONCERT code; CONCERT development history; modeling applied for designing engine combustion systems; modeling applied to improve fundamental understanding; CONCERT3D results for current production combustors; CONCERT3D model of NASA/GE E3 combustor; HYBRID CONCERT CFD/Monte-Carlo modeling approach; and future modeling directions.
Flashback Detection Sensor for Hydrogen Augmented Natural Gas Combustion
DOE Office of Scientific and Technical Information (OSTI.GOV)
Thornton, J.D.; Chorpening, B.T.; Sidwell, T.
2007-05-01
The use of hydrogen augmented fuel is being investigated by various researchers as a method to extend the lean operating limit, and potentially reduce thermal NOx formation in natural gas fired lean premixed (LPM) combustion systems. The resulting increase in flame speed during hydrogen augmentation, however, increases the propensity for flashback in LPM systems. Real-time in-situ monitoring of flashback is important for the development of control strategies for use of hydrogen augmented fuel in state-of-the-art combustion systems, and for the development of advanced hydrogen combustion systems. The National Energy Technology Laboratory (NETL) and Woodward Industrial Controls are developing a combustionmore » control and diagnostics sensor (CCADS), which has already been demonstrated as a useful sensor for in-situ monitoring of natural gas combustion, including detection of important combustion events such as flashback and lean blowoff. Since CCADS is a flame ionization sensor technique, the low ion concentration produced in pure hydrogen combustion raises concerns of whether CCADS can be used to monitor flashback in hydrogen augmented combustion. This paper discusses CCADS tests conducted at 0.2-0.6 MPa (2-6 atm), demonstrating flashback detection with fuel compositions up to 80% hydrogen (by volume) mixed with natural gas. NETL’s Simulation Validation (SimVal) combustor offers full optical access to pressurized combustion during these tests. The CCADS data and high-speed video show the reaction zone moves upstream into the nozzle as the hydrogen fuel concentration increases, as is expected with the increased flame speed of the mixture. The CCADS data and video also demonstrate the opportunity for using CCADS to provide the necessary in-situ monitor to control flashback and lean blowoff in hydrogen augmented combustion applications.« less
A Model for the Development of an Organization’s Information System (IS) Security System
1986-12-01
INTRODUCTION — = 52 B. A RISK ASSESSMENT 52 1. Background 52 2. Threat Identification -— — 53 3. Impact Analysis 54 C. LOGICAL DESIGN • — 59 D. PRACTICAL DESIGN...OF ESTIMATED IMPACT AND FREQUENCY • 93 APPENDIX H: COMBINED MATRIX OF 1, F, AND ALE 9 4 APPENDIX I: SECURITY RESOURCES (CONTROLS) 9 5 APPENDIX J...that have been developed, the computer’s impact is sometimes hard to discern. Except in recent years, with the increasing use of microcomputers, the
6 CFR Appendix C to Part 5 - DHS Systems of Records Exempt From the Privacy Act
Code of Federal Regulations, 2010 CFR
2010-01-01
... DISCLOSURE OF RECORDS AND INFORMATION Pt. 5, App. C Appendix C to Part 5—DHS Systems of Records Exempt From... Homeland Security (DHS) Freedom of Information Act (FOIA) and Privacy Act (PA) Record System allows the DHS... information contained in other systems of records subject to such exemptions pursuant to 5 U.S.C. 552a(j)(2...
Steam generator on-line efficiency monitor
DOE Office of Scientific and Technical Information (OSTI.GOV)
Johnson, R.K.; Kaya, A.; Keyes, M.A. IV
1987-08-04
This patent describes a system for automatically and continuously determining the efficiency of a combustion process in a fossil-fuel fired vapor generator for utilization by an automatic load control system that controls the distribution of a system load among a plurality of vapor generators, comprising: a first function generator, connected to an oxygen transducer for sensing the level of excess air in the flue gas, for generating a first signal indicative of the total air supplied for combustion in percent by weight; a second function generator, connected to a combustibles transducer for sensing the level of combustibles in the fluemore » gas, for generating a second signal indicative of the percent combustibles present in the flue gas; means for correcting the first signal, connected to the first and second function generators, when the oxygen transducer is of a type that operates at a temperature level sufficient to cause the unburned combustibles to react with the oxygen present in the flue gas; an ambient air temperature transducer for generating a third signal indicative of the temperature of the ambient air supplied to the vapor generator for combustion.« less
Apparatus for incinerating hazardous waste
Chang, Robert C. W.
1994-01-01
An apparatus for incinerating wastes, including an incinerator having a combustion chamber, a fluidtight shell enclosing the combustion chamber, an afterburner, an off-gas particulate removal system and an emergency off-gas cooling system. The region between the inner surface of the shell and the outer surface of the combustion chamber forms a cavity. Air is supplied to the cavity and heated as it passes over the outer surface of the combustion chamber. Heated air is drawn from the cavity and mixed with fuel for input into the combustion chamber. The pressure in the cavity is maintained at least approximately 2.5 cm WC (about 1" WC) higher than the pressure in the combustion chamber. Gases cannot leak from the combustion chamber since the pressure outside the chamber (inside the cavity) is higher than the pressure inside the chamber. The apparatus can be used to treat any combustible wastes, including biological wastes, toxic materials, low level radioactive wastes, and mixed hazardous and low level transuranic wastes.
Apparatus for incinerating hazardous waste
Chang, R.C.W.
1994-12-20
An apparatus is described for incinerating wastes, including an incinerator having a combustion chamber, a fluid-tight shell enclosing the combustion chamber, an afterburner, an off-gas particulate removal system and an emergency off-gas cooling system. The region between the inner surface of the shell and the outer surface of the combustion chamber forms a cavity. Air is supplied to the cavity and heated as it passes over the outer surface of the combustion chamber. Heated air is drawn from the cavity and mixed with fuel for input into the combustion chamber. The pressure in the cavity is maintained at least approximately 2.5 cm WC higher than the pressure in the combustion chamber. Gases cannot leak from the combustion chamber since the pressure outside the chamber (inside the cavity) is higher than the pressure inside the chamber. The apparatus can be used to treat any combustible wastes, including biological wastes, toxic materials, low level radioactive wastes, and mixed hazardous and low level transuranic wastes. 1 figure.
Mean Flow Augmented Acoustics in Rocket Systems
NASA Technical Reports Server (NTRS)
Fischbach, Sean R.
2015-01-01
Combustion instability in solid rocket motors and liquid engines is a complication that continues to plague designers and engineers. Many rocket systems experience violent fluctuations in pressure, velocity, and temperature originating from the complex interactions between the combustion process and gas dynamics. During sever cases of combustion instability fluctuation amplitudes can reach values equal to or greater than the average chamber pressure. Large amplitude oscillations lead to damaged injectors, loss of rocket performance, damaged payloads, and in some cases breach of case/loss of mission. Historic difficulties in modeling and predicting combustion instability has reduced most rocket systems experiencing instability into a costly fix through testing paradigm or to scrap the system entirely.
Development of Air Supply System for Gas Turbine Combustor Test Rig
NASA Astrophysics Data System (ADS)
Kamarudin, Norhaimi Izlan; Hanafi, Muhammad; Mantari, Asril Rajo; Jaafar, Mohammad Nazri Mohd
2010-06-01
Complete combustion process occurs when the air and fuel burns at their stoichiometric ratio, which determines the appropriate amount of air needed to be supplied to the combustion chamber. Thus, designing an appropriate air supply system is important, especially for multi-fuel combustion. Each type of fuel has different molecular properties and structures which influence the stoichiometric ratio. Therefore, the designed air supply system must be operable for different types of fuels. Basically, the design of the air supply system is at atmospheric pressure. It is important that the air which enters the combustion chamber is stable and straight. From the calculation, the maximum required mass flow rate of air is 0.1468kg/s.
Device to lower NOx in a gas turbine engine combustion system
Laster, Walter R; Schilp, Reinhard; Wiebe, David J
2015-02-24
An emissions control system for a gas turbine engine including a flow-directing structure (24) that delivers combustion gases (22) from a burner (32) to a turbine. The emissions control system includes: a conduit (48) configured to establish fluid communication between compressed air (22) and the combustion gases within the flow-directing structure (24). The compressed air (22) is disposed at a location upstream of a combustor head-end and exhibits an intermediate static pressure less than a static pressure of the combustion gases within the combustor (14). During operation of the gas turbine engine a pressure difference between the intermediate static pressure and a static pressure of the combustion gases within the flow-directing structure (24) is effective to generate a fluid flow through the conduit (48).
Oxide Protective Coats for Ir/Re Rocket Combustion Chambers
NASA Technical Reports Server (NTRS)
Fortini, Arthur; Tuffias, Robert H.
2003-01-01
An improved material system has been developed for rocket engine combustion chambers for burning oxygen/ hydrogen mixtures or novel monopropellants, which are highly oxidizing at operating temperatures. The baseline for developing the improved material system is a prior iridium/rhenium system for chambers burning nitrogen tetroxide/monomethyl hydrazine mixtures, which are less oxidizing. The baseline combustion chamber comprises an outer layer of rhenium that provides structural support, plus an inner layer of iridium that acts as a barrier to oxidation of the rhenium. In the improved material system, the layer of iridium is thin and is coated with a thermal fatigue-resistant refractory oxide (specifically, hafnium oxide) that serves partly as a thermal barrier to decrease the temperature and thus the rate of oxidation of the rhenium. The oxide layer also acts as a barrier against the transport of oxidizing species to the surface of the iridium. Tests in which various oxygen/hydrogen mixtures were burned in iridium/rhenium combustion chambers lined with hafnium oxide showed that the operational lifetimes of combustion chambers of the improved material system are an order of magnitude greater than those of the baseline combustion chambers.
Internet of Things Based Combustible Ice Safety Monitoring System Framework
NASA Astrophysics Data System (ADS)
Sun, Enji
2017-05-01
As the development of human society, more energy is requires to meet the need of human daily lives. New energies play a significant role in solving the problems of serious environmental pollution and resources exhaustion in the present world. Combustible ice is essentially frozen natural gas, which can literally be lit on fire bringing a whole new meaning to fire and ice with less pollutant. This paper analysed the advantages and risks on the uses of combustible ice. By compare to other kinds of alternative energies, the advantages of the uses of combustible ice were concluded. The combustible ice basic physical characters and safety risks were analysed. The developments troubles and key utilizations of combustible ice were predicted in the end. A real-time safety monitoring system framework based on the internet of things (IOT) was built to be applied in the future mining, which provide a brand new way to monitoring the combustible ice mining safety.
Mechanism of plasma-assisted ignition for H2 and C1-C5 hydrocarbons
NASA Astrophysics Data System (ADS)
Starikovskiy, Andrey; Aleksandrov, Nikolay
2016-09-01
Nonequilibrium plasma demonstrates ability to control ultra-lean, ultra-fast, low-temperature flames and appears to be an extremely promising technology for a wide range of applications, including aviation GTEs, piston engines, ramjets, scramjets and detonation initiation for pulsed detonation engines. To use nonequilibrium plasma for ignition and combustion in real energetic systems, one must understand the mechanisms of plasma-assisted ignition and combustion and be able to numerically simulate the discharge and combustion processes under various conditions. A new, validated mechanism for high-temperature hydrocarbon plasma assisted combustion was built and allows to qualitatively describe plasma-assisted combustion close and above the self-ignition threshold. The principal mechanisms of plasma-assisted ignition and combustion have been established and validated for a wide range of plasma and gas parameters. These results provide a basis for improving various energy-conversion combustion systems, from automobile to aircraft engines, using nonequilibrium plasma methods.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Westbrook, C K; Mizobuchi, Y; Poinsot, T J
2004-08-26
Progress in the field of computational combustion over the past 50 years is reviewed. Particular attention is given to those classes of models that are common to most system modeling efforts, including fluid dynamics, chemical kinetics, liquid sprays, and turbulent flame models. The developments in combustion modeling are placed into the time-dependent context of the accompanying exponential growth in computer capabilities and Moore's Law. Superimposed on this steady growth, the occasional sudden advances in modeling capabilities are identified and their impacts are discussed. Integration of submodels into system models for spark ignition, diesel and homogeneous charge, compression ignition engines, surfacemore » and catalytic combustion, pulse combustion, and detonations are described. Finally, the current state of combustion modeling is illustrated by descriptions of a very large jet lifted 3D turbulent hydrogen flame with direct numerical simulation and 3D large eddy simulations of practical gas burner combustion devices.« less
Method and apparatus for detecting combustion instability in continuous combustion systems
Benson, Kelly J.; Thornton, Jimmy D.; Richards, George A.; Straub, Douglas L.
2006-08-29
An apparatus and method to sense the onset of combustion stability is presented. An electrode is positioned in a turbine combustion chamber such that the electrode is exposed to gases in the combustion chamber. A control module applies a voltage potential to the electrode and detects a combustion ionization signal and determines if there is an oscillation in the combustion ionization signal indicative of the occurrence of combustion stability or the onset of combustion instability. A second electrode held in a coplanar but spaced apart manner by an insulating member from the electrode provides a combustion ionization signal to the control module when the first electrode fails. The control module broadcasts a notice if the parameters indicate the combustion process is at the onset of combustion instability or broadcasts an alarm signal if the parameters indicate the combustion process is unstable.
Path planning during combustion mode switch
Jiang, Li; Ravi, Nikhil
2015-12-29
Systems and methods are provided for transitioning between a first combustion mode and a second combustion mode in an internal combustion engine. A current operating point of the engine is identified and a target operating point for the internal combustion engine in the second combustion mode is also determined. A predefined optimized transition operating point is selected from memory. While operating in the first combustion mode, one or more engine actuator settings are adjusted to cause the operating point of the internal combustion engine to approach the selected optimized transition operating point. When the engine is operating at the selected optimized transition operating point, the combustion mode is switched from the first combustion mode to the second combustion mode. While operating in the second combustion mode, one or more engine actuator settings are adjusted to cause the operating point of the internal combustion to approach the target operating point.
An improved model for the combustion of AP composite propellants
NASA Technical Reports Server (NTRS)
Cohen, N. S.; Strand, L. D.
1981-01-01
This paper presents several improvements to the BDP model of steady-state burning of AP composite solid propellants. The Price-Boggs-Derr model of AP monopropellant burning is incorporated to represent the AP. A separate energy equation is written for the binder to permit a different surface temperature from the AP; this includes an analysis of the sharing of primary diffusion flame energy, and correction of a BDP model inconsistency in treating the binder regression rate. A method for assembling component contributions to calculate the burning rates of multimodal propellants is also presented. Results are shown in the form of representative burning rate curves, comparisons with data, and calculated internal details of interest. Ideas for future work are discussed in an Appendix.
12 CFR Appendix A to Part 630 - Supplemental Information Disclosure Guidelines
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 6 2010-01-01 2010-01-01 false Supplemental Information Disclosure Guidelines A Appendix A to Part 630 Banks and Banking FARM CREDIT ADMINISTRATION FARM CREDIT SYSTEM DISCLOSURE TO INVESTORS IN SYSTEMWIDE AND CONSOLIDATED BANK DEBT OBLIGATIONS OF THE FARM CREDIT SYSTEM Pt. 630...
40 CFR Appendix I to Part 94 - Emission-Related Engine Parameters and Specifications
Code of Federal Regulations, 2010 CFR
2010-07-01
... PROGRAMS (CONTINUED) CONTROL OF EMISSIONS FROM MARINE COMPRESSION-IGNITION ENGINES Pt. 94, App. I Appendix...—Reciprocating Engines. 1. Compression ratio. 2. Type of air aspiration (natural, Roots blown, supercharged.... Temperature control system calibration. 4. Maximum allowable inlet air restriction. III. Fuel System. 1...
29 CFR Appendix B to Subpart M of... - Guardrail Systems
Code of Federal Regulations, 2014 CFR
2014-07-01
... 29 Labor 8 2014-07-01 2014-07-01 false Guardrail Systems B Appendix B to Subpart M of Part 1926 Labor Regulations Relating to Labor (Continued) OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR (CONTINUED) SAFETY AND HEALTH REGULATIONS FOR CONSTRUCTION Fall Protection Pt. 1926...
29 CFR Appendix B to Subpart M of... - Guardrail Systems
Code of Federal Regulations, 2013 CFR
2013-07-01
... 29 Labor 8 2013-07-01 2013-07-01 false Guardrail Systems B Appendix B to Subpart M of Part 1926 Labor Regulations Relating to Labor (Continued) OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR (CONTINUED) SAFETY AND HEALTH REGULATIONS FOR CONSTRUCTION Fall Protection Pt. 1926...
29 CFR Appendix B to Subpart M of... - Guardrail Systems
Code of Federal Regulations, 2012 CFR
2012-07-01
... 29 Labor 8 2012-07-01 2012-07-01 false Guardrail Systems B Appendix B to Subpart M of Part 1926 Labor Regulations Relating to Labor (Continued) OCCUPATIONAL SAFETY AND HEALTH ADMINISTRATION, DEPARTMENT OF LABOR (CONTINUED) SAFETY AND HEALTH REGULATIONS FOR CONSTRUCTION Fall Protection Pt. 1926...
Appendix X. ComField Information Management System.
ERIC Educational Resources Information Center
Coffin, Robert W.
This appendix outlines the ComField information management system which is designed to give the project management a comprehensive tool for decisionmaking and to free instructors from tasks of keeping current records of every student's performance, help them plan their time more efficiently for counseling students and planning instruction, and…
14 CFR Appendix J to Part 25 - Emergency Evacuation
Code of Federal Regulations, 2010 CFR
2010-01-01
... AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES Pt. 25, App. J Appendix J to Part 25—Emergency Evacuation...-candles prior to the activation of the airplane emergency lighting system. The source(s) of the initial... airplane emergency lighting system. (b) The airplane must be in a normal attitude with landing gear...
12 CFR Appendix A to Subpart H of... - Consumer Grievance Process
Code of Federal Regulations, 2011 CFR
2011-01-01
... of the bank has violated the requirements of this subpart should contact the Consumer Complaints... 12 Banks and Banking 2 2011-01-01 2011-01-01 false Consumer Grievance Process A Appendix A to... SYSTEM MEMBERSHIP OF STATE BANKING INSTITUTIONS IN THE FEDERAL RESERVE SYSTEM (REGULATION H) Consumer...
12 CFR Appendix A to Subpart H of... - Consumer Grievance Process
Code of Federal Regulations, 2012 CFR
2012-01-01
... of the bank has violated the requirements of this subpart should contact the Consumer Complaints... 12 Banks and Banking 2 2012-01-01 2012-01-01 false Consumer Grievance Process A Appendix A to... SYSTEM MEMBERSHIP OF STATE BANKING INSTITUTIONS IN THE FEDERAL RESERVE SYSTEM (REGULATION H) Consumer...
12 CFR Appendix A to Subpart H of... - Consumer Grievance Process
Code of Federal Regulations, 2013 CFR
2013-01-01
... of the bank has violated the requirements of this subpart should contact the Consumer Complaints... 12 Banks and Banking 2 2013-01-01 2013-01-01 false Consumer Grievance Process A Appendix A to... SYSTEM MEMBERSHIP OF STATE BANKING INSTITUTIONS IN THE FEDERAL RESERVE SYSTEM (REGULATION H) Consumer...
12 CFR Appendix A to Subpart H of... - Consumer Grievance Process
Code of Federal Regulations, 2014 CFR
2014-01-01
... of the bank has violated the requirements of this subpart should contact the Consumer Complaints... 12 Banks and Banking 2 2014-01-01 2014-01-01 false Consumer Grievance Process A Appendix A to... SYSTEM MEMBERSHIP OF STATE BANKING INSTITUTIONS IN THE FEDERAL RESERVE SYSTEM (REGULATION H) Consumer...
System and method for cooling a combustion gas charge
Massey, Mary Cecelia; Boberg, Thomas Earl
2010-05-25
The present invention relates to a system and method for cooling a combustion gas charge prior. The combustion gas charge may include compressed intake air, exhaust gas, or a mixture thereof. An evaporator is provided that may then receive a relatively high temperature combustion gas charge and discharge at a relatively lower temperature. The evaporator may be configured to operate with refrigeration cycle components and/or to receive a fluid below atmospheric pressure as the phase-change cooling medium.
NASA Astrophysics Data System (ADS)
Inozemtsev, A. A.; Sazhenkov, A. N.; Tsatiashvili, V. V.; Abramchuk, T. V.; Shipigusev, V. A.; Andreeva, T. P.; Gumerov, A. R.; Ilyin, A. N.; Gubaidullin, I. T.
2015-05-01
The paper formulates the issue of development of experimental base with noninvasive optical-electronic tools for control of combustion in a combustion chamber of gas turbine engine. The design and specifications of a pilot sample of optronic system are explained; this noninvasive system was created in the framework of project of development of main critical technologies for designing of aviation gas turbine engine PD-14. The testbench run data are presented.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Waterland, L.; Lee, J.W.
1989-04-01
A series of demonstration tests of the American Combustion, Inc., Thermal Destruction System was performed under the SITE program. This oxygen-enhanced combustion system was retrofit to the rotary-kiln incinerator at EPA's Combustion Research Facility. The system's performance was tested firing contaminated soil from the Stringfellow Superfund Site, both alone and mixed with a coal tar waste (KO87). Comparative performance with conventional incinerator operation was also tested. Compliance with the incinerator performance standards of 99.99% principal organic hazardous constituents (POHC) destruction and removal efficiency and particulate emissions of less than 180 mg/dscm at 7% O2 was measured for all tests. Themore » Pyretron system was capable of in-compliance performance at double the mixed waste feedrate and at a 60% increase in batch waste charge mass than possible with conventional incineration. Scrubber blowdown and kiln ash contained no detectable levels of any of the POHCs chosen.« less
7 CFR Appendix A to Subpart G of... - Internal Directives
Code of Federal Regulations, 2010 CFR
2010-01-01
... 7 Agriculture 1 2010-01-01 2010-01-01 false Internal Directives A Appendix A to Subpart G of Part 1 Agriculture Office of the Secretary of Agriculture ADMINISTRATIVE REGULATIONS Privacy Act Regulations Pt. 1, Subpt. G, App. A Appendix A to Subpart G of Part 1—Internal Directives Section 1 General requirements. Each agency that maintains a system...
12 CFR Appendix I to Part 27 - Monthly Home Loan Activity Format
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 1 2011-01-01 2011-01-01 false Monthly Home Loan Activity Format I Appendix I to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. I Appendix I to Part 27—Monthly Home Loan Activity Format EC22SE91...
12 CFR Appendix I to Part 27 - Monthly Home Loan Activity Format
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 1 2013-01-01 2013-01-01 false Monthly Home Loan Activity Format I Appendix I to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. I Appendix I to Part 27—Monthly Home Loan Activity Format EC22SE91...
12 CFR Appendix I to Part 27 - Monthly Home Loan Activity Format
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 1 2014-01-01 2014-01-01 false Monthly Home Loan Activity Format I Appendix I to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. I Appendix I to Part 27—Monthly Home Loan Activity Format EC22SE91...
12 CFR Appendix I to Part 27 - Monthly Home Loan Activity Format
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 1 2012-01-01 2012-01-01 false Monthly Home Loan Activity Format I Appendix I to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. I Appendix I to Part 27—Monthly Home Loan Activity Format EC22SE91...
12 CFR Appendix I to Part 27 - Monthly Home Loan Activity Format
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 1 2010-01-01 2010-01-01 false Monthly Home Loan Activity Format I Appendix I to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. I Appendix I to Part 27—Monthly Home Loan Activity Format EC22SE91...
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 3 2014-01-01 2014-01-01 false Total Annual Loan Cost Rate Computations for Reverse Mortgage Transactions K Appendix K to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED..., App. K Appendix K to Part 226—Total Annual Loan Cost Rate Computations for Reverse Mortgage...
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 3 2013-01-01 2013-01-01 false Total Annual Loan Cost Rate Computations for Reverse Mortgage Transactions K Appendix K to Part 226 Banks and Banking FEDERAL RESERVE SYSTEM (CONTINUED..., App. K Appendix K to Part 226—Total Annual Loan Cost Rate Computations for Reverse Mortgage...
12 CFR Appendix G to Part 226 - Open-End Model Forms and Clauses
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 3 2014-01-01 2014-01-01 false Open-End Model Forms and Clauses G Appendix G... RESERVE SYSTEM (CONTINUED) TRUTH IN LENDING (REGULATION Z) Pt. 226, App. G Appendix G to Part 226—Open-End... Card Accounts Under an Open-End (Not Home-Secured) Consumer Credit Plan [Interest will be charged to...
12 CFR Appendix III to Part 27 - Fair Housing Lending Inquiry/Application Log Sheet
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 1 2010-01-01 2010-01-01 false Fair Housing Lending Inquiry/Application Log Sheet III Appendix III to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. III Appendix III to Part 27—Fair Housing Lending...
APTI Course 427, Combustion Evaluation. Student Workbook.
ERIC Educational Resources Information Center
Beard, J. Taylor; And Others
Presented are exercises intended to supplement course work in air pollution control, specifically as they relate to combustion. Chapters offered in this workbook include: (1) Combustion Calculations, (2) Combustion System Design Problems, (3) Emission Calculations I, (4) Emission Calculations II, (5) Afterburner Design Problems, and (6) Cumbustion…
Dynamical and statistical behavior of discrete combustion waves: a theoretical and numerical study.
Bharath, Naine Tarun; Rashkovskiy, Sergey A; Tewari, Surya P; Gundawar, Manoj Kumar
2013-04-01
We present a detailed theoretical and numerical study of combustion waves in a discrete one-dimensional disordered system. The distances between neighboring reaction cells were modeled with a gamma distribution. The results show that the random structure of the microheterogeneous system plays a crucial role in the dynamical and statistical behavior of the system. This is a consequence of the nonlinear interaction of the random structure of the system with the thermal wave. An analysis of the experimental data on the combustion of a gasless system (Ti + xSi) and a wide range of thermite systems was performed in view of the developed model. We have shown that the burning rate of the powder system sensitively depends on its internal structure. The present model allows for reproducing theoretically the experimental data for a wide range of pyrotechnic mixtures. We show that Arrhenius' macrokinetics at combustion of disperse systems can take place even in the absence of Arrhenius' microkinetics; it can have a purely thermal nature and be related to their heterogeneity and to the existence of threshold temperature. It is also observed that the combustion of disperse systems always occurs in the microheterogeneous mode according to the relay-race mechanism.
Dynamical and statistical behavior of discrete combustion waves: A theoretical and numerical study
NASA Astrophysics Data System (ADS)
Bharath, Naine Tarun; Rashkovskiy, Sergey A.; Tewari, Surya P.; Gundawar, Manoj Kumar
2013-04-01
We present a detailed theoretical and numerical study of combustion waves in a discrete one-dimensional disordered system. The distances between neighboring reaction cells were modeled with a gamma distribution. The results show that the random structure of the microheterogeneous system plays a crucial role in the dynamical and statistical behavior of the system. This is a consequence of the nonlinear interaction of the random structure of the system with the thermal wave. An analysis of the experimental data on the combustion of a gasless system (Ti + xSi) and a wide range of thermite systems was performed in view of the developed model. We have shown that the burning rate of the powder system sensitively depends on its internal structure. The present model allows for reproducing theoretically the experimental data for a wide range of pyrotechnic mixtures. We show that Arrhenius’ macrokinetics at combustion of disperse systems can take place even in the absence of Arrhenius’ microkinetics; it can have a purely thermal nature and be related to their heterogeneity and to the existence of threshold temperature. It is also observed that the combustion of disperse systems always occurs in the microheterogeneous mode according to the relay-race mechanism.
Molecular-beam gas-sampling system
NASA Technical Reports Server (NTRS)
Young, W. S.; Knuth, E. L.
1972-01-01
A molecular beam mass spectrometer system for rocket motor combustion chamber sampling is described. The history of the sampling system is reviewed. The problems associated with rocket motor combustion chamber sampling are reported. Several design equations are presented. The results of the experiments include the effects of cooling water flow rates, the optimum separation gap between the end plate and sampling nozzle, and preliminary data on compositions in a rocket motor combustion chamber.
USAF Aircraft Engine Emission Goals: A Critical Review.
1979-09-01
21 June 1965 and Change 1; and the National Pollution Discharge Elimination System . it applies to all Air Force installations and facilities, the Air...the combustion problems in turbine engines from a more applied viewpoint. He states: "While the combustion system was the primary limitation in... microemulsions and to determine their capacity for reducing smoke emissions from an aviation gas turbine combustion system . (2) A secondary objective is
Test of acoustic tone source and propulsion performance of C8A Buffalo suppressor nozzle
NASA Technical Reports Server (NTRS)
Marrs, C. C.; Harkonen, D. L.; Okeefe, J. V.
1974-01-01
Results are presented for a static acoustic and propulsion performance ground test conducted at the Boeing hot nozzle facility on the C8A Buffalo noise suppressor nozzle. Various methods to remove a nozzle-associated 2000-Hz tone are evaluated. Results of testing this rectangular-array lobed nozzle for propulsion performance and acoustic directivity are reported. Recommendations for future nozzle modifications and further testing are included. Appendix A contains the test plan. Appendix B presents the test log. Appendix C contains plots of the one-third octave sound pressure levels recorded during the test. Appendix D describes the acoustic data recording and reduction systems. The performance data is tabulated in Appendix E.
30 CFR Appendix I to Subpart C of... - National Consensus Standards
Code of Federal Regulations, 2011 CFR
2011-07-01
... Dioxide Extinguishing Systems. NFPA No. 12A—Halon 1301 Extinguishing Systems. NFPA No. 13—Water Sprinkler.... § 57.4261 NFPA No. 14—Standpipe and Hose Systems. § 57.4533 NFPA Fire Protection Handbook. § 57.4560... Fire Prevention and Control Pt. 57, Subpt. C., App. I Appendix I to Subpart C of Part 57—National...
30 CFR Appendix I to Subpart C of... - National Consensus Standards
Code of Federal Regulations, 2012 CFR
2012-07-01
... Dioxide Extinguishing Systems. NFPA No. 12A—Halon 1301 Extinguishing Systems. NFPA No. 13—Water Sprinkler.... § 57.4261 NFPA No. 14—Standpipe and Hose Systems. § 57.4533 NFPA Fire Protection Handbook. § 57.4560... Fire Prevention and Control Pt. 57, Subpt. C., App. I Appendix I to Subpart C of Part 57—National...
30 CFR Appendix I to Subpart C of... - National Consensus Standards
Code of Federal Regulations, 2013 CFR
2013-07-01
... Dioxide Extinguishing Systems. NFPA No. 12A—Halon 1301 Extinguishing Systems. NFPA No. 13—Water Sprinkler.... § 57.4261 NFPA No. 14—Standpipe and Hose Systems. § 57.4533 NFPA Fire Protection Handbook. § 57.4560... Fire Prevention and Control Pt. 57, Subpt. C., App. I Appendix I to Subpart C of Part 57—National...
30 CFR Appendix I to Subpart C of... - National Consensus Standards
Code of Federal Regulations, 2014 CFR
2014-07-01
... Dioxide Extinguishing Systems. NFPA No. 12A—Halon 1301 Extinguishing Systems. NFPA No. 13—Water Sprinkler.... § 57.4261 NFPA No. 14—Standpipe and Hose Systems. § 57.4533 NFPA Fire Protection Handbook. § 57.4560... Fire Prevention and Control Pt. 57, Subpt. C., App. I Appendix I to Subpart C of Part 57—National...
Review of Combustion-acoustic Instabilities
NASA Technical Reports Server (NTRS)
Oyediran, Ayo; Darling, Douglas; Radhakrishnan, Krishnan
1995-01-01
Combustion-acoustic instabilities occur when the acoustic energy increase due to the unsteady heat release of the flame is greater than the losses of acoustic energy from the system. The problem of combustion-acoustic instability is a concern in many devices for various reasons, as each device may have a unique mechanism causing unsteady heat release rates and many have unique boundary conditions. To accurately predict and quantify combustion-acoustic stabilities, the unsteady heat release rate and boundary conditions need to be accurately determined. The present review brings together work performed on a variety of practical combustion devices. Many theoretical and experimental investigations of the unsteady heat release rate have been performed, some based on perturbations in the fuel delivery system particularly for rocket instabilities, while others are based on hydrodynamic processes as in ramjet dump combustors. The boundary conditions for rocket engines have been analyzed and measured extensively. However, less work has been done to measure acoustic boundary conditions in many other combustion systems.
Simulation of Combustion Systems with Realistic g-Jitter
NASA Technical Reports Server (NTRS)
Mell, W. E.; McGrattan, K. B.; Nakamura, Y.; Baum, H. R.
2001-01-01
A number of facilities are available for microgravity combustion experiments: aircraft, drop towers, sounding rockets, the space shuttle, and, in the future, the International Space Station (ISS). Acceleration disturbances or g-jitter about the background level of reduced gravity exist in all these microgravity facilities. While g-jitter is routinely measured, a quantitative comparison of the quality of g-jitter among the different microgravity facilities, in terms of its affects on combustion experiments, has not been compiled. Low frequency g-jitter (< 1 Hz) has been repeatedly observed to disturb a number of combustion systems. Guidelines regarding tolerable levels of acceleration disturbances for combustion experiments have been developed for use in the design of ISS experiments. The validity of these guidelines, however, remains unknown. In this project a transient, 3-D numerical model is under development to simulate the effects of realistic g-jitter on a number of combustion systems. The measured acceleration vector or some representation of it can be used as input to the simulation.
Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants
NASA Technical Reports Server (NTRS)
Gross, R. S.
1980-01-01
A sound data base was established by analytically and experimentally generating basic regenerative cooling, combustion performance, combustion stability, and combustion chamber heat transfer parameters for LOX/HC propellants, with specific application to second generation orbit maneuvering and reaction control systems (OMS/RCS) for the Space Shuttle Orbiter.
40 CFR Table 2 to Subpart Eeee of... - Emission Limits
Code of Federal Regulations, 2011 CFR
2011-07-01
... for combustion devices using supplemental combustion air, by venting emissions through a closed vent... concentration less than or equal to 20 ppmv, on a dry basis corrected to 3 percent oxygen for combustion devices using supplemental combustion air, by venting emissions through a closed vent system to any combination...
Design of biomass management systems and components for closed loop life support systems
NASA Technical Reports Server (NTRS)
Nevill, Gale E., Jr.
1991-01-01
The design of a biomass management system (BMS) for use in a closed loop support system is presented by University of Florida students as the culmination of two design courses. The report is divided into two appendixes, each presenting the results of one of the design courses. The first appendix discusses the preliminary design of the biomass management system and is subdivided into five subsystems: (1) planting and harvesting, (2) food management, (3) resource recovery, (4) refurbishing, and (5) transport. Each subsystem is investigated for possible solutions to problems, and recommendations and conclusions for an integrated BMS are discussed. The second appendix discusses the specific design of components for the BMS and is divided into three sections: (1) a sectored plant growth unit with support systems, (2) a container and receiving mechanism, and (3) an air curtain system for fugitive particle control. In this section components are designed, fabricated, and tested.
Thermal engine driven heat pump for recovery of volatile organic compounds
Drake, Richard L.
1991-01-01
The present invention relates to a method and apparatus for separating volatile organic compounds from a stream of process gas. An internal combustion engine drives a plurality of refrigeration systems, an electrical generator and an air compressor. The exhaust of the internal combustion engine drives an inert gas subsystem and a heater for the gas. A water jacket captures waste heat from the internal combustion engine and drives a second heater for the gas and possibly an additional refrigeration system for the supply of chilled water. The refrigeration systems mechanically driven by the internal combustion engine effect the precipitation of volatile organic compounds from the stream of gas.
Experimental studies of thermal preparation of internal combustion engine
NASA Astrophysics Data System (ADS)
Karnaukhov, N. N.; Merdanov, Sh M.; V, Konev V.; Borodin, D. M.
2018-05-01
In conditions of autonomous functioning of road construction machines, it becomes necessary to use its internal sources. This can be done by using a heat recovery system of an internal combustion engine (ICE). For this purpose, it is proposed to use heat accumulators that accumulate heat of the internal combustion engine during the operation of the machine. Experimental studies have been carried out to evaluate the efficiency of using the proposed pre-start thermal preparation system, which combines a regular system based on liquid diesel fuel heaters and an ICE heat recovery system. As a result, the stages of operation of the preheating thermal preparation system, mathematical models and the dependence of the temperature change of the antifreeze at the exit from the internal combustion engine on the warm-up time are determined.
Stagnation point reverse flow combustor for a combustion system
NASA Technical Reports Server (NTRS)
Zinn, Ben T. (Inventor); Neumeier, Yedidia (Inventor); Seitzman, Jerry M. (Inventor); Jagoda, Jechiel (Inventor); Hashmonay, Ben-Ami (Inventor)
2007-01-01
A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end.
Combustor oscillation attenuation via the control of fuel-supply line dynamics
Richards, George A.; Gemmen, Randall S.
1998-01-01
Combustion oscillation control in combustion systems using hydrocarbon fuels is provided by acoustically tuning a fuel-delivery line to a desired phase of the combustion oscillations for providing a pulse of a fuel-rich region at the oscillating flame front at each time when the oscillation produced pressure in the combustion chamber is in a low pressure phase. The additional heat release produced by burning such fuel-rich regions during low combustion chamber pressure effectively attenuates the combustion oscillations to a selected value.
40 CFR Appendix B to Subpart Uuuuu... - -HCl and HF Monitoring Provisions
Code of Federal Regulations, 2013 CFR
2013-07-01
... extractive Fourier Transform Infrared Spectroscopy (FTIR) continuous emissions monitoring systems in appendix... Fourier Transform Infrared (FTIR) Spectroscopy” (incorporated by reference, see § 63.14), each applied...
40 CFR Appendix B to Subpart Uuuuu... - -HCl and HF Monitoring Provisions
Code of Federal Regulations, 2014 CFR
2014-07-01
... extractive Fourier Transform Infrared Spectroscopy (FTIR) continuous emissions monitoring systems in appendix... Fourier Transform Infrared (FTIR) Spectroscopy” (incorporated by reference, see § 63.14), each applied...
[Study on expert system of infrared spectral characteristic of combustible smoke agent].
Song, Dong-ming; Guan, Hua; Hou, Wei; Pan, Gong-pei
2009-05-01
The present paper studied the application of expert system in prediction of infrared spectral characteristic of combustible anti-infrared smoke agent. The construction of the expert system was founded, based on the theory of minimum free energy and infrared spectral addition. After the direction of smoke agent was input, the expert system could figure out the final combustion products. Then infrared spectrogram of smoke could also be simulated by adding the spectra of all of the combustion products. Meanwhile, the screening index of smoke was provided in the wave bands of 3-5 im and 8-14 microm. FTIR spectroscope was used to investigate the performance of one kind of HC smoke. The combustion products calculated by the expert system were coincident with the actual data, and the simulant infrared spectrum was also similar to the real one of the smoke. The screening index given by the system was consistent with the known facts. It was showed that a new approach was offered for the fast discrimination of varieties of directions of smoke agent.
Method and system for controlled combustion engines
Oppenheim, A. K.
1990-01-01
A system for controlling combustion in internal combustion engines of both the Diesel or Otto type, which relies on establishing fluid dynamic conditions and structures wherein fuel and air are entrained, mixed and caused to be ignited in the interior of a multiplicity of eddies, and where these structures are caused to sequentially fill the headspace of the cylinders.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Smith, P.V.
1995-12-31
Coal fired, low emission sources are a major factor in the air quality problems facing eastern European cities. These sources include: stoker-fired boilers which feed district heating systems and also meet local industrial steam demand, hand-fired boilers which provide heat for one building or a small group of buildings, and masonary tile stoves which heat individual rooms. Global Environmental Systems is marketing through Global Environmental Systems of Polane, Inc. catalysts to improve the combustion of coal, wood or fuel oils in these combustion systems. PCCL-II Combustion Catalysts promotes more complete combustion, reduces or eliminates slag formations, soot, corrosion and somemore » air pollution emissions and is especially effective on high sulfur-high vanadium residual oils. Glo-Klen is a semi-dry powder continuous acting catalyst that is injected directly into the furnace of boilers by operating personnel. It is a multi-purpose catalyst that is a furnace combustion catalyst that saves fuel by increasing combustion efficiency, a cleaner of heat transfer surfaces that saves additional fuel by increasing the absorption of heat, a corrosion-inhibiting catalyst that reduces costly corrosion damage and an air pollution reducing catalyst that reduces air pollution type stack emissions. The reduction of sulfur dioxides from coal or oil-fired boilers of the hand fired stoker design and larger, can be controlled by the induction of the Glo-Klen combustion catalyst and either hydrated lime or pulverized limestone.« less
NASA Astrophysics Data System (ADS)
Hernandez, Manuel Johannes
A general consensus in the scientific and research community is the need to restrict carbon emissions in energy systems. Therefore, extensive research efforts are underway to develop the next generation of energy systems. In the field of power generation, researchers are actively investigating novel methods to produce electricity in a cleaner, efficient form. Recently, Oxy-Combustion for magnetohydrodynamic power extraction has generated significant interest, since the idea was proposed as a method for clean power generation in coal and natural gas power plants. Oxy-combustion technologies have been proposed to provide high enthalpy, electrically conductive flows for direct conversion of electricity. Direct power extraction via magnetohydrodynamics (MHD) can occur as a consequence of the motion of "seeded" combustion products in the presence of magnetic fields. However, oxy-combustion technologies for MHD power extraction has not been demonstrated in the available literature. Furthermore, there are still fundamental unexplored questions remaining, associated with this technology, for MHD power extraction. In this present study, previous magnetohydrodynamic combustion technologies and technical issues in this field were assessed to develop a new combustion system for electrically conductive flows. The research aims were to fully understand the current-state-of-the-art of open-cycle magnetohydrodynamic technologies and present new future directions and concepts. The design criteria, methodology, and technical specifications of an advanced cooled oxy-combustion technology are presented in this dissertation. The design was based on a combined analytical, empirical, and numerical approach. Analytical one-dimensional (1D) design tools initiated design construction. Design variants were analyzed and vetted against performance criteria through the application of computational fluid dynamics modeling. CFD-generated flow fields permitted insightful visualization of the design concepts. Therefore, numerical computational fluid dynamics (CFD) models were developed to design and optimize the combustion flow fields of oxy-fuel combustion systems. These models were analyzed to understand the boundary layer and heat transfer profile and qualitative behaviors in the product designs. Advanced materials for high-temperature applications were assessed for their possible implementation in the product design. A trade-off analysis indicated that this scheme may incur elevated product cost and a difficulty in manufacturing. Active cooling strategies were considered for product development. A rocket-based cooling scheme, regenerative cooling, was implemented to provide active cooling. In the hot gas path (HGP) cooling design, CFD models were developed to predict the variation of heat removal along the oxy-combustion wall for various operating conditions. The oxy-combustion technology was manufactured using electrical discharge machining (EDM). The product development lifecycle in this dissertation encompassed preliminary design, detailed design, and demonstration and validation of the product. Towards the final stages of the product development, Fuel-rich oxy combustion experiments were carried out to demonstrate and observe flame characteristics from the designed technology and to predict heat transfer loads. The demonstration findings of oxy-combustion flames are presented in this work to contribute the developing field of MHD direct power extraction, which lacks oxy-combustion design data and qualitative combustion datasets. The findings show that this oxy-combustion concept is capable of providing a high-enthalpy MHD environment for seeding, in order to render the flow to be conductive. Based on previous findings, temperatures in the range of 2800-3000 K may enable magnetohydrodynamic power extraction. The combustor hardware design was developed to contribute to engineered systems rated less than 100 kW for demonstration. The product hardware was designed to produce gas velocities of 2000 m/s gas and temperatures within the following range of 2800-3000 K. In the injection system, the momentum flux ratio (MFR) was estimated to be 16. The heat loss fraction in this oxy-combustion system, based on CFD and analytical calculations, at optimal operating conditions, was estimated to be less than 10 percent. Furthermore, the heat transfer design removed approximately 7 MW/m2. The experimental performance of oxy-combustion systems demonstrates promise for advanced power generation applications.
Combustion flame-plasma hybrid reactor systems, and chemical reactant sources
Kong, Peter C
2013-11-26
Combustion flame-plasma hybrid reactor systems, chemical reactant sources, and related methods are disclosed. In one embodiment, a combustion flame-plasma hybrid reactor system comprising a reaction chamber, a combustion torch positioned to direct a flame into the reaction chamber, and one or more reactant feed assemblies configured to electrically energize at least one electrically conductive solid reactant structure to form a plasma and feed each electrically conductive solid reactant structure into the plasma to form at least one product is disclosed. In an additional embodiment, a chemical reactant source for a combustion flame-plasma hybrid reactor comprising an elongated electrically conductive reactant structure consisting essentially of at least one chemical reactant is disclosed. In further embodiments, methods of forming a chemical reactant source and methods of chemically converting at least one reactant into at least one product are disclosed.
40 CFR Appendix B to Subpart Uuuuu - -HCl and HF Monitoring Provisions
Code of Federal Regulations, 2012 CFR
2012-07-01
... Fourier Transform Infrared Spectroscopy (FTIR) continuous emissions monitoring systems in appendix B to... Fourier Transform Infrared (FTIR) Spectroscopy” (incorporated by reference, see § 63.14), each applied...
Code of Federal Regulations, 2010 CFR
2010-07-01
... LAKES SYSTEM Pt. 132, App. A Appendix A to Part 132—Great Lakes Water Quality Initiative Methodologies... 40 Protection of Environment 21 2010-07-01 2010-07-01 false Great Lakes Water Quality Initiative Methodologies for Development of Aquatic Life Criteria and Values A Appendix A to Part 132 Protection of...
Code of Federal Regulations, 2011 CFR
2011-07-01
... LAKES SYSTEM Pt. 132, App. A Appendix A to Part 132—Great Lakes Water Quality Initiative Methodologies... 40 Protection of Environment 22 2011-07-01 2011-07-01 false Great Lakes Water Quality Initiative Methodologies for Development of Aquatic Life Criteria and Values A Appendix A to Part 132 Protection of...
12 CFR Appendix IV to Part 27 - Home Loan Data Submission
Code of Federal Regulations, 2014 CFR
2014-01-01
... 12 Banks and Banking 1 2014-01-01 2014-01-01 false Home Loan Data Submission IV Appendix IV to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. IV Appendix IV to Part 27—Home Loan Data Submission ER21JN94.003 ER21JN94...
12 CFR Appendix IV to Part 27 - Home Loan Data Submission
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 1 2013-01-01 2013-01-01 false Home Loan Data Submission IV Appendix IV to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. IV Appendix IV to Part 27—Home Loan Data Submission ER21JN94.003 ER21JN94...
12 CFR Appendix IV to Part 27 - Home Loan Data Submission
Code of Federal Regulations, 2011 CFR
2011-01-01
... 12 Banks and Banking 1 2011-01-01 2011-01-01 false Home Loan Data Submission IV Appendix IV to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. IV Appendix IV to Part 27—Home Loan Data Submission ER21JN94.003 ER21JN94...
12 CFR Appendix IV to Part 27 - Home Loan Data Submission
Code of Federal Regulations, 2012 CFR
2012-01-01
... 12 Banks and Banking 1 2012-01-01 2012-01-01 false Home Loan Data Submission IV Appendix IV to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. IV Appendix IV to Part 27—Home Loan Data Submission ER21JN94.003 ER21JN94...
12 CFR Appendix G to Part 226 - Open-End Model Forms and Clauses
Code of Federal Regulations, 2013 CFR
2013-01-01
... 12 Banks and Banking 3 2013-01-01 2013-01-01 false Open-End Model Forms and Clauses G Appendix G... RESERVE SYSTEM (CONTINUED) TRUTH IN LENDING (REGULATION Z) Pt. 226, App. G Appendix G to Part 226—Open-End Model Forms and Clauses G-1Balance Computation Methods Model Clauses (Home-equity Plans) (§§ 226.6 and...
12 CFR Appendix B to Part 230 - Model Clauses and Sample Forms
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 3 2010-01-01 2010-01-01 false Model Clauses and Sample Forms B Appendix B to... SYSTEM TRUTH IN SAVINGS (REGULATION DD) Pt. 230, App. B Appendix B to Part 230—Model Clauses and Sample Forms Table of contents B-1—Model Clauses for Account Disclosures (Section 230.4(b)) B-2—Model Clauses...
32 CFR Appendix C to Part 310 - DoD Blanket Routine Uses
Code of Federal Regulations, 2010 CFR
2010-07-01
... 32 National Defense 2 2010-07-01 2010-07-01 false DoD Blanket Routine Uses C Appendix C to Part...) PRIVACY PROGRAM DOD PRIVACY PROGRAM Pt. 310, App. C Appendix C to Part 310—DoD Blanket Routine Uses (See paragraph (c) of § 310.22 of subpart E) A. Routine Use—Law Enforcement If a system of records maintained by...
12 CFR Appendix IV to Part 27 - Home Loan Data Submission
Code of Federal Regulations, 2010 CFR
2010-01-01
... 12 Banks and Banking 1 2010-01-01 2010-01-01 false Home Loan Data Submission IV Appendix IV to Part 27 Banks and Banking COMPTROLLER OF THE CURRENCY, DEPARTMENT OF THE TREASURY FAIR HOUSING HOME LOAN DATA SYSTEM Pt. 27, App. IV Appendix IV to Part 27—Home Loan Data Submission ER21JN94.003 ER21JN94...
40 CFR Appendix B to Part 132 - Great Lakes Water Quality Initiative
Code of Federal Regulations, 2011 CFR
2011-07-01
... WATER QUALITY GUIDANCE FOR THE GREAT LAKES SYSTEM Pt. 132, App. B Appendix B to Part 132—Great Lakes Water Quality Initiative Methodology for Deriving Bioaccumulation Factors Great Lakes States and Tribes... system. For log KOW, the log of the octanol-water partition coefficient is a base 10 logarithm. Uptake...
40 CFR Appendix B to Part 132 - Great Lakes Water Quality Initiative
Code of Federal Regulations, 2010 CFR
2010-07-01
... WATER QUALITY GUIDANCE FOR THE GREAT LAKES SYSTEM Pt. 132, App. B Appendix B to Part 132—Great Lakes Water Quality Initiative Methodology for Deriving Bioaccumulation Factors Great Lakes States and Tribes... system. For log KOW, the log of the octanol-water partition coefficient is a base 10 logarithm. Uptake...
14 CFR 415.129 - Flight safety system test data.
Code of Federal Regulations, 2012 CFR
2012-01-01
..., acceptance, age surveillance, and preflight testing of a flight safety system and its subsystems and..., subsystem, and component testing requirements of part 417 of this chapter and appendix E to part 417 of this... demonstrate similarity by performing the analysis required by appendix E of part 417 of this chapter. The...
14 CFR 415.129 - Flight safety system test data.
Code of Federal Regulations, 2011 CFR
2011-01-01
..., acceptance, age surveillance, and preflight testing of a flight safety system and its subsystems and..., subsystem, and component testing requirements of part 417 of this chapter and appendix E to part 417 of this... demonstrate similarity by performing the analysis required by appendix E of part 417 of this chapter. The...
14 CFR 415.129 - Flight safety system test data.
Code of Federal Regulations, 2013 CFR
2013-01-01
..., acceptance, age surveillance, and preflight testing of a flight safety system and its subsystems and..., subsystem, and component testing requirements of part 417 of this chapter and appendix E to part 417 of this... demonstrate similarity by performing the analysis required by appendix E of part 417 of this chapter. The...
14 CFR 415.129 - Flight safety system test data.
Code of Federal Regulations, 2010 CFR
2010-01-01
..., acceptance, age surveillance, and preflight testing of a flight safety system and its subsystems and..., subsystem, and component testing requirements of part 417 of this chapter and appendix E to part 417 of this... demonstrate similarity by performing the analysis required by appendix E of part 417 of this chapter. The...
14 CFR 415.129 - Flight safety system test data.
Code of Federal Regulations, 2014 CFR
2014-01-01
..., acceptance, age surveillance, and preflight testing of a flight safety system and its subsystems and..., subsystem, and component testing requirements of part 417 of this chapter and appendix E to part 417 of this... demonstrate similarity by performing the analysis required by appendix E of part 417 of this chapter. The...
Code of Federal Regulations, 2011 CFR
2011-07-01
..., Specification Test Procedures for Monitoring Systems for Effluent Stream Gas Volumetric Flow Rate E Appendix E... Stream Gas Volumetric Flow Rate 1. Principle and applicability. 1.1Principle. Effluent stream gas... method is applicable to subparts which require continuous gas volumetric flow rate measurement...
Code of Federal Regulations, 2010 CFR
2010-07-01
..., Specification Test Procedures for Monitoring Systems for Effluent Stream Gas Volumetric Flow Rate E Appendix E... Stream Gas Volumetric Flow Rate 1. Principle and applicability. 1.1Principle. Effluent stream gas... method is applicable to subparts which require continuous gas volumetric flow rate measurement...
32 CFR Appendix H to Part 323 - DLA Exemption Rules
Code of Federal Regulations, 2011 CFR
2011-07-01
... PROGRAM DEFENSE LOGISTICS AGENCY PRIVACY PROGRAM Pt. 323, App. H Appendix H to Part 323—DLA Exemption... systems of records maintained by the Defense Logistics Agency will be exempt from the requirements of 5 U... Defense Logistics Agency claims the same exemptions for the records from those “other” systems that are...