Sample records for lugs

  1. Weapon System Costing Methodology for Aircraft Airframes and Basic Structures Volume II - Estimating Handbook and User’s Manual, Part 2

    DTIC Science & Technology

    1975-05-01

    4bo» i) (46u t2) ( 4tib > 3 ) ( 4bD » fa) .1 .1 .1 .1 LÜG LÜG LÜG LUG LÜG LUG LÜG Lud LÜG LUG LUG LUG LÜG LÜG LUG Lüb LÜG LUG...PC2UI LUG PC310 LUG PL 111 LuG PC211 LÜG PL 31 1 LÜG PL212 PL312 .OB LUG LUG LÄWüING GEAR «LWüRK (4bb»1) + (468»1) (4bbf2) + (46P»2) ( 4bD »3...JiJCDtJCDCDt3(JCDO»-tOOCDC3tDC3i-J_7CD( t^cJtJCJ(D^J Ducju>ot-Jt-Jur>j > 03 J- IT J- -* IP ip >r IP 0- *S -* <D O rj >1 O --i TD -D -i TD O 4 * UJ

  2. Investigation of Selectively-Reinforced Metallic Lugs

    NASA Technical Reports Server (NTRS)

    Farley, Gary L.; Abada, Christopher H.

    2007-01-01

    An investigation of the effects of material and geometric variables on the response of U-shaped band-reinforced metallic lugs was performed. Variables studied were reinforcement, adhesive and metallic lug mechanical properties, hole diameter, reinforcement and adhesive thickness, and the distance from the hole s center to the end of the lug. Generally, U-shaped band reinforced lugs exhibited superior performance than non-reinforced lugs, that is higher load at the conventional lug design criteria of four percent hole elongation. Depending upon the reinforcement configuration the increase in load may be negligible to 15 or 20 percent. U-shaped band reinforcement increases lug load carrying capability primarily through two mechanisms; increasing the slope of the response curve after the initial knee and restraining overall deformation of the metallic portion of the lug facilitating increased yielding of metallic material between the hole and the edge of the metallic portion of the lug.

  3. Precise 3D Lug Pose Detection Sensor for Automatic Robot Welding Using a Structured-Light Vision System

    PubMed Central

    Park, Jae Byung; Lee, Seung Hun; Lee, Il Jae

    2009-01-01

    In this study, we propose a precise 3D lug pose detection sensor for automatic robot welding of a lug to a huge steel plate used in shipbuilding, where the lug is a handle to carry the huge steel plate. The proposed sensor consists of a camera and four laser line diodes, and its design parameters are determined by analyzing its detectable range and resolution. For the lug pose acquisition, four laser lines are projected on both lug and plate, and the projected lines are detected by the camera. For robust detection of the projected lines against the illumination change, the vertical threshold, thinning, Hough transform and separated Hough transform algorithms are successively applied to the camera image. The lug pose acquisition is carried out by two stages: the top view alignment and the side view alignment. The top view alignment is to detect the coarse lug pose relatively far from the lug, and the side view alignment is to detect the fine lug pose close to the lug. After the top view alignment, the robot is controlled to move close to the side of the lug for the side view alignment. By this way, the precise 3D lug pose can be obtained. Finally, experiments with the sensor prototype are carried out to verify the feasibility and effectiveness of the proposed sensor. PMID:22400007

  4. The Role of Lug Preheating, Melt Pool Temperature, and Lug Entrance Delay on the Cast-on-Strap Joining Process

    NASA Astrophysics Data System (ADS)

    Pahlavan, Sohrab; Nikpour, Saman; Mirjalili, Mostafa; Alagheband, Ali; Azimi, Mohammadyousef; Taji, Iman

    2017-07-01

    This work deals with effective parameters in the cast-on-strap (COS) process during which grid lugs of a lead-acid battery are joined together by a strap. The effects of lug preheating, melt pool temperature, and lug entrance delay on the quality of joints and casting defects were investigated. Lug preheating was found to propitiously reduce joint internal voids because of flux elimination. Its adverse effect on lowering lug wettability, however, made it unfavorable under the experimental conditions. The melt pool temperature also showed a two-sided effect depending on the process conditions. Raising the temperature increases the strap melt fluidity, which improves the joint contact area; however, it has a negative effect on lug wettability by flux evaporation. Besides, higher temperatures cause more lug back-melting and, hence, lower relative contact lengths. Therefore, an intermediate temperature of 683 K (410 °C) was found to make the most proper condition. Moreover, the case at which the lugs enter the mold coincident with its filling by the melt rendered the best joint quality. In this condition, the melt flows through the interlug spaces, which helps the voids to escape, resulting in the better joint interface. As the conclusion, the lug entrance time has the most effective role on joint quality, considering that lug preheating does not show any improving effect.

  5. 7 CFR 51.1527 - Standard pack.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... peach boxes, lug boxes and small consumer packages. In layer-packed California peach boxes or lug boxes... package. The number of plums or prunes in California peach boxes or lug boxes shall not vary more than 4... container. (ii) Face and fill packs in cartons and lug boxes. In face and fill packs in cartons and lug...

  6. 7 CFR 51.1527 - Standard pack.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... peach boxes, lug boxes and small consumer packages. In layer-packed California peach boxes or lug boxes... package. The number of plums or prunes in California peach boxes or lug boxes shall not vary more than 4... container. (ii) Face and fill packs in cartons and lug boxes. In face and fill packs in cartons and lug...

  7. A Study on Wheel Sinkage and Rolling Resistance with variations in wheel geometry for Plain and Lugged wheels on TRI -1 Soil Simulant

    NASA Astrophysics Data System (ADS)

    Gireesh Kumar, Pala; Jayalekshmi, S.

    2018-03-01

    Wheel-soil Interaction studies are gaining momentum in the field of Terramechanics, but the basis is Terzaghi’s bearing capacity equation. For the current study, on a lunar soil simulant TRI – 1, two plain rigid wheels are considered, i.e., small wheel (dia. of 210 mm and width of 50 mm) and large wheel (dia. 160 mm and width 32 mm). Also, different number of lugs (N = 8, 12, 16) with various lug heights (h = 5 mm, 10 mm, 15 mm) are used. In this paper, the variation of wheel sinkages from experiments obtained for various wheel weights are examined and presented. The parameter, Coefficient of rolling resistance (CRR) is determined for various cases. Hence, rolling resistance was determined and examined from the obtained CRR for all cases. Among the cases examined, the large wheel with weight 67.44 N for plain wheels and weight 67.85 N for lugged wheel (no. of lugs = 16, and height of lugs = 5 mm) registered better mobility. Similarly, for small wheel with weight 52.189 N for plain wheel and weight 52.481 N for lugged wheel (no. of lugs = 16, and height of lugs = 5 mm) registered better mobility, a lesser rolling resistance for these cases.

  8. 7 CFR 29.3152 - Lugs or Cutters (C Group).

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... percent uniform, and 15 percent injury tolerance. C4L Fair Buff Lugs. Thin, mature to ripe, firm to open... percent injury tolerance. C5L Low Buff Lugs. Thin, mature, firm to open, wavy dull finish, pale color... Fair Tan Lugs. Medium to thin body, mature to ripe, firm to open, wavy to even, moderate finish, weak...

  9. 7 CFR 29.3152 - Lugs or Cutters (C Group).

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... percent uniform, and 15 percent injury tolerance. C4L Fair Buff Lugs. Thin, mature to ripe, firm to open... percent injury tolerance. C5L Low Buff Lugs. Thin, mature, firm to open, wavy dull finish, pale color... Fair Tan Lugs. Medium to thin body, mature to ripe, firm to open, wavy to even, moderate finish, weak...

  10. 7 CFR 29.3152 - Lugs or Cutters (C Group).

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... percent uniform, and 15 percent injury tolerance. C4L Fair Buff Lugs. Thin, mature to ripe, firm to open... percent injury tolerance. C5L Low Buff Lugs. Thin, mature, firm to open, wavy dull finish, pale color... Fair Tan Lugs. Medium to thin body, mature to ripe, firm to open, wavy to even, moderate finish, weak...

  11. 7 CFR 29.3152 - Lugs or Cutters (C Group).

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... intensity, narrow, 70 percent uniform, and 30 percent injury tolerance. C1F Choice Tan Lugs. Medium to thin... uniform, and 5 percent injury tolerance. C2F Fine Tan Lugs. Medium to thin body, ripe, open, smooth... injury tolerance. C3F Good Tan Lugs. Medium to thin body, ripe, open, even, clear finish, moderate color...

  12. 7 CFR 29.3152 - Lugs or Cutters (C Group).

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... intensity, narrow, 70 percent uniform, and 30 percent injury tolerance. C1F Choice Tan Lugs. Medium to thin... uniform, and 5 percent injury tolerance. C2F Fine Tan Lugs. Medium to thin body, ripe, open, smooth... injury tolerance. C3F Good Tan Lugs. Medium to thin body, ripe, open, even, clear finish, moderate color...

  13. Tip cap for a turbine rotor blade

    DOEpatents

    Kimmel, Keith D

    2014-03-25

    A turbine rotor blade with a spar and shell construction, and a tip cap that includes a row of lugs extending from a bottom side that form dovetail grooves that engage with similar shaped lugs and grooves on a tip end of the spar to secure the tip cap to the spar against radial displacement. The lug on the trailing edge end of the tip cap is aligned perpendicular to a chordwise line of the blade in the trailing edge region in order to minimize stress due to the lugs wanting to bend under high centrifugal loads. A two piece tip cap with lugs at different angles will reduce the bending stress even more.

  14. 7 CFR 51.1527 - Standard pack.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... size, 45 size, 50 size, 55 size, etc.). (i) California peach boxes, lug boxes and small consumer packages. In layer-packed California peach boxes or lug boxes, and in small layer packed consumer packages... California peach boxes or lug boxes shall not vary more than 4 from the number indicated on the package...

  15. 7 CFR 51.1527 - Standard pack.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... size, 45 size, 50 size, 55 size, etc.). (i) California peach boxes, lug boxes and small consumer packages. In layer-packed California peach boxes or lug boxes, and in small layer packed consumer packages... California peach boxes or lug boxes shall not vary more than 4 from the number indicated on the package...

  16. 7 CFR 29.2439 - Lugs (X Group).

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 7 Agriculture 2 2014-01-01 2014-01-01 false Lugs (X Group). 29.2439 Section 29.2439 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... INSPECTION Standards Grades § 29.2439 Lugs (X Group). This group consists of leaves that normally grow near...

  17. 7 CFR 29.2439 - Lugs (X Group).

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 2 2010-01-01 2010-01-01 false Lugs (X Group). 29.2439 Section 29.2439 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... INSPECTION Standards Grades § 29.2439 Lugs (X Group). This group consists of leaves that normally grow near...

  18. 7 CFR 29.2439 - Lugs (X Group).

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 7 Agriculture 2 2013-01-01 2013-01-01 false Lugs (X Group). 29.2439 Section 29.2439 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... INSPECTION Standards Grades § 29.2439 Lugs (X Group). This group consists of leaves that normally grow near...

  19. 7 CFR 29.2439 - Lugs (X Group).

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 7 Agriculture 2 2012-01-01 2012-01-01 false Lugs (X Group). 29.2439 Section 29.2439 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... INSPECTION Standards Grades § 29.2439 Lugs (X Group). This group consists of leaves that normally grow near...

  20. 7 CFR 29.2439 - Lugs (X Group).

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 7 Agriculture 2 2011-01-01 2011-01-01 false Lugs (X Group). 29.2439 Section 29.2439 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... INSPECTION Standards Grades § 29.2439 Lugs (X Group). This group consists of leaves that normally grow near...

  1. NASA Structural Analysis Report on the American Airlines Flight 587 Accident - Local Analysis of the Right Rear Lug

    NASA Technical Reports Server (NTRS)

    Raju, Ivatury S; Glaessgen, Edward H.; Mason, Brian H; Krishnamurthy, Thiagarajan; Davila, Carlos G

    2005-01-01

    A detailed finite element analysis of the right rear lug of the American Airlines Flight 587 - Airbus A300-600R was performed as part of the National Transportation Safety Board s failure investigation of the accident that occurred on November 12, 2001. The loads experienced by the right rear lug are evaluated using global models of the vertical tail, local models near the right rear lug, and a global-local analysis procedure. The right rear lug was analyzed using two modeling approaches. In the first approach, solid-shell type modeling is used, and in the second approach, layered-shell type modeling is used. The solid-shell and the layered-shell modeling approaches were used in progressive failure analyses (PFA) to determine the load, mode, and location of failure in the right rear lug under loading representative of an Airbus certification test conducted in 1985 (the 1985-certification test). Both analyses were in excellent agreement with each other on the predicted failure loads, failure mode, and location of failure. The solid-shell type modeling was then used to analyze both a subcomponent test conducted by Airbus in 2003 (the 2003-subcomponent test) and the accident condition. Excellent agreement was observed between the analyses and the observed failures in both cases. From the analyses conducted and presented in this paper, the following conclusions were drawn. The moment, Mx (moment about the fuselage longitudinal axis), has significant effect on the failure load of the lugs. Higher absolute values of Mx give lower failure loads. The predicted load, mode, and location of the failure of the 1985-certification test, 2003-subcomponent test, and the accident condition are in very good agreement. This agreement suggests that the 1985-certification and 2003- subcomponent tests represent the accident condition accurately. The failure mode of the right rear lug for the 1985-certification test, 2003-subcomponent test, and the accident load case is identified as a cleavage-type failure. For the accident case, the predicted failure load for the right rear lug from the PFA is greater than 1.98 times the limit load of the lugs. I.

  2. Structural Analysis of the Right Rear Lug of American Airlines Flight 587

    NASA Technical Reports Server (NTRS)

    Raju, Ivatury S.; Glaessgen, Edward H.; Mason, Brian H.; Krishnamurthy, Thiagarajan; Davila, Carlos G.

    2006-01-01

    A detailed finite element analysis of the right rear lug of the American Airlines Flight 587 - Airbus A300-600R was performed as part of the National Transportation Safety Board s failure investigation of the accident that occurred on November 12, 2001. The loads experienced by the right rear lug are evaluated using global models of the vertical tail, local models near the right rear lug, and a global-local analysis procedure. The right rear lug was analyzed using two modeling approaches. In the first approach, solid-shell type modeling is used, and in the second approach, layered-shell type modeling is used. The solid-shell and the layered-shell modeling approaches were used in progressive failure analyses (PFA) to determine the load, mode, and location of failure in the right rear lug under loading representative of an Airbus certification test conducted in 1985 (the 1985-certification test). Both analyses were in excellent agreement with each other on the predicted failure loads, failure mode, and location of failure. The solid-shell type modeling was then used to analyze both a subcomponent test conducted by Airbus in 2003 (the 2003-subcomponent test) and the accident condition. Excellent agreement was observed between the analyses and the observed failures in both cases. The moment, Mx (moment about the fuselage longitudinal axis), has significant effect on the failure load of the lugs. Higher absolute values of Mx give lower failure loads. The predicted load, mode, and location of the failure of the 1985- certification test, 2003-subcomponent test, and the accident condition are in very good agreement. This agreement suggests that the 1985-certification and 2003-subcomponent tests represent the accident condition accurately. The failure mode of the right rear lug for the 1985-certification test, 2003-subcomponent test, and the accident load case is identified as a cleavage-type failure. For the accident case, the predicted failure load for the right rear lug from the PFA is greater than 1.98 times the limit load of the lugs.

  3. 76 FR 69168 - Airworthiness Directives; Airbus Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-11-08

    ... examination of the cracked ribs confirmed that the cracks were the result of pitting corrosion in the forward lug hole. Also on both aeroplanes, medium to heavy corrosion was found in the forward lugs on the... ribs confirmed that the cracks were the result of pitting corrosion in the forward lug hole. Also on...

  4. 7 CFR 29.1165 - Lugs (X Group).

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 7 Agriculture 2 2013-01-01 2013-01-01 false Lugs (X Group). 29.1165 Section 29.1165 Agriculture... INSPECTION Standards Grades § 29.1165 Lugs (X Group). This group consists of leaves normally grown near the bottom of the stalk. Leaves of the X group usually have a blunt tip and open face; they show some ground...

  5. 7 CFR 29.3650 - Lugs (X Group).

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 7 Agriculture 2 2014-01-01 2014-01-01 false Lugs (X Group). 29.3650 Section 29.3650 Agriculture... INSPECTION Standards Grades § 29.3650 Lugs (X Group). This group consists of leaves that normally grow on the lower portions of the stalk. Leaves of the X group usually have a high degree of maturity and show...

  6. 7 CFR 29.3650 - Lugs (X Group).

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 7 Agriculture 2 2012-01-01 2012-01-01 false Lugs (X Group). 29.3650 Section 29.3650 Agriculture... INSPECTION Standards Grades § 29.3650 Lugs (X Group). This group consists of leaves that normally grow on the lower portions of the stalk. Leaves of the X group usually have a high degree of maturity and show...

  7. 7 CFR 29.3650 - Lugs (X Group).

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 7 Agriculture 2 2011-01-01 2011-01-01 false Lugs (X Group). 29.3650 Section 29.3650 Agriculture... INSPECTION Standards Grades § 29.3650 Lugs (X Group). This group consists of leaves that normally grow on the lower portions of the stalk. Leaves of the X group usually have a high degree of maturity and show...

  8. 7 CFR 29.2664 - Lugs (X Group).

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 7 Agriculture 2 2012-01-01 2012-01-01 false Lugs (X Group). 29.2664 Section 29.2664 Agriculture... INSPECTION Standards Grades § 29.2664 Lugs (X Group). This group consists of leaves that normally grow near the bottom of the stalk. Leaves of the X group usually have a high degree of maturity and show ground...

  9. 7 CFR 29.1165 - Lugs (X Group).

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 7 Agriculture 2 2011-01-01 2011-01-01 false Lugs (X Group). 29.1165 Section 29.1165 Agriculture... INSPECTION Standards Grades § 29.1165 Lugs (X Group). This group consists of leaves normally grown near the bottom of the stalk. Leaves of the X group usually have a blunt tip and open face; they show some ground...

  10. 7 CFR 29.2664 - Lugs (X Group).

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 7 Agriculture 2 2013-01-01 2013-01-01 false Lugs (X Group). 29.2664 Section 29.2664 Agriculture... INSPECTION Standards Grades § 29.2664 Lugs (X Group). This group consists of leaves that normally grow near the bottom of the stalk. Leaves of the X group usually have a high degree of maturity and show ground...

  11. 7 CFR 29.3650 - Lugs (X Group).

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... 7 Agriculture 2 2013-01-01 2013-01-01 false Lugs (X Group). 29.3650 Section 29.3650 Agriculture... INSPECTION Standards Grades § 29.3650 Lugs (X Group). This group consists of leaves that normally grow on the lower portions of the stalk. Leaves of the X group usually have a high degree of maturity and show...

  12. 7 CFR 29.2664 - Lugs (X Group).

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 7 Agriculture 2 2011-01-01 2011-01-01 false Lugs (X Group). 29.2664 Section 29.2664 Agriculture... INSPECTION Standards Grades § 29.2664 Lugs (X Group). This group consists of leaves that normally grow near the bottom of the stalk. Leaves of the X group usually have a high degree of maturity and show ground...

  13. 7 CFR 29.1165 - Lugs (X Group).

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 7 Agriculture 2 2014-01-01 2014-01-01 false Lugs (X Group). 29.1165 Section 29.1165 Agriculture... INSPECTION Standards Grades § 29.1165 Lugs (X Group). This group consists of leaves normally grown near the bottom of the stalk. Leaves of the X group usually have a blunt tip and open face; they show some ground...

  14. 7 CFR 29.1165 - Lugs (X Group).

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 2 2010-01-01 2010-01-01 false Lugs (X Group). 29.1165 Section 29.1165 Agriculture... INSPECTION Standards Grades § 29.1165 Lugs (X Group). This group consists of leaves normally grown near the bottom of the stalk. Leaves of the X group usually have a blunt tip and open face; they show some ground...

  15. 7 CFR 29.2664 - Lugs (X Group).

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 2 2010-01-01 2010-01-01 false Lugs (X Group). 29.2664 Section 29.2664 Agriculture... INSPECTION Standards Grades § 29.2664 Lugs (X Group). This group consists of leaves that normally grow near the bottom of the stalk. Leaves of the X group usually have a high degree of maturity and show ground...

  16. 7 CFR 29.3650 - Lugs (X Group).

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 2 2010-01-01 2010-01-01 false Lugs (X Group). 29.3650 Section 29.3650 Agriculture... INSPECTION Standards Grades § 29.3650 Lugs (X Group). This group consists of leaves that normally grow on the lower portions of the stalk. Leaves of the X group usually have a high degree of maturity and show...

  17. 7 CFR 29.2664 - Lugs (X Group).

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... 7 Agriculture 2 2014-01-01 2014-01-01 false Lugs (X Group). 29.2664 Section 29.2664 Agriculture... INSPECTION Standards Grades § 29.2664 Lugs (X Group). This group consists of leaves that normally grow near the bottom of the stalk. Leaves of the X group usually have a high degree of maturity and show ground...

  18. 7 CFR 29.1165 - Lugs (X Group).

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... 7 Agriculture 2 2012-01-01 2012-01-01 false Lugs (X Group). 29.1165 Section 29.1165 Agriculture... INSPECTION Standards Grades § 29.1165 Lugs (X Group). This group consists of leaves normally grown near the bottom of the stalk. Leaves of the X group usually have a blunt tip and open face; they show some ground...

  19. Stress analysis of advanced attack helicopter composite main rotor blade root end lug

    NASA Technical Reports Server (NTRS)

    Baker, D. J.

    1982-01-01

    Stress analysis of the Advanced Attack Helicopter (AAH) composite main rotor blade root end lug is described. The stress concentration factor determined from a finite element analysis is compared to an empirical value used in the lug design. The analysis and test data indicate that the stress concentration is primarily a function of configuration and independent of the range of material properties typical of Kevlar-49/epoxy and glass epoxy.

  20. Coaxial connector for use with printed circuit board edge connector

    DOEpatents

    Howard, Donald R.; MacGill, Robert A.

    1989-01-01

    A coaxial cable connector for interfacing with an edge connector for a printed circuit board whereby a coaxial cable can be interconnected with a printed circuit board through the edge connector. The coaxial connector includes a body having two leg portions extending from one side for receiving the edge connector therebetween, and a tubular portion extending from an opposing side for receiving a coaxial cable. A cavity within the body receives a lug of the edge connector and the center conductor of the coaxial cable. Adjacent lugs of the edge connector can be bend around the edge connector housing to function as spring-loaded contacts for receiving the coaxial connector. The lugs also function to facilitate shielding of the center conductor where fastened to the edge connector lug.

  1. 77 FR 59732 - Airworthiness Directives; Airbus Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-10-01

    ... corrosion and rust traces in the lugs and on the bearing outer surface, discovered visually during scheduled... and rust traces in the lugs and on the bearing outer surface of the nose landing gear (NLG) during...

  2. The fatigue strength of riveted joints and lugs

    NASA Technical Reports Server (NTRS)

    Schijve, J

    1956-01-01

    This report deals with a number of tests on riveted joints and lugs for the primary purpose of comparing the several types of riveted joints and to study the effect of various factors on the fatigue strength of lugs. A check was made to ascertain whether or not an estimate of the fatigue life at a certain loading could be made from the dimensions of the joint and the fatigue data of the unnotched materials. Recommendations are made on the proportioning of joints to obtain better fatigue behavior.

  3. Condensation Testing - Shelters

    DTIC Science & Technology

    2011-12-15

    configured as recommended by the manufacturer. b. Instrument the shelter interior with four (4) temperature sensors (thermocouples, thermistors , etc...the chassis or frame secured by one of the following: spot welded terminal lug, soldering lug, screw, nut, and lockwasher? 32. On

  4. 7. DETAIL VIEW OF ROCKER ARM, SHOWING POCKETS, LUGS, INCLINED ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    7. DETAIL VIEW OF ROCKER ARM, SHOWING POCKETS, LUGS, INCLINED STOPPING BLOCK AT SHOREWARD END OF TRACK GIRDER - Seddon Island Scherzer Rolling Lift Bridge, Spanning Garrison Channel from Tampa to Seddon Island, Tampa, Hillsborough County, FL

  5. THREADED ADAPTOR FOR LUGGED PIPE ENDS

    DOEpatents

    Robb, J.E.

    1962-06-01

    An adaptor is designed for enabling a threaded part to be connected to a member at a region having lugs normally receiving bayonet slots of another part for attachment of the latter. It has been found desirable to replace a closure cap connected in a bayonet joint to the end of a coolant tube containing nuclear- reactor fuel elements, with a threaded valve. An adaptor is used which has J- slots receiving lugs on the end of the reactor tube, a thread for connection with the valve, and gear-tooth section enabling a gear-type of tool to rotate the adaptor to seal the valve to the end of the reactor tube. (AEC)

  6. 33. DETAILS OF SAMPLE SUPPORT FRAME ASSEMLBY, LIFTING LUG, AND ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    33. DETAILS OF SAMPLE SUPPORT FRAME ASSEMLBY, LIFTING LUG, AND SAMPLE CARRIER ROD. F.C. TORKELSON DRAWING NUMBER 842-ARVFS-701-S-5. INEL INDEX CODE NUMBER: 075 0701 60 851 151979. - Idaho National Engineering Laboratory, Advanced Reentry Vehicle Fusing System, Scoville, Butte County, ID

  7. 7 CFR 51.1527 - Standard pack.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... plums or prunes in the top layer of any package shall be reasonably representative in quality and size... minimum diameter, or number of fruit per package, or in accordance with the arrangement of the top layer... peach boxes, lug boxes and small consumer packages. In layer-packed California peach boxes or lug boxes...

  8. 77 FR 58330 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-20

    ... requires repetitive inspections of the aft attach lugs of the elevator tab control mechanisms, and replacement of any discrepant elevator tab control mechanism. Since we issued that AD, Boeing has developed a modification of the aft attach lugs of the elevator tab control mechanisms, which will adequately address the...

  9. Blade retainer assembly

    NASA Technical Reports Server (NTRS)

    Luebering, G. W. (Inventor)

    1977-01-01

    A retaining assembly is provided for locking radially extending blades in a rotor disc associated with a gas turbine engine. The assembly includes a pair of spaced apart lugs axially extending from one side of the disc to form an access gap for insertion of a blade tang into a dovetail slot in the rotor disc. A pair of axially aligned inwardly facing recesses are disposed in the lugs. A retaining member resides in the recesses and extends across the gap to preclude egress of the blade tang from the dovetail slot. The retaining member includes at least one axially extending protrusion adapted to radially overlap and abuttingly engage a radially inwardly facing abutment surface on the lugs.

  10. 77 FR 55773 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-09-11

    ...) inspections for cracking of the left and right rib hinge bearing lugs of the aft face of the center section of... bearing lugs of the aft face of the center section of the horizontal stabilizer; measuring crack length...). Recognition That Reporting of Findings Is Not Required American Airlines stated it recognizes that reporting...

  11. 75 FR 43807 - Airworthiness Directives; Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Model PW-6U Sailplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-07-27

    ...: Cracks on the lug of the rear attachment fitting of the horizontal stabilizer have been detected during..., Kansas City, Missouri 64106; telephone: (816) 329-4130; fax: (816) 329-4090. SUPPLEMENTARY INFORMATION... lug of the rear attachment fitting of the horizontal stabilizer have been detected during the...

  12. D-section structural tubes

    NASA Technical Reports Server (NTRS)

    Leete, II, John H. (Inventor); Skinner, William J. (Inventor)

    1989-01-01

    Structural members for a frame or truss are formed of two substantially identical elongated tubular like members each having a planar extending wall with the tubular members joined together along the planar wall, back to back, and end portions of the joined planar walls form extending lugs. A complementary joint fitting includes a clevis having a slot for receiving the lug.

  13. A user`s guide to LUGSAN II. A computer program to calculate and archive lug and sway brace loads for aircraft-carried stores

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Dunn, W.N.

    1998-03-01

    LUG and Sway brace ANalysis (LUGSAN) II is an analysis and database computer program that is designed to calculate store lug and sway brace loads for aircraft captive carriage. LUGSAN II combines the rigid body dynamics code, SWAY85, with a Macintosh Hypercard database to function both as an analysis and archival system. This report describes the LUGSAN II application program, which operates on the Macintosh System (Hypercard 2.2 or later) and includes function descriptions, layout examples, and sample sessions. Although this report is primarily a user`s manual, a brief overview of the LUGSAN II computer code is included with suggestedmore » resources for programmers.« less

  14. Cryogenic Cam Butterfly Valve

    NASA Technical Reports Server (NTRS)

    McCormack, Kenneth J. (Inventor)

    2016-01-01

    A cryogenic cam butterfly valve has a body that includes an axially extending fluid conduit formed there through. A disc lug is connected to a back side of a valve disc and has a circular bore that receives and is larger than a cam of a cam shaft. The valve disc is rotatable for a quarter turn within the body about a lug axis that is offset from the shaft axis. Actuating the cam shaft in the closing rotational direction first causes the camming side of the cam of the cam shaft to rotate the disc lug and the valve disc a quarter turn from the open position to the closed position. Further actuating causes the camming side of the cam shaft to translate the valve disc into sealed contact with the valve seat. Opening rotational direction of the cam shaft reverses these motions.

  15. Comparison of two computer codes for crack growth analysis: NASCRAC Versus NASA/FLAGRO

    NASA Technical Reports Server (NTRS)

    Stallworth, R.; Meyers, C. A.; Stinson, H. C.

    1989-01-01

    Results are presented from the comparison study of two computer codes for crack growth analysis - NASCRAC and NASA/FLAGRO. The two computer codes gave compatible conservative results when the part through crack analysis solutions were analyzed versus experimental test data. Results showed good correlation between the codes for the through crack at a lug solution. For the through crack at a lug solution, NASA/FLAGRO gave the most conservative results.

  16. Structural health management of aerospace hotspots under fatigue loading

    NASA Astrophysics Data System (ADS)

    Soni, Sunilkumar

    Sustainability and life-cycle assessments of aerospace systems, such as aircraft structures and propulsion systems, represent growing challenges in engineering. Hence, there has been an increasing demand in using structural health monitoring (SHM) techniques for continuous monitoring of these systems in an effort to improve safety and reduce maintenance costs. The current research is part of an ongoing multidisciplinary effort to develop a robust SHM framework resulting in improved models for damage-state awareness and life prediction, and enhancing capability of future aircraft systems. Lug joints, a typical structural hotspot, were chosen as the test article for the current study. The thesis focuses on integrated SHM techniques for damage detection and characterization in lug joints. Piezoelectric wafer sensors (PZTs) are used to generate guided Lamb waves as they can be easily used for onboard applications. Sensor placement in certain regions of a structural component is not feasible due to the inaccessibility of the area to be monitored. Therefore, a virtual sensing concept is introduced to acquire sensor data from finite element (FE) models. A full three dimensional FE analysis of lug joints with piezoelectric transducers, accounting for piezoelectrical-mechanical coupling, was performed in Abaqus and the sensor signals were simulated. These modeled sensors are called virtual sensors. A combination of real data from PZTs and virtual sensing data from FE analysis is used to monitor and detect fatigue damage in aluminum lug joints. Experiments were conducted on lug joints under fatigue loads and sensor signals collected were used to validate the simulated sensor response. An optimal sensor placement methodology for lug joints is developed based on a detection theory framework to maximize the detection rate and minimize the false alarm rate. The placement technique is such that the sensor features can be directly correlated to damage. The technique accounts for a number of factors, such as actuation frequency and strength, minimum damage size, damage detection scheme, material damping, signal to noise ratio and sensing radius. Advanced information processing methodologies are discussed for damage diagnosis. A new, instantaneous approach for damage detection, localization and quantification is proposed for applications to practical problems associated with changes in reference states under different environmental and operational conditions. Such an approach improves feature extraction for state awareness, resulting in robust life prediction capabilities.

  17. Investigation of vibration characteristics of electric motors

    NASA Technical Reports Server (NTRS)

    Bakshis, A. K.; Tamoshyunas, Y. K.

    1973-01-01

    The vibration characteristics of electric motors were analyzed using mathematical statistics methods. The equipment used and the method of conducting the test are described. Curves are developed to show the visualization of the electric motor vibrations in the vertical direction. Additional curves are included to show the amplitude-phase frequency characteristic of dynamic rotor-housing vibrations at the first lug and the same data for the second lug of the electric motor. Mathematical models were created to show the transmission function of the dynamic rotor housing system.

  18. Clamp for use in winding large magnet coils

    DOEpatents

    Brown, Robert L.; Kenney, Walter J.

    1983-01-01

    In one aspect, the invention is a novel arrangement for applying forces to urns of a vertically extending helical coil which is wound about a support. The apparatus includes a first rigid member extending towards the turns. A second rigid member extends transversely from the end of the first and has a vertically extending face provided with a generally straight groove extending transversely of the turns. A longitudinal passage in the first member connects to the groove to form therewith a continuous guideway for rollable articles. A rigid lug longitudinally movable in the groove is provided with a projection which extends out of the groove and beneath the bottom of a selected turn of the coil. A train of rigid, rollable articles is disposed in the guideway inwardly of the lug. Means are provided for applying force to that end of the train which is relatively remote from the lug, to urge the latter against the bottom face of the selected turn. As a result, that turn is moved upward along the face of the support, establishing a selected spacing between that turn and the previously formed turn of the coil. When upward movement of the selected turn stops, the force applied to the lug immediately translates to a force which urges the above-mentioned grooved face against all of the formed turns, thus compressing them against the support. The above-mentioned first and second members are swingably mounted so that they can be temporarily moved out of the winding path, thus permitting continuous winding.

  19. Clamp for use in winding large magnet coils

    DOEpatents

    Brown, R.L.; Kenney, W.J.

    1981-05-05

    In one aspect, the invention is a novel arrangement for applying forces to turns of a vertically extending helical coil which is wound about a support. The apparatus includes a first rigid member extending towards the turns. A second rigid member extends transversely from the end of the first and has a vertically extending face provided with a generally straight groove extending transversely of the turns. A longitudinal passage in the first member connects to the groove to form therewith a continuous guideway for rollable articles. A rigid lug longitudinally movable in the groove is provided with a projection which extends out of the groove and beneath the bottom of a selected turn of the coil. A train of rigid, rollable articles is disposed in the guideway inwardly of the lug. Means are provided for applying force to that end of the train which is relatively remote from the lug, to urge the latter against the bottom face of the selected turn. As a result, that turn is moved upward along the face of the support, establishing a selected spacing between that turn and the previously formed turn of the coil. When upward movement of the selected turn stops, the force applied to the lug immediately translates to a force which urges the above-mentioned grooved face against all of the formed turns, thus compressing them against the support. The above-mentioned first and second members are swingably mounted so that they can be temporarily moved out of the winding path, thus permitting continuous winding.

  20. Don/doff support stand for use with rear entry space suits

    NASA Technical Reports Server (NTRS)

    Kosmo, Joseph J. (Inventor); Tri, Terry O. (Inventor); Spenny, William E. (Inventor); West, Philip R. (Inventor)

    1988-01-01

    A don/doff support stand for use with rear entry space suits is disclosed. The support stand is designed for use in one-g environments; however, certain features of the stand can be used on future spacecraft, lunar, or planetary bases. The present invention has a retainer which receives a protrucing lug fixed on the torso section of the space suit. When the lug is locked in the retainer, the space suit is held in a generally upright position. In a one-g environment a portable ladder is positioned adjacent to the rear entry of the space suit supported by the stand. The astronaut climbs up the ladder and grasps a hand bar assembly positioned above the rear entry. The astronaut then slips his legs through the open rear entry and down into the abdominal portion of the suite. The astronaut then lowers himself fully into the suit. The portable ladder is then removed and the astronaut can close the rear entry door. The lug is then disengaged from the retainer and the astronaut is free to engage in training exercises in the suit. When suit use is over, the astronaut returns to the stand and inserts the lug into the retainer. A technician repositions the ladder. The astronaut opens the rear entry door, grasps the hand bar assembly and does a chin-up to extricate himself from the suit. The astronaut climbs down the movable ladder while the suit is supported by the stand.

  1. Don/Doff support stand for use with rear entry space suits

    NASA Technical Reports Server (NTRS)

    Kosmo, Joseph J. (Inventor); Tri, Terry O. (Inventor); Spenny, William E. (Inventor); West, Philip R. (Inventor)

    1989-01-01

    A don/doff support stand for use with rear entry space suits is disclosed. The support stand is designed for use in one-g environments; however, certain features of the stand can be used on future space-craft, lunar or planetary bases. The present invention has a retainer which receives a protruding lug fixed on the torso section of the space suit. When the lug is locked in the retainer, the space suit is held in a generally upright position. In a one-g environment a portable ladder is positioned adjacent to the rear entry of the space suit supported by the stand. The astronaut climbs up the ladder and grasps a hand bar assembly positioned above the rear entry. The astronaut then slips his legs through the open rear entry and down into the abdominal portion of the suit. The astronaut then lowers himself fully into the suit. The portable ladder is then removed and the astronaut can close the rear entry door. The lug is then disengaged from the retainer and the astronaut is free to engage in training exercises in the suit. When suit use is over, the astronaut returns to the stand and inserts the lug into the retainer. A technician repositions the ladder. The astronaut opens the rear entry door, grasps the hand bar assembly and does a chin-up to extricate himself from the suit. The astronaut climbs down the movable ladder while the suit is supported by the stand.

  2. Reliability of pelvic floor measurements on three- and four-dimensional ultrasound during and after first pregnancy: implications for training.

    PubMed

    van Veelen, G A; Schweitzer, K J; van der Vaart, C H

    2013-11-01

    To evaluate the reliability of measurements of the levator hiatus and levator-urethra gap (LUG) using three/four-dimensional (3D/4D) transperineal ultrasound in women during their first pregnancy and 6 months postpartum, and to assess the learning process for these measurements. An inexperienced observer was taught to perform measurements of the levator hiatus and LUG by an experienced observer. After training, 3D/4D ultrasound volume datasets of 40 women in the first trimester were analyzed by these two observers. Another training session then took place and both observers repeated the analyses of the same volume datasets. Finally, analyses of 40 volume datasets of the women 6 months postpartum were performed by both observers. Intra- and interobserver reliability were determined by intraclass correlation coefficients (ICC) with 95% CIs. For levator hiatal measurements, in the women during their first pregnancy the interobserver reliability was substantial to almost perfect after both the first and second training session (ICC, 0.62-0.83 and 0.71-0.89, respectively, for anteroposterior diameter, transverse diameter and area at rest, on contraction and on Valsalva) and the intraobserver reliability was substantial to almost perfect for both observers. For these measurements performed once the women had delivered, interobserver reliability was moderate to almost perfect. For LUG measurements performed during pregnancy, interobserver reliability was slight to moderate after the first training session (ICC, 0.14-0.54), but improved after the second training session (ICC, 0.38-0.71), and intraobserver reliability was moderate to substantial for the experienced observer and slight to moderate for the inexperienced observer. For these measurements performed when the women had delivered, interobserver reliability was fair to moderate. The levator hiatus and LUG can be measured reliably using 3D/4D ultrasound in primigravid and primiparous women. The technique to measure dimensions of the levator hiatus requires limited teaching, but LUG measurements are more difficult and require more extensive training. Copyright © 2013 ISUOG. Published by John Wiley & Sons Ltd.

  3. RSRM nozzle actuator bracket/lug fracture mechanics qualification test

    NASA Technical Reports Server (NTRS)

    Kelley, Peggy

    1993-01-01

    This is the final report for the actuator bracket/lug fracture mechanics qualification test. The test plan (CTP-0071) outlined a two-phase test program designed to answer questions about the fracture criticality of the redesigned solid rocket motor (RSRM) nozzle actuator bracket. An analysis conducted using the NASA/FLAGRO fracture mechanics computer program indicated that the actuator bracket might be a fracture critical component. In the NASA/FLAGRO analysis, a simple lug model was used to represent the actuator bracket. It was calculated that the bracket would fracture if subjected to an actuator stall load in the presence of a 0.10 in. corner crack at the actuator attachment hole. The 0.10 in. crack size corresponds to the nondestructive inspection detectability limit for the actuator bracket. The inspection method used is the dye penetrant method. The actuator stall load (103,424 lb) is the maximum load which the actuator bracket is required to withstand during motor operation. This testing was designed to establish the accuracy of the analytical model and to directly determine whether the actuator bracket is capable of meeting fracture mechanics safe-life requirements.

  4. Proceedings of the Tri-Service Conference on Corrosion (1987) Held at the Air Force Academy, Colorado on 5-7 May 1987.

    DTIC Science & Technology

    1987-05-01

    j, ’er-,t- -- Case Studies of .- ’." Failures", Proceedinqs, 198O Tri-Ser vice Conference on Corrosion, AFWAL-TR-81- 401(, 1o1. 1, 2’.1-270, (II1). 3...Spiehler, 1981. Gulf of Mexico Study of "v’-. Biofouling on OTEC heat exchanger candidate alloys. Materials Performance 8:16-21. - Little, B. 1980... Case Studies Figure 2 shows the configuration of a straight shank attachment lug without bushing. All lugs, with or without bushing, that were

  5. Wheelspace windage cover plate for turbine

    DOEpatents

    Lathrop, Norman Douglas

    2002-01-01

    Windage cover plates are secured between the wheels and spacer of a turbine rotor to prevent hot flow path gas ingestion into the wheelspace cavities. Each cover plate includes a linear, axially extending body curved circumferentially with a radially outwardly directed wall at one axial end. The wall defines a axially opening recess for receiving a dovetail lug. The cover plate includes an axially extending tongue received in a circumferential groove of the spacer. The cover plate is secured with the tongue in the groove and dovetail lug in the recess. Lap joints between circumferentially adjacent cover plates are provided.

  6. Fatigue Investigation of the E-2B/C Nose Landing Gear

    DTIC Science & Technology

    1975-12-31

    Specimen - Outer Cylinder and Caster Barrel 9 3 E-2B NLG Test Specimen - Drag Brace 10 4 E-2B NLG Drag Brace Attachment Lugs Modification . . 11 5...Attachment Lug Fracture Surface . . 23 ■■■■ ? 16 Tow Link Modification 30 17 Tow Link #2 Failur 31 18 Tow Link #2 Fracture Face 32 19...34-" ’’- .-.„.,.,„...^ ,.., M1| lf^^~i*>-^^-^^ "u- II li ’ 7«™.™»«*" ■ NADC-75369-30 Bach «hock «true assembly consist« of the «xle- caster barrel, outer cylinder

  7. Space probe/satellite ejection apparatus for spacecraft

    NASA Technical Reports Server (NTRS)

    Smyly, H. M.; Miller, C. D.; Cloyd, R. A.; Heller, C. (Inventor)

    1984-01-01

    An ejection apparatus for spinning and propelling objects for ejection from a spacecraft at a desired velocity and rotational speed is discussed. The apparatus includes a launch cradle on which the space object to be ejected rests. The cradle is rotatably supported by a central hub secured to the upper end of the pneumatic cylinder piston shaft. Release mechanisms consisting of a retractable pin and locking lug is utilized to hold the cradle and object to be ejected. The release mechanism has a fixed barrier member which holds the retractable pin in engagement with the locking lug until release by upward movement of the launch cradle beyond the barrier height.

  8. Advanced Life Analysis Methods. Volume 3. Experimental Evaluation of Crack Growth Analysis Methods for Attachment Lugs

    DTIC Science & Technology

    1984-09-17

    hole at an angle to the radial direction. No 6t.ress intensity factors were developed for a non -radial crack. To circumvent non -radial growth, for which...Structural Lugs 10 6.00 TETM TESX, MARI LOCKHEED L𔃼.0 GRUP IIhA AND 2Rii * 2~~~~.0 .RUPINI .01 .05 1 .2 .5. 9 99PROABLTY F*ý,r 1-40 4oprsno R ato nTs rga... controlled and systematically varied. In the fifth column of the table it is shown whether or not the pin is lubricated during testing. Loading directions

  9. The advertisement call of Bokermannohyla flavopicta Leite, Pezzuti & Garcia, 2012 (Anura: Hylidae) from the mountains of Chapada Diamantina, Bahia, Brazil.

    PubMed

    Rocha, Pedro Carvalho; Thompson, Julia Resende; Leite, Felipe Sá Fortes; Garcia, Paulo Christiano De Anchietta

    2016-01-07

    Bokermannohyla Faivovich, Haddad, Garcia, Frost, Campbell & Wheeler (2005) is a Brazilian treefrog genus currently composed of 32 species (Brandão et al. 2012; Leite et al. 2012; Frost 2015). The genus comprehends four, putatively monophyletic, species groups: B. circumdata, B. claresignata, B. martinsi, and B. pseudopseudis (sensu Faivovich et al. 2005). The B. pseudopseudis group includes nine species: B. alvarengai (Bokermann 1956), B. flavopicta Leite et al. 2012, B. ibitiguara (Cardoso 1983), B. itapoty Lugli & Haddad 2006a, B. oxente Lugli & Haddad 2006b, B. pseudopseudis (Miranda-Ribeiro 1937), B. sagarana Leite et al. 2011, B. sapiranga Brandão et al. 2012, and B. saxicola (Bokermann 1964).

  10. Backpack Safety (For Parents)

    MedlinePlus

    ... backaches because they're lugging around their entire locker's worth of books, school supplies, and personal items ... rests with kids: Encourage kids to use their locker or desk often throughout the day instead of ...

  11. 7 CFR 925.215 - Assessment rate.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... AND ORDERS; FRUITS, VEGETABLES, NUTS), DEPARTMENT OF AGRICULTURE GRAPES GROWN IN A DESIGNATED AREA OF... rate of $0.0125 per 18-pound lug is established for grapes grown in a designated area of southeastern...

  12. 7 CFR 925.215 - Assessment rate.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... and Orders; Fruits, Vegetables, Nuts), DEPARTMENT OF AGRICULTURE GRAPES GROWN IN A DESIGNATED AREA OF... rate of $0.01 per 18-pound lug is established for grapes grown in a designated area of southeastern...

  13. 7 CFR 925.215 - Assessment rate.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... and Orders; Fruits, Vegetables, Nuts), DEPARTMENT OF AGRICULTURE GRAPES GROWN IN A DESIGNATED AREA OF... rate of $0.01 per 18-pound lug is established for grapes grown in a designated area of southeastern...

  14. 7 CFR 925.215 - Assessment rate.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... and Orders; Fruits, Vegetables, Nuts), DEPARTMENT OF AGRICULTURE GRAPES GROWN IN A DESIGNATED AREA OF... rate of $0.0125 per 18-pound lug is established for grapes grown in a designated area of southeastern...

  15. 7 CFR 925.215 - Assessment rate.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... AND ORDERS; FRUITS, VEGETABLES, NUTS), DEPARTMENT OF AGRICULTURE GRAPES GROWN IN A DESIGNATED AREA OF... rate of $0.0165 per 18-pound lug is established for grapes grown in a designated area of southeastern...

  16. Meta-Analysis of Cardiac Mortality in Three Cohorts of Carbon Black Production Workers

    PubMed Central

    Morfeld, Peter; Mundt, Kenneth A.; Dell, Linda D.; Sorahan, Tom; McCunney, Robert J.

    2016-01-01

    Epidemiological studies have demonstrated associations between airborne environmental particle exposure and cardiac disease and mortality; however, few have examined such effects from poorly soluble particles of low toxicity such as manufactured carbon black (CB) particles in the work place. We combined standardised mortality ratio (SMR) and Cox proportional hazards results from cohort studies of US, UK and German CB production workers. Under a common protocol, we analysed mortality from all causes, heart disease (HD), ischemic heart disease (IHD) and acute myocardial infarction (AMI). Fixed and random effects (RE) meta-regression models were fit for employment duration, and for overall cumulative and lugged quantitative CB exposure estimates. Full cohort meta-SMRs (RE) were 1.01 (95% confidence interval (CI) 0.79–1.29) for HD; 1.02 (95% CI 0.80–1.30) for IHD, and 1.08 (95% CI 0.74–1.59) for AMI mortality. For all three outcomes, meta-SMRs were heterogeneous, increased with time since first and time since last exposure, and peaked after 25–29 or 10–14 years, respectively. Meta-Cox coefficients showed no association with lugged duration of exposure. A small but imprecise increased AMI mortality risk was suggested for cumulative exposure (RE-hazards ratio (HR) = 1.10 per 100 mg/m3-years; 95% CI 0.92–1.31), but not for lugged exposures. Our results do not demonstrate that airborne CB exposure increases all-cause or cardiac disease mortality. PMID:27005647

  17. 49 CFR 178.356-1 - General requirements.

    Code of Federal Regulations, 2010 CFR

    2010-10-01

    ... filled with a molded-in-place, fire-resistant, phenolic-foam insulation interspersed with wooden members... over 5 gallons capacity must be closed by means of 12-gauge bolted ring with drop forged lugs, one of...

  18. 49 CFR 178.356-1 - General requirements.

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... filled with a molded-in-place, fire-resistant, phenolic-foam insulation interspersed with wooden members... over 5 gallons capacity must be closed by means of 12-gauge bolted ring with drop forged lugs, one of...

  19. 49 CFR 178.356-1 - General requirements.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... filled with a molded-in-place, fire-resistant, phenolic-foam insulation interspersed with wooden members... over 5 gallons capacity must be closed by means of 12-gauge bolted ring with drop forged lugs, one of...

  20. 49 CFR 178.356-1 - General requirements.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... filled with a molded-in-place, fire-resistant, phenolic-foam insulation interspersed with wooden members... over 5 gallons capacity must be closed by means of 12-gauge bolted ring with drop forged lugs, one of...

  1. Universal solar-cell terminal

    NASA Technical Reports Server (NTRS)

    Bashin, S.; Kelley, F. G.

    1977-01-01

    Terminal, which replaces stakes or lugs in conventional design with loop receptacles for wires from cell and harness, uses dissimilar bonding properties (metal-to-glass and/or ceramics) of iron-nickel-cobalt alloy in conjunction with standard termination.

  2. Reactivity control assembly for nuclear reactor

    DOEpatents

    Bollinger, Lawrence R.

    1984-01-01

    Reactivity control assembly for nuclear reactor comprises supports stacked above reactor core for holding control rods. Couplers associated with the supports and a vertically movable drive shaft have lugs at their lower ends for engagement with the supports.

  3. 7 CFR 30.37 - Class 2; fire-cured types and groups.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... REGULATIONS TOBACCO STOCKS AND STANDARDS Classification of Leaf Tobacco Covering Classes, Types and Groups of.... Groups applicable to types 21, 22, and 23: A—Wrappers. B—Heavy Leaf. C—Thin Leaf. X—Lugs. N—Nondescript...

  4. 7 CFR 30.37 - Class 2; fire-cured types and groups.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... REGULATIONS TOBACCO STOCKS AND STANDARDS Classification of Leaf Tobacco Covering Classes, Types and Groups of.... Groups applicable to types 21, 22, and 23: A—Wrappers. B—Heavy Leaf. C—Thin Leaf. X—Lugs. N—Nondescript...

  5. 7 CFR 30.37 - Class 2; fire-cured types and groups.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    ... REGULATIONS TOBACCO STOCKS AND STANDARDS Classification of Leaf Tobacco Covering Classes, Types and Groups of.... Groups applicable to types 21, 22, and 23: A—Wrappers. B—Heavy Leaf. C—Thin Leaf. X—Lugs. N—Nondescript...

  6. 7 CFR 30.37 - Class 2; fire-cured types and groups.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    ... REGULATIONS TOBACCO STOCKS AND STANDARDS Classification of Leaf Tobacco Covering Classes, Types and Groups of.... Groups applicable to types 21, 22, and 23: A—Wrappers. B—Heavy Leaf. C—Thin Leaf. X—Lugs. N—Nondescript...

  7. 7 CFR 30.37 - Class 2; fire-cured types and groups.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    ... REGULATIONS TOBACCO STOCKS AND STANDARDS Classification of Leaf Tobacco Covering Classes, Types and Groups of.... Groups applicable to types 21, 22, and 23: A—Wrappers. B—Heavy Leaf. C—Thin Leaf. X—Lugs. N—Nondescript...

  8. 7 CFR 29.1225 - Key to standard grademarks.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER.... Groups B—Leaf. H—Smoking Leaf. C—Cutters. X—Lugs. P—Primings. M—Mixed Group. N—Nondescript. S—Scrap...

  9. 7 CFR 29.1225 - Key to standard grademarks.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER.... Groups B—Leaf. H—Smoking Leaf. C—Cutters. X—Lugs. P—Primings. M—Mixed Group. N—Nondescript. S—Scrap...

  10. Composite structural materials

    NASA Technical Reports Server (NTRS)

    Ansell, G. S.; Loewy, R. G.; Wiberley, S. E.

    1983-01-01

    Transverse properties of fiber constituents in composites, fatigue in composite materials, matrix dominated properties of high performance composites, numerical investigation of moisture effects, numerical investigation of the micromechanics of composite fracture, advanced analysis methods, compact lug design, and the RP-1 and RP-2 sailplanes projects are discussed.

  11. 7 CFR 29.3182 - Key to standard grademarks.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER.... Groups X—Flyings. C—Lugs or Cutters B—Leaf. T—Tips. M—Mixed. N—Nondescript. S—Scrap. Qualities 1—Choice...

  12. 7 CFR 29.3182 - Key to standard grademarks.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER.... Groups X—Flyings. C—Lugs or Cutters B—Leaf. T—Tips. M—Mixed. N—Nondescript. S—Scrap. Qualities 1—Choice...

  13. Simulator Sickness in the AH-1S (Cobra) Flight Simulator

    DTIC Science & Technology

    1989-09-01

    ADJUSTABLE ARMAMENT BOMB LUG (upper rack use only) AFT ATTACHING POINT SWAY GRACE PAD HANS DEBRIS DIRECTOR ~~ CAPTIVE LOCKINGPI FORWARDHARNESS...Qualification training) Training Stage : Qualification Continuation Refresher AAPART (Check Ride) Mission All rights reserved Essex Corporation 1040 Woodcock Road

  14. Bus Maintenance is a Sound Investment.

    ERIC Educational Resources Information Center

    American School Board Journal, 1981

    1981-01-01

    Preventive school bus maintenance to reduce long-term costs should include daily visual inspections by drivers, frequent checks by mechanics, and comprehensive inspections every 5,000 miles. Mechanics recommend checking tail lights, batteries, brakes, lug nuts, leaf springs, tail pipes, and exhaust pipe hangers. (RW)

  15. 7 CFR 925.160 - Reports.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Reports. 925.160 Section 925.160 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements..., varietal name, shipment destination (city and state), and the number of lugs shipped (pounds). (b) When...

  16. 7 CFR 925.13 - Container.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Container. 925.13 Section 925.13 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements... SOUTHEASTERN CALIFORNIA Definitions § 925.13 Container. Container means any lug, box, bag, crate, carton, or...

  17. 7 CFR 917.12 - Container.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Container. 917.12 Section 917.12 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements... CALIFORNIA Order Regulating Handling Definitions § 917.12 Container. Container means a box, bag, crate, lug...

  18. 7 CFR 916.14 - Container.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Container. 916.14 Section 916.14 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements... Regulating Handling Definitions § 916.14 Container. Container means a box, bag, crate, lug, basket, carton...

  19. 7 CFR 924.17 - Container.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Container. 924.17 Section 924.17 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements... Container. Container means a box, bag, crate, lug, basket, carton, package, or any other type of receptacle...

  20. 7 CFR 29.3031 - Group.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... 7 Agriculture 2 2011-01-01 2011-01-01 false Group. 29.3031 Section 29.3031 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... follows: Flyings (X), Lugs or Cutters (C), Leaf (B), Tips (T), Mixed (M), Nondescript (N), and Scrap (S...

  1. 7 CFR 29.3031 - Group.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 2 2010-01-01 2010-01-01 false Group. 29.3031 Section 29.3031 Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing... follows: Flyings (X), Lugs or Cutters (C), Leaf (B), Tips (T), Mixed (M), Nondescript (N), and Scrap (S...

  2. 7 CFR 920.14 - Container.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... 7 Agriculture 8 2010-01-01 2010-01-01 false Container. 920.14 Section 920.14 Agriculture Regulations of the Department of Agriculture (Continued) AGRICULTURAL MARKETING SERVICE (Marketing Agreements... Definitions § 920.14 Container. Container means a box, bag, crate, lug, basket, carton, package, or any other...

  3. 33 CFR 159.79 - Terminals.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 33 Navigation and Navigable Waters 2 2011-07-01 2011-07-01 false Terminals. 159.79 Section 159.79 Navigation and Navigable Waters COAST GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) POLLUTION MARINE SANITATION DEVICES Design, Construction, and Testing § 159.79 Terminals. Terminals must be solderless lugs...

  4. Development of thermoplastic composite aircraft structures

    NASA Technical Reports Server (NTRS)

    Renieri, Michael P.; Burpo, Steven J.; Roundy, Lance M.; Todd, Stephanie A.; Kim, H. J.

    1992-01-01

    Efforts focused on the use of thermoplastic composite materials in the development of structural details associated with an advanced fighter fuselage section with applicability to transport design. In support of these designs, mechanics developments were conducted in two areas. First, a dissipative strain energy approach to material characterization and failure prediction, developed at the Naval Research Laboratory, was evaluated as a design/analysis tool. Second, a finite element formulation for thick composites was developed and incorporated into a lug analysis method which incorporates pin bending effects. Manufacturing concepts were developed for an upper fuel cell cover. A detailed trade study produced two promising concepts: fiber placement and single-step diaphragm forming. Based on the innovative design/manufacturing concepts for the fuselage section primary structure, elements were designed, fabricated, and structurally tested. These elements focused on key issues such as thick composite lugs and low cost forming of fastenerless, stiffener/moldine concepts. Manufacturing techniques included autoclave consolidation, single diaphragm consolidation (SDCC) and roll-forming.

  5. Precision aligned split V-block

    DOEpatents

    George, Irwin S.

    1984-01-01

    A precision aligned split V-block for holding a workpiece during a milling operation having an expandable frame for allowing various sized workpieces to be accommodated, is easily secured directly to the mill table and having key lugs in one base of the split V-block that assures constant alignment.

  6. Strength Behaviour of Fatigue Cracked Lugs (Festigkeitsverhalten von Rissbehafteten Augenstaeben),

    DTIC Science & Technology

    1981-01-01

    either surface cracks or corner cracks at holes. NASA TN 1)-8244 64 A.F. Grandt Stress intensity factors for some through fracked fastener holes...with Hydropuise L~ngszylinder longitudinal cylinder Druckblversorgung =pressure oil Supply Hydraulikaggregat = hydraulic control unit Fig 7.5 Plan of

  7. 78 FR 15281 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-03-11

    ... horizontal stabilizer. This AD requires repetitive high frequency eddy current (HFEC) inspections for... repetitive high frequency eddy current (HFEC) inspections for cracking of the left and right rib hinge... high frequency eddy current (HFEC) inspection for cracking of the left and right rib hinge bearing lugs...

  8. 49 CFR 178.255-11 - Tank mountings.

    Code of Federal Regulations, 2011 CFR

    2011-10-01

    ... 49 Transportation 3 2011-10-01 2011-10-01 false Tank mountings. 178.255-11 Section 178.255-11... Portable Tanks § 178.255-11 Tank mountings. (a) Tanks shall be designed and fabricated with mountings to... requirement. (b) All tank mountings such as skids, fastenings, brackets, cradles, lifting lugs, etc., intended...

  9. 49 CFR 178.255-11 - Tank mountings.

    Code of Federal Regulations, 2014 CFR

    2014-10-01

    ... 49 Transportation 3 2014-10-01 2014-10-01 false Tank mountings. 178.255-11 Section 178.255-11... Portable Tanks § 178.255-11 Tank mountings. (a) Tanks shall be designed and fabricated with mountings to... requirement. (b) All tank mountings such as skids, fastenings, brackets, cradles, lifting lugs, etc., intended...

  10. 49 CFR 178.255-11 - Tank mountings.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... 49 Transportation 3 2012-10-01 2012-10-01 false Tank mountings. 178.255-11 Section 178.255-11... Portable Tanks § 178.255-11 Tank mountings. (a) Tanks shall be designed and fabricated with mountings to... requirement. (b) All tank mountings such as skids, fastenings, brackets, cradles, lifting lugs, etc., intended...

  11. 49 CFR 178.255-11 - Tank mountings.

    Code of Federal Regulations, 2013 CFR

    2013-10-01

    ... 49 Transportation 3 2013-10-01 2013-10-01 false Tank mountings. 178.255-11 Section 178.255-11... Portable Tanks § 178.255-11 Tank mountings. (a) Tanks shall be designed and fabricated with mountings to... requirement. (b) All tank mountings such as skids, fastenings, brackets, cradles, lifting lugs, etc., intended...

  12. 7 CFR 29.3686 - Key to standard grademarks.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER... 3—Good R—Reddish brown X—Lugs 4—Fair D—Dark brown N—Nondescript 5—Low M—Mixed S—Scrap G—Green [30 FR...

  13. 7 CFR 29.3686 - Key to standard grademarks.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ... Agriculture Regulations of the Department of Agriculture AGRICULTURAL MARKETING SERVICE (Standards, Inspections, Marketing Practices), DEPARTMENT OF AGRICULTURE COMMODITY STANDARDS AND STANDARD CONTAINER... 3—Good R—Reddish brown X—Lugs 4—Fair D—Dark brown N—Nondescript 5—Low M—Mixed S—Scrap G—Green [30 FR...

  14. 29 CFR 1926.754 - Structural steel assembly.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 29 Labor 8 2010-07-01 2010-07-01 false Structural steel assembly. 1926.754 Section 1926.754 Labor... (CONTINUED) SAFETY AND HEALTH REGULATIONS FOR CONSTRUCTION Steel Erection § 1926.754 Structural steel...) Tripping hazards. Shear connectors (such as headed steel studs, steel bars or steel lugs), reinforcing bars...

  15. 29 CFR 1926.754 - Structural steel assembly.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 29 Labor 8 2011-07-01 2011-07-01 false Structural steel assembly. 1926.754 Section 1926.754 Labor... (CONTINUED) SAFETY AND HEALTH REGULATIONS FOR CONSTRUCTION Steel Erection § 1926.754 Structural steel...) Tripping hazards. Shear connectors (such as headed steel studs, steel bars or steel lugs), reinforcing bars...

  16. Supermarket Artists

    ERIC Educational Resources Information Center

    Szekely, George

    2010-01-01

    As soon as they graduate from arm-length viewing in shopping-cart seats, children take off to adventure in aisles, touching just about everything. Kids will pocket fallen signs and lug unusual, empty shelves and packaging materials in hopes of taking them home. Kids recognize and compliment supermarket artists--stock clerks who create container…

  17. 77 FR 45513 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-08-01

    ... prompted by a report of elevator vibration and bearing swage failures. This proposed AD would require, for... aft attach lugs for the elevator tab control mechanism, and replacement if necessary, and for other... elevator tab control mechanism, which could result in elevator and tab vibration. Consequent structural...

  18. Fine gravel controls hydrologic and erodibility responses to trampling disturbance for coarse-textured soils with weak cyanobacterial crusts.

    USDA-ARS?s Scientific Manuscript database

    We compared short-term effects of lug-soled boot trampling disturbance on water infiltration and soil erodibility on coarse-textured soils covered by a mixture of fine gravel and coarse sand over weak cyanobacterially-dominated biological soil crusts. Trampling significantly reduced final infiltrati...

  19. Blends of Crystallizable Polybutadiene Isomers: Compatibilization by Addition of Amorphous Diblock Copolymer

    DTIC Science & Technology

    1991-07-24

    Fourth International Meeting. 2, 898, A. Mangini, ed., Pergamon Press, England, 1962. Morero, D., E. Mantica, and L. Porni , Nuovo Cimento. Sup~pl. 15. 10...311, 1969. Natta G., and P. Corradini, Journal of Polymer Science, 20, 251, 1956. Natta, G., L. Porni , A. Carbonaro, and G. Lugli, Makromolekulare

  20. 29 CFR 1910.213 - Woodworking machinery requirements.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... as to be free from sensible vibration when the largest size tool is mounted and run idle at full... lugs cast on the frame or with an equivalent means to limit the size of the saw blade that can be... in-running rolls at any point. The guard shall be constructed of heavy material, preferably metal...

  1. 29 CFR 1910.213 - Woodworking machinery requirements.

    Code of Federal Regulations, 2013 CFR

    2013-07-01

    ... as to be free from sensible vibration when the largest size tool is mounted and run idle at full... lugs cast on the frame or with an equivalent means to limit the size of the saw blade that can be... in-running rolls at any point. The guard shall be constructed of heavy material, preferably metal...

  2. 29 CFR 1910.213 - Woodworking machinery requirements.

    Code of Federal Regulations, 2014 CFR

    2014-07-01

    ... as to be free from sensible vibration when the largest size tool is mounted and run idle at full... lugs cast on the frame or with an equivalent means to limit the size of the saw blade that can be... in-running rolls at any point. The guard shall be constructed of heavy material, preferably metal...

  3. 29 CFR 1910.213 - Woodworking machinery requirements.

    Code of Federal Regulations, 2012 CFR

    2012-07-01

    ... as to be free from sensible vibration when the largest size tool is mounted and run idle at full... lugs cast on the frame or with an equivalent means to limit the size of the saw blade that can be... in-running rolls at any point. The guard shall be constructed of heavy material, preferably metal...

  4. 29 CFR 1910.213 - Woodworking machinery requirements.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... as to be free from sensible vibration when the largest size tool is mounted and run idle at full... lugs cast on the frame or with an equivalent means to limit the size of the saw blade that can be... in-running rolls at any point. The guard shall be constructed of heavy material, preferably metal...

  5. Thought Textbooks Would All Be Gone by Now? Well, Think Again

    ERIC Educational Resources Information Center

    Trotter, Andrew

    2007-01-01

    Compared with a couple of years ago, children in many California schools have one less tome to lug in their backpacks. Instead of standard textbooks, they use what publisher Pearson Education Inc. calls its "digital path" to California's elementary history and social sciences curriculum. Since the state school board approved it in…

  6. 46 CFR 114.600 - Incorporation by reference.

    Code of Federal Regulations, 2012 CFR

    2012-10-01

    ... Storage Tank Water Heaters 119.320 UL 486A-1992—Wire Connectors and Soldering Lugs For Use With Copper...-93, Standard Specification for Copper-Silicon Alloy Plate, Sheet, Strip, and Rolled Bar for General...) Apparatus 114.400 ASTM B 122/B 122M-95, Standard Specification for Copper-Nickel-Tin Alloy , Copper-Nickel...

  7. 7 CFR 51.2338 - Standard pack.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    .... (c) Boxes, flats, lugs, or cartons: (1) Fruit packed in containers with cell compartments, cardboard fillers or molded trays shall be of proper size for the cells, fillers, or molds in which they are packed...” means the greatest dimension measured at right angles to a line from stem to blossom end. (f) In order...

  8. 7 CFR 51.2338 - Standard pack.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    .... (c) Boxes, flats, lugs, or cartons: (1) Fruit packed in containers with cell compartments, cardboard fillers or molded trays shall be of proper size for the cells, fillers, or molds in which they are packed...” means the greatest dimension measured at right angles to a line from stem to blossom end. (f) In order...

  9. 77 FR 2664 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-01-19

    ...). SUMMARY: We propose to adopt a new airworthiness directive (AD) for all The Boeing Company Model 717-200... the left and right rib hinge bearing lugs of the center section of the horizontal stabilizer; and crack measurement, repairs, and installation of a new center section rib if necessary. We are proposing...

  10. On-line crack prognosis in attachment lug using Lamb wave-deterministic resampling particle filter-based method

    NASA Astrophysics Data System (ADS)

    Yuan, Shenfang; Chen, Jian; Yang, Weibo; Qiu, Lei

    2017-08-01

    Fatigue crack growth prognosis is important for prolonging service time, improving safety, and reducing maintenance cost in many safety-critical systems, such as in aircraft, wind turbines, bridges, and nuclear plants. Combining fatigue crack growth models with the particle filter (PF) method has proved promising to deal with the uncertainties during fatigue crack growth and reach a more accurate prognosis. However, research on prognosis methods integrating on-line crack monitoring with the PF method is still lacking, as well as experimental verifications. Besides, the PF methods adopted so far are almost all sequential importance resampling-based PFs, which usually encounter sample impoverishment problems, and hence performs poorly. To solve these problems, in this paper, the piezoelectric transducers (PZTs)-based active Lamb wave method is adopted for on-line crack monitoring. The deterministic resampling PF (DRPF) is proposed to be used in fatigue crack growth prognosis, which can overcome the sample impoverishment problem. The proposed method is verified through fatigue tests of attachment lugs, which are a kind of important joint component in aerospace systems.

  11. Quick-release connector module

    NASA Technical Reports Server (NTRS)

    Sedig, Albert R. (Inventor)

    1995-01-01

    A multi-bay electrical connector is described, of the type that has a frame (12, FIG. 2 ) with cavities (14) that each holds a separate module 20, which enables quick withdrawal of a single module from the frame and its quick replacement. A lock arm (42) is slidable along a first side (50) of a first cavity, and has at least one lock lug (80). A first module has a barrier part (70) that lies inward of the lock lug, which prevents outward movement of the first module out of the frame cavity. The lock arm can be moved to an unlocked position wherein the barrier part on the module lies inward of a gap (84) in the lock arm to permit the module to be pulled out of the frame cavity and later inserted therein. A latch (54) is slidable on the frame in directions (A, B) perpendicular to the sliding movement of the lock arm, and has an abutment (112, FIG. 5 ) that abuts a shoulder (114) on the lock arm to keep the lock arm in its unlocked position until the latch is released.

  12. Genetic diversity, population structure and subdivision of local Balkan pig breeds in Austria, Croatia, Serbia and Bosnia-Herzegovina and its practical value in conservation programs.

    PubMed

    Druml, Thomas; Salajpal, Kresimir; Dikic, Maria; Urosevic, Miroslav; Grilz-Seger, Gertrud; Baumung, Roswitha

    2012-03-01

    At present the Croatian Turopolje pig population comprises about 157 breeding animals. In Austria, 324 Turopolje pigs originating from six Croatian founder animals are registered. Multiple bottlenecks have occurred in this population, one major one rather recently and several more older and moderate ones. In addition, it has been subdivided into three subpopulations, one in Austria and two in Croatia, with restricted gene flow. These specificities explain the delicate situation of this endangered Croatian lard-type pig breed. In order to identify candidate breeding animals or gene pools for future conservation breeding programs, we studied the genetic diversity and population structure of this breed using microsatellite data from 197 individuals belonging to five different breeds. The genetic diversity of the Turopolje pig is dramatically low with observed heterozygosities values ranging from 0.38 to 0.57. Split into three populations since 1994, two genetic clusters could be identified: one highly conserved Croatian gene pool in Turopoljski Lug and the"Posavina" gene pool mainly present in the Austrian population. The second Croatian subpopulation in Lonjsko Polje in the Posavina region shows a constant gene flow from the Turopoljski Lug animals. One practical conclusion is that it is necessary to develop a "Posavina" boar line to preserve the "Posavina" gene pool and constitute a corresponding population in Croatia. Animals of the highly inbred herd in Turopoljski Lug should not be crossed with animals of other populations since they represent a specific phenotype-genotype combination. However to increase the genetic diversity of this herd, a program to optimize its sex ratio should be carried out, as was done in the Austrian population where the level of heterozygosity has remained moderate despite its heavy bottleneck in 1994. © 2012 Druml et al; licensee BioMed Central Ltd.

  13. 78 FR 28147 - Grapes Grown in Designated Area of Southeastern California; Increased Assessment Rate

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-14

    ... Service 7 CFR Part 925 [Doc. No. AMS-FV-13-0005; FV13-925-1 PR] Grapes Grown in Designated Area of... California Desert Grape Administrative Committee (Committee) for the 2013 and subsequent fiscal periods from $0.0150 to $0.0165 per 18-pound lug of grapes handled. The Committee locally administers the...

  14. 78 FR 6251 - Airworthiness Directives; The Boeing Company Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-01-30

    ... airplanes. This proposed AD was prompted by reports of cracks and heat damage on pivot joint components... proposing this AD to detect and correct heat damage and cracks in the pivot pin, truck beam lugs, and inner... joint components have been found with cracks or heat damage. There have been 11 such findings on Model...

  15. Identification of Selected Child-Resistant Closures (Continuous Thread, Lug-Bayonet, and Snap Closures).

    ERIC Educational Resources Information Center

    Gross, Rosalind L.; White, Harry E.

    This publication describes a selected group of child-resistant closures used in packaging five categories of medicine and household products. The material in the document was collected to train survey personnel to identify closures for a planned household study of the effectiveness of child-resistant packaging. The 39 closures described are of…

  16. 7 CFR 29.1225 - Key to standard grademarks.

    Code of Federal Regulations, 2014 CFR

    2014-01-01

    .... Qualities 1—Choice. 2—Fine. 3—Good. 4—Fair. 5—Low. 6—Poor. Color Symbols L—Lemon. LL—Whitish-lemon. F—Orange.... GK—Green variegated. GG—Gray green. KL—Variegated lemon. KF—Variegated orange. KV—Variegated greenish. KM—Variegated mixed. KD—Variegated dark red. LL—Whitish-lemon. Combination Symbols XL—Lug side. PO...

  17. 7 CFR 29.1225 - Key to standard grademarks.

    Code of Federal Regulations, 2013 CFR

    2013-01-01

    .... Qualities 1—Choice. 2—Fine. 3—Good. 4—Fair. 5—Low. 6—Poor. Color Symbols L—Lemon. LL—Whitish-lemon. F—Orange.... GK—Green variegated. GG—Gray green. KL—Variegated lemon. KF—Variegated orange. KV—Variegated greenish. KM—Variegated mixed. KD—Variegated dark red. LL—Whitish-lemon. Combination Symbols XL—Lug side. PO...

  18. 7 CFR 29.1225 - Key to standard grademarks.

    Code of Federal Regulations, 2012 CFR

    2012-01-01

    .... Qualities 1—Choice. 2—Fine. 3—Good. 4—Fair. 5—Low. 6—Poor. Color Symbols L—Lemon. LL—Whitish-lemon. F—Orange.... GK—Green variegated. GG—Gray green. KL—Variegated lemon. KF—Variegated orange. KV—Variegated greenish. KM—Variegated mixed. KD—Variegated dark red. LL—Whitish-lemon. Combination Symbols XL—Lug side. PO...

  19. Tool for Guiding An Auger

    NASA Technical Reports Server (NTRS)

    Wesselski, C. J.

    1983-01-01

    Auger and Ram have same pitch, which minimizes damage to workpiece and load carried by auger. Auger firmly fastened onto ram shaft by screw and kept from rotating on shaft by slot machined into end of stem and male driving lug that engages slot. Used to install threaded studs in plastic or rubber where impractical to mold them in.

  20. 75 FR 16648 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-02

    .... Subsequent investigation revealed extensive damage to the elevator tab control system. Severe vibration in... and right elevator control tab mechanisms for gaps between the swage ring and the aft attach lug, and... replacing any discrepant elevator tab control mechanism, including performing the detailed inspection on the...

  1. Recreational trampling experiments: Effects of trampler weight and shoe type

    Treesearch

    David N. Cole

    1995-01-01

    A standard protocol for conducting experimental trampling studies was developed by Cole and Bayfield (1993). Two variables that were not standardized in that protocol are the type of shoe worn by tramplers and the weight of tramplers. In a study conducted in four different vegetation types, tramplers wearing lug-soled boots caused significantly more immediate...

  2. 40 CFR 94.107 - Determination of maximum test speed.

    Code of Federal Regulations, 2010 CFR

    2010-07-01

    ... 40 Protection of Environment 20 2010-07-01 2010-07-01 false Determination of maximum test speed... Determination of maximum test speed. (a) Overview. This section specifies how to determine maximum test speed from a lug curve. This maximum test speed is used in §§ 94.105, 94.106, and § 94.109 (including the...

  3. 40 CFR 94.107 - Determination of maximum test speed.

    Code of Federal Regulations, 2011 CFR

    2011-07-01

    ... 40 Protection of Environment 20 2011-07-01 2011-07-01 false Determination of maximum test speed... Determination of maximum test speed. (a) Overview. This section specifies how to determine maximum test speed from a lug curve. This maximum test speed is used in §§ 94.105, 94.106, and § 94.109 (including the...

  4. 77 FR 39184 - Grapes Grown in Designated Area of Southeastern California; Increased Assessment Rate

    Federal Register 2010, 2011, 2012, 2013, 2014

    2012-07-02

    ... Service 7 CFR Part 925 [Doc. No. AMS-FV-11-0090; FV12-925-1 PR] Grapes Grown in Designated Area of... Grape Administrative Committee (Committee) for the 2012 and subsequent fiscal periods from $0.0125 to $0.0150 per 18- pound lug of grapes handled. The Committee locally administers the marketing order, which...

  5. 76 FR 7119 - Grapes Grown in Designated Area of Southeastern California; Increased Assessment Rate

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-02-09

    ... Service 7 CFR Part 925 [Doc. No. AMS-FV-10-0104; FV11-925-1 PR] Grapes Grown in Designated Area of... Grape Administrative Committee (Committee) for the 2011 and subsequent fiscal periods from $0.01 to $0.0125 per 18- pound lug of grapes handled. The Committee locally administers the marketing order, which...

  6. 7 CFR 917.442 - California Peach Container and Pack Regulation.

    Code of Federal Regulations, 2011 CFR

    2011-01-01

    ...) Each No. 22E standard lug box of loose-filled peaches shall bear on one outside end, in plain sight and... peaches in any such volume-filled container need only be filled to within one-inch of the top of the container. (2) Each package or container of peaches shall bear, on one outside end in plain sight and in...

  7. 7 CFR 917.442 - California Peach Container and Pack Regulation.

    Code of Federal Regulations, 2010 CFR

    2010-01-01

    ...) Each No. 22E standard lug box of loose-filled peaches shall bear on one outside end, in plain sight and... peaches in any such volume-filled container need only be filled to within one-inch of the top of the container. (2) Each package or container of peaches shall bear, on one outside end in plain sight and in...

  8. 76 FR 430 - Airworthiness Directives; The Boeing Company Model MD-90-30 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-01-05

    ... (FAA), DOT. ACTION: Final rule. SUMMARY: We are adopting a new airworthiness directive (AD) for the... the hinge bearing lugs of the left and right sides of the center section ribs of the horizontal... cracks found on either the left or right (or in one case, both) sides of the center section ribs of the...

  9. 75 FR 60665 - Airworthiness Directives; McDonnell Douglas Corporation Model MD-90-30 Airplanes

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-10-01

    ... proposed rulemaking (NPRM). SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Model... for cracking on the hinge bearing lugs of the left and right sides of the center section ribs of the... results from reports of cracks found on either the left or right (or in one case, both) sides of the...

  10. 78 FR 32632 - 36(b)(1) Arms Sales Notification

    Federal Register 2010, 2011, 2012, 2013, 2014

    2013-05-31

    ... low-drag training bombs, 240 MK-82 inert low-drag general purpose bombs, 90 GBU-12 inert laser-guided bombs, 60-GBU-38 inert GPS guided bombs, 120,000 PGU-27 inert training rounds, pilot training, JP- 8.../BBU-35B Training Chaff, 3,750 BDU-33D/B w/lugs/Mk4 spot low-drag training bombs, 240 MK-82 inert low...

  11. 76 FR 15802 - Airworthiness Directives; Eurocopter France (Eurocopter) Model EC130 B4 Helicopters

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-03-22

    ... in insert D of Figure 5 of the EASB, and determine if it is covered with heat shrink, P/N... shown in insert D of Figure 5 or the attachment screw is not covered with heat shrink, modify the.... Figure 5 of the EASB does not show the heat shrink installed for clarity of screw head and lug detail. (3...

  12. Telescoping columns. [parabolic antenna support

    NASA Technical Reports Server (NTRS)

    Mazur, J. T. (Inventor)

    1980-01-01

    An extendable column is described which consists of several axially elongated rigid structural sections nested within one another. Each section includes a number of rotatably attached screws running along its length. The next inner section includes threaded lugs oriented to threadingly engage the screws. The column is extended or retracted upon rotation of the screws. The screws of each section are selectively rotated by a motor and an engagement mechanism.

  13. Self-Metric Software. Volume I. Summary of Technical Progress.

    DTIC Science & Technology

    1980-04-01

    Development: A CSDL Project History, RADC-TR-77-213, pp. 33-41. A-42186. [3] Goodenough, J. B. and Zara , R. V., "The Effect of Software Structure on Software...1979. **Visiting assistant professor. 99 MISION Of Rome Air Devlopmnt Centfr RWV pta"aa nd eXgdatAA ’~AW&W4 dwveput, ’t* &a -a # "*ate 4UZtLug ~W~A~n

  14. High-Capacity Heat-Pipe Evaporator

    NASA Technical Reports Server (NTRS)

    Oren, J. A.; Duschatko, R. J.; Voss, F. E.; Sauer, L. W.

    1989-01-01

    Heat pipe with cylindrical heat-input surface has higher contact thermal conductance than one with usual flat surface. Cylindrical heat absorber promotes nearly uniform flow of heat into pipe at all places around periphery of pipe, helps eliminate hotspots on heat source. Lugs in aluminum pipe carry heat from outer surface to liquid oozing from capillaries of wick. Liquid absorbs heat, evaporates, and passes out of evaporator through interlug passages.

  15. Beyond the Degree Checklist: What's the Real Point of College?

    ERIC Educational Resources Information Center

    Demetriou, Cynthia

    2007-01-01

    Natasha is a nursing student with a 4.0 grade point average, a first-generation East Indian American, and the first woman in her family to go to college. Lugging a twenty-five-pound book bag of texts that cause her slight frame to slump forward under the weight, she carries a far heavier burden of familial expectation and pride. She has expressed…

  16. 75 FR 21499 - Airworthiness Directives; The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2010-04-26

    ...;Prices of new books are listed in the first FEDERAL REGISTER issue of each #0;week. #0; #0; #0; #0;#0... currently requires doing a detailed inspection of the inboard and outboard aft attach lugs of the left and... replacement part before and after installation. For certain airplanes, this new AD adds improved repetitive...

  17. OSA Proceedings on Picosecond Electronics and Optoelectronics. Volume 4

    DTIC Science & Technology

    1989-01-01

    Weisbuch, and G. A. Mourou vi Optical Phonon-Assisted Tunneling in Double Quantum - Well Structures ........ 111 Y Oberli, Jagdeep Shah, T. C. Damen, R. F...GaAs Quantum Wells During Photoexcitation .......................................... 158 Stephen M. Goodnick and Paolo Lugli Phonons and Phonon...246 R. A. Buhnnan Optical Detection of Resonant Tunneling of Electrons in Quantum Wells ........ 247 G. Livescu, A. M, Fox, T. Sizer, W. H. Knox, and

  18. Improving the Accuracy of Structural Fatigue Life Tracking Through Dynamic Strain Sensor Calibration

    DTIC Science & Technology

    2011-09-01

    strength corrosion resistant 7075 -T6 alloy, and included hinge lugs, a bulkhead, spars, and wing skins that were fastened together using welds, rivets...release, distribution unlimited 13. SUPPLEMENTARY NOTES See also ADA580921. International Workshop on Structural Health Monitoring: From Condition -based...greater than 10% under the same loading conditions [1]. These differences must be accounted for to have acceptable accuracy levels in the ultimate

  19. 76 FR 66620 - Airworthiness Directives; Bombardier, Inc. Model CL-215-1A10, CL-215-6B11 (CL-215T Variant), and...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-10-27

    ... effective date of this AD: Perform an in situ eddy current inspection for cracks on the forward lug of the...-6B11 (CL-415 Variant) airplanes). Thereafter, repeat the in situ eddy current inspection at intervals not to exceed 165 land landings. (2) If no crack is found: Repeat the in situ eddy current inspection...

  20. Clonidine and Cortical Plasticity: Possible Evidence for Noradrenergic Involvement.

    DTIC Science & Technology

    1984-10-31

    Recording, MHPG, Development of CNS, Plasticity. INTRODUCTION Temporary closure of one eye for even a short duration during a three week to three...bottom line shows the daily schedule of injections along with the cycle of general illumination in the colony. EiLug.2- Composite ocular dominance...Neureaci., 4 (1984) 1354. 1360. 15. DEGRELL, I., VENNER , K., KUMMER, P., and STOCK, G., Monoamine metabolites in the CSF of conscious unrestrained cats

  1. An Amoeba/Zoozanthellae Consortium as a Model System for Animal/Algal Symbiosis

    DTIC Science & Technology

    1991-06-18

    extensive multiple fission of Morph-1 cells. Morphology-V: Minigiants - 15-40 microns, complex net-like morphology resulted from fussion of mini oells...seaweeds and sea water (1:1) and autoclaved (20 minutes, 120aC, 250 psi). Nuclear staining: For staining the nuclei, cells were allowed to attach and...water were added (lug/ml) and the amoebae were observed under a fluorescent microscope. Nuclear stains penetrated fixed cells easily and brightly

  2. Dynamic Testing with the NSWC Three-Degree-of-Freedom Gas Bearing

    DTIC Science & Technology

    1982-03-08

    aerodynamic effects caused by the rate of change of angular variables. The three- degree-of-freedom gas bearing support was designed to permit the...Because the model is spinning, a mechanical Initiator woild be unduly complicated. The air jet has been found to be en entirely reliable and effective ...used for all data reduction. The only other diff 1- culty experienced was binding (intermittent stator/ rotor contact) Ln the gas bear- * Lug after

  3. Fractographic Examination of the Vertical Stabilizer and Rudder from American Airlines Flight 587

    NASA Technical Reports Server (NTRS)

    Fox, Matthew R.; Schultheisz, Carl R.; Reeder, James R.

    2005-01-01

    The first major structural component failure of a composite part on a commercial airplane occurred during the crash of American Airlines Flight 587. The fractured composite lugs that attached the vertical stabilizer to the aircraft tail and the fractured composite honeycomb rudder were examined as part of the National Transportation Safety Board investigation of the accident. In this paper the composite fractures are described and the resulting clues to the failure events are discussed.

  4. Remote Munitions Deployment from an Unmanned Ground Vehicle

    DTIC Science & Technology

    2011-08-09

    pack in a series of toe lugs. Then the rear of the pack is pushed downward over a novel spring-loaded latch /release mechanism, remaining locked in...Mason, Patrick R. Griffin, Charles E. Dean Page 4 of 5 UNCLASSIFIED developments and testing, it is not secured by a latch /release mechanism...However, the locating tabs act to wedge the pack in place while still allowing it to pull free during launch. Figure 6: Munitions secured and

  5. Load Lugging Locomotion: Lessons from Indigenous People, Rhino Beetles, and Wallabies

    DTIC Science & Technology

    2001-05-01

    they consume metabolic energy at the same rate! Even hopping at a 4-minute mile pace, kangaroos are only at about a third of their aerobic capacity...carried for free. However, there is not a clear link between the mechanical work performed in walking and the metabolic cost. Rhinoceros beetles are...more cheaply. But kangaroos and wallabies can use internal springs to save energy during their hopping gait and to carry loads in their pouches. These

  6. 76 FR 52215 - Airworthiness Directives; General Electric Company CF34-10E2A1; CF34-10E5; CF34-10E5A1; CF34-10E6...

    Federal Register 2010, 2011, 2012, 2013, 2014

    2011-08-22

    ...; CF34-10E7; and CF34- 10E7-B Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION... cracked at the attachment lugs. We are issuing this AD to prevent high-cycle fatigue cracking of the fan..., uncontained failure of the engine, and damage to the airplane. DATES: This AD is effective September 26, 2011...

  7. Deception Algorithm. Appendices

    DTIC Science & Technology

    1994-06-30

    NOT. THE RAIN AND MUD MADE QUITE SLIPPERY. COULDHAVE BEEN QUITE A FEW INJURIES WHEN LUGGING THE DECOY AROUND. 1111 37106 HF7A HFCMT IN MOPP4 IT WAS... 10 TIMES. 1009 35115 HF5A FFCMT THE TARGET BACKGROUND HELPED GIVE AWAY THE DECOYS BECAUSE THEY WERE PUT UP ON THE SIDE OF A HILL. COLOR WAS DARKER...FFENGCMT I ENGAGED TARGETS THAT I THOUGHT WERE DECOYS APPROXIMATELY 10 TIMES BECAUSE OF RANGE TO TARGET. I COULD NOT ID MOST OF THE TIME AT NIGHT AT LONG

  8. Fatigue Testing of Vampire Wings,

    DTIC Science & Technology

    1979-06-01

    Fork End Upper (Threaded) Lug 2 Lower Root End Filling (R.E.F.) Through Inboard 8 mm (?4 in.) Dia . Bolt Holes. STA.747 (Fig.15) 3 Main Spar Assembl’ at...AD-AOA9 402 AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA) F/G 1/ 3 FATIGUE TESTING OF VAMPIRE WINGS.(U) JUN 79 R A BRUTON. C A PATCHING...Number: (c) Summary in Isolation: ARL-Struc.-Report-378 Unclassified 3 . Title: FATIGUE TESTING OF VAMPIRE WINGS 4. Personal Author(s): 5. Document Date

  9. Advanced Metallic Air Vehicle Structure Program

    DTIC Science & Technology

    1974-06-01

    soapstone line around the periphery of the lower plate from XFO.00 to the outboard edge using edge of MSLO X7224175 as guide. Remove MSLO X7224175. D...hole in the lug reinforcement plates). Make soapstone line to edge of MSLO to denote periphery of cutouts. E. Relocate MSLO X7224175 on opposite end of...of plate). G. Drill .50 diameter holes (10) using the Bux- Magnetic drill unit. See MAP-I-3 for approximate locations of these start and stop holes. A 1

  10. Nondestructive Evaluation (NDE) Capabilities Data Book (3rd Edition)

    DTIC Science & Technology

    1997-11-01

    include: 4340 Steel Flat Plate Panels Bolt Holes in i85 Scvcnth Stage Compressor Disks Visual Inspection of Fatigue Cracks in Inconel 718 and HaynEs 188...safety engineer * The maintenance engineer * Thc manufacturing / production process engineer • The liaison (rework and repair) engineer a ’[ lhc life...TC03: Through crnck from an offset hole in a plate TC04: Through crack from hole in a lug TC05: Through crack from hole in plate with a row of holcs

  11. Tumor Suppressor Activity of the EphB2 Receptor in Prostate Cancer

    DTIC Science & Technology

    2007-11-01

    S, Chen Y, Elkahloun A , Basik M, Bova GS, Bubendorf L, Lugli A , Sauter G, Schleutker J , Ozcelik H, Elowe S, Pawson T, Trent JM, Carpten JD...Collins FS, Mousses S, Bailey-Wilson J , Furbert-Harris P, Dunston G, Powell IJ, Carpten JD (2006) A common nonsense mutation in EphB2 is...associated with prostate cancer risk in African American men with a positive family history. J Med Genet 43:507-511. Knudsen BS, Miranti CK (2006) The impact

  12. 18. Photographic copy of photograph, dated 20 April 1971 (original ...

    Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey

    18. Photographic copy of photograph, dated 20 April 1971 (original print in possession of CSSD-HO, Huntsville, AL). Photographer unknown. View of missile site control building interior. At the interior of the turret, one can see the inspection fixture (furnished by the weapon system contractor) being installed on the antenna array support ring. This fixture was used to check the locations of the tapped holes through 36 shear key lugs - Stanley R. Mickelsen Safeguard Complex, Missile Site Control Building, Northeast of Tactical Road; southeast of Tactical Road South, Nekoma, Cavalier County, ND

  13. Materials Examination of the Vertical Stabilizer from American Airlines Flight 587

    NASA Technical Reports Server (NTRS)

    Fox, Matthew R.; Schultheisz, Carl R.; Reeder, James R.; Jensen, Brian J.

    2005-01-01

    The first in-flight failure of a primary structural component made from composite material on a commercial airplane led to the crash of American Airlines Flight 587. As part of the National Transportation Safety Board investigation of the accident, the composite materials of the vertical stabilizer were tested, microstructure was analyzed, and fractured composite lugs that attached the vertical stabilizer to the aircraft tail were examined. In this paper the materials testing and analysis is presented, composite fractures are described, and the resulting clues to the failure events are discussed.

  14. Progress on S53 for Rotary Gear Actuators

    DTIC Science & Technology

    2008-02-01

    materials MP35N Ni alloy rods HP-9-4-30 or 4340 high strength steel gears (Cd plated) 17 - 4PH stainless bushings Ti wing spar Bad galvanic couples...Bushings: 17 - 4PH in Ti spar MP35N in gear 6 Galvanic corrosion of current system 7 Extent of the problem This is a problem with all F-18 lugs Matter...Titanium plate with 17 - 4PH bush – also refurbished from previous trials • Gears made from HP9-4-30 or S53 with MP35N bushes STREAMLINED CORROSION TESTING

  15. Exploratory development of a twin-spool turbocharger for a high-output diesel engine. Final report, September 1983-June 1986

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Hess, R.; King, J.F.; Harp, J.L.

    1986-08-01

    The analysis, design, fabrication, and experimental testing of a twin-spool turbocharger was conducted for the Cummins NTC-475 diesel engine. Two major designs of the twin-spool turbocharger were fabricated and tested: 1) Compact design, concentric shaft-to-shaft bearing coupled turbocharger incorporating a) split 40/sup 0/ backswept impeller, b) split AiResearch Ti8A85 turbine rotor, c) adjustable vaned compressor diffuser, and d) nozzleless AiResearch turbine (volute) housing; and 2) Independently supported (shafts dynamically de-coupled) concentric shaft design incorporating a) separate structures for bearing support of the inner shaft b) split 25/sup 0/ backswept compressor impeller, c) split T18A40/Ti8A85 turbine rotor/exducer combination, and d) dividedmore » volute, adjustable-nozzle turbine housing. While bench tests were performed on both designs, engine testing was successfully carried out using the latter designs. Tests indicated that the second twin-spool configuration gave performance comparable to the originally equipped two-stage turbocharger system of the NTC-475 diesel engine (rated BHP of 425 hp at 2100 RPM, best BSFC of 0.35 at engine lug) with the added benefit of extending engine lugging range to 1200 RPM (from 1300 RPM, as originally equipped). This configuration gave peak compressor efficiency of about 75% and peak turbine efficiency of about 80%, both attributed to the reduction inducer angle of attack and exducer exit swirl angle made possible by the twin-spool concept.« less

  16. Experimental Validation of a Differential Variational Inequality-Based Approach for Handling Friction and Contact in Vehicle

    DTIC Science & Technology

    2015-11-20

    drawbar pull , wheel torque, and sinkage were measured for a lug-less rigid wheel for several slip cases and loading scenarios. The wheel used in this...0.6, µ =0.5, h =1× 10−3 seconds, τ =5×10−2 N. The quantitative results of this study are summarized in Figs. 11 through 13 for the drawbar pull , torque...and sinkage, respectively. It can be seen that as the slip of the wheel increases, the drawbar pull , torque, and sinkage also increase and the

  17. Temporal Clustering in the Multi-Target Tracking Environment

    DTIC Science & Technology

    1988-08-01

    UNLASS IliED % ,, SECURITY CLASSIFICATION OF THIS PAGE (When Data Entered)_ REPORT DOCUMENTATION PAGE BF READ INSTRUCTIONS6. PEFORE COMPLETING FORM...1. REPORT NUMBER (. )OVT ACCESSION No. 3. RE-Ur-’SAFIT/CI/NR 88- 1 ? ,7 1 11 - _t tA Jr TITLE (and Subtitle) S. TYPE OF REPORT A PERIOD COVEREDTLMfP6...AL C405TEW .GI )K T 4 MULT)- F11M9THESI I, TiNtLqET TOLFNCK lUG 6.mVjllop,3MrJT TEI ~6. PERFORMING O-4O. REPORT hUMBER AU THOR(s) 8. CONTRACT OR

  18. Composite structural materials

    NASA Technical Reports Server (NTRS)

    Ansell, G. S.; Loewy, R. G.; Wiberley, S. E.

    1983-01-01

    Progress and plans are reported for investigations of: (1) the mechanical properties of high performance carbon fibers; (2) fatigue in composite materials; (3) moisture and temperature effects on the mechanical properties of graphite-epoxy laminates; (4) the theory of inhomogeneous swelling in epoxy resin; (5) numerical studies of the micromechanics of composite fracture; (6) free edge failures of composite laminates; (7) analysis of unbalanced laminates; (8) compact lug design; (9) quantification of Saint-Venant's principles for a general prismatic member; (10) variation of resin properties through the thickness of cured samples; and (11) the wing fuselage ensemble of the RP-1 and RP-2 sailplanes.

  19. Operations Charioteer, Musketeer, Touchstone, Cornerstone, Aqueduct, Sculpin and Julin. Tests Mill Yard, Diamond Beech, Mighty Oak, Middle Note Mission Ghost, Mission Cyber, Misty Echo, Disko Elm, Mineral Quarry, Distant Zenith, Diamond Fortune, and Hunters Trophy

    DTIC Science & Technology

    1999-05-01

    2l.SU -Wf6e:uJfr-02tSU -V 69E ;W 9-2l IS« 0VS9 v 6se :w e"g(HSH ttWS:uJB-86SU ¥0l-8:uJ9"fr6SUOVW WW2 :lug-98SU U68l-:ujg-,£SSH — —VZL-VU61ZSU...and JAYCOR conducted infrared window material optical properties experiments; Lawrence Livermore National Laboratory (LLNL) conducted 146 device

  20. Mass Spectral Investigation on Toxins. I. Isolation, Purification, and Characterization of Hepatotoxins from Freshwater Blue-Green Algae (Cyanobacteria) by High-Performance Liquid Chromatography and Fast Atom Bombardment Mass Spectrometric Techniques.

    DTIC Science & Technology

    1986-09-01

    analysis ’" methods in environmental samples. The hepatotoxins from laboratory cultures of M. aeruginosa Strain 7820,15 Anabena flos- aguae (A. 4flos...flos- aguae S-23-g-1l (8 lug) F1 The results from the amino acid analysis using the Llqui-Mat Analyzer are listed in Table 2. The elution times of the...Runnegar, M.T.C., and Huynh, V.L. Effec- tiveness of Activated Carbon in the Removal of Algal Toxin from Potable Water Supplies: A Pilot Plant

  1. Quick-Connect Nut

    NASA Technical Reports Server (NTRS)

    1999-01-01

    Marshall Space Flight Center (MSFC) has developed a specially-designed nut, called the Quick-Connect Nut, for quick and easy assembly of components in the harsh environment of space, as in assembly of International Space Station. The design permits nuts to be installed simply by pushing them onto standard bolts, then giving a quick twist. To remove, they are unscrewed like conventional nuts. Possible applications include the mining industry for erecting support barriers, assembling underwater oil drilling platforms, fire-fighting equipment, scaffolding, assembly-line machinery, industrial cranes, and even changing lug nuts on race cars. The speed of assembly can make the difference between life and death in different aspects of life on Earth.

  2. Word Frequency Analysis MOS: 11B. Skill Levels 1 & 2.

    DTIC Science & Technology

    1981-05-01

    aYNPENT 20 EXT’ ACTYR 2U FAR 20 FIGER - 20 FULLY .20 HANUS 20 HOURS 20 IDENTIFICA’PIDN 20 INS TROCYIONS. ~ 20 LAS ! 20_. L IFTI1G C 20 -LIVITE.- 20 LUG2...PRIMER t I$ pAG .. . .Ib . EL~S ...... 1 .SECTRS -.. .18 SHIFT I+.~r ____ 0S SPE 18m0 SNE.SPITI STATIONARY 18 TAP* 0~ TES!EO 18 TIGNTEV lb TISSLE la TREE...I’SO a INS.UCT!ONS b KILL S LANE -7 S Aphil 1 LOE S LEADERSHIP S LETTER *LIMIT......... ! LIPS ... . LIST .. LISTEN *(ITiFx 8 LUGb Loup I e4hr.AlIt

  3. Benefit from NASA

    NASA Image and Video Library

    1999-10-12

    Marshall Space Flight Center (MSFC) has developed a specially-designed nut, called the Quick-Connect Nut, for quick and easy assembly of components in the harsh environment of space, as in assembly of International Space Station. The design permits nuts to be installed simply by pushing them onto standard bolts, then giving a quick twist. To remove, they are unscrewed like conventional nuts. Possible applications include the mining industry for erecting support barriers, assembling underwater oil drilling platforms, fire-fighting equipment, scaffolding, assembly-line machinery, industrial cranes, and even changing lug nuts on race cars. The speed of assembly can make the difference between life and death in different aspects of life on Earth.

  4. CRUCIBLE LINING METHOD

    DOEpatents

    Bone, W.H.; Schmidt, W.W.

    1958-11-01

    A method is presented for forming refractory liners in cylindrical reaction vessels used for the reductlon of uranium tetrafluoride to metallic uranium. A preliminary form, having positioning lugs attached thereto, is inserted into the reaction vessel and the refractory powder, usually CaO, is put in the annular space between the form and the inner wall of the reaction vessel. A jolting table is used to compact this charge of liner material ln place, and after thls has been done, the preliminary form is removed and the flnal form or plug is lnserted without disturbing the partially completed lining. The remainder of the lining charge is then introduced and compacted by jolting, after which the form is removed.

  5. Finite element mesh refinement criteria for stress analysis

    NASA Technical Reports Server (NTRS)

    Kittur, Madan G.; Huston, Ronald L.

    1990-01-01

    This paper discusses procedures for finite-element mesh selection and refinement. The objective is to improve accuracy. The procedures are based on (1) the minimization of the stiffness matrix race (optimizing node location); (2) the use of h-version refinement (rezoning, element size reduction, and increasing the number of elements); and (3) the use of p-version refinement (increasing the order of polynomial approximation of the elements). A step-by-step procedure of mesh selection, improvement, and refinement is presented. The criteria for 'goodness' of a mesh are based on strain energy, displacement, and stress values at selected critical points of a structure. An analysis of an aircraft lug problem is presented as an example.

  6. Mass loss of a TEOS-coated, reinforced carbon-carbon composite subjected to a simulted shuttle entry environment

    NASA Technical Reports Server (NTRS)

    Stroud, C. W.; Rummler, D. R.

    1980-01-01

    Coated, reinforced carbon-carbon (RCC) is used for the leading edges of the space shuttle. The mass loss characteristics of RCC specimens coated with tetraethyl orthosilicate (TEOS) were determine for conditions which simulated the environment expected at the lug attachment area of the leading edge. Mission simulation included simultaneous application of load, temperature, and oxygen partial pressure. Maximum specimen temperature was 900 K (1160 F). Specimens were exposed for up to 80 simulated missions. Stress levels up to 6.8 MPa (980 psi) did not significantly affect the mass loss characteristics of the TEOS-coated RCC material. Mass loss was correlated with the bulk density of the specimens.

  7. Monitoring of bolted joints using piezoelectric active-sensing for aerospace applications

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Park, Gyuhae; Farrar, Charles R; Park, Chan - Yik

    2010-01-01

    This paper is a report of an initial investigation into tracking and monitoring the integrity of bolted joints using piezoelectric active-sensors. The target application of this study is a fitting lug assembly of unmanned aerial vehicles (UAVs), where a composite wing is mounted to a UAV fuselage. The SHM methods deployed in this study are impedance-based SHM techniques, time-series analysis, and high-frequency response functions measured by piezoelectric active-sensors. Different types of simulated damage are introduced into the structure, and the capability of each technique is examined and compared. Additional considerations encountered in this initial investigation are made to guide furthermore » thorough research required for the successful field deployment of this technology.« less

  8. Turbine airfoil fabricated from tapered extrusions

    DOEpatents

    Marra, John J

    2013-07-16

    An airfoil (30) and fabrication process for turbine blades with cooling channels (26). Tapered tubes (32A-32D) are bonded together in a parallel sequence, forming a leading edge (21), a trailing edge (22), and pressure and suction side walls (23, 24) connected by internal ribs (25). The tapered tubes may be extruded without camber to simplify the extrusion process, then bonded along matching surfaces (34), forming a non-cambered airfoil (28), which may be cambered in a hot forming process and cut (48) to length. The tubes may have tapered walls that are thinner at the blade tip (T1) than at the base (T2), reducing mass. A cap (50) may be attached to the blade tip. A mounting lug (58) may be forged (60) on the airfoil base and then machined, completing the blade for mounting in a turbine rotor disk.

  9. Advanced Main Combustion Chamber structural jacket strength analysis

    NASA Astrophysics Data System (ADS)

    Johnston, L. M.; Perkins, L. A.; Denniston, C. L.; Price, J. M.

    1993-04-01

    The structural analysis of the Advanced Main Combustion Chamber (AMCC) is presented. The AMCC is an advanced fabrication concept of the Space Shuttle Main Engine main combustion chamber (MCC). Reduced cost and fabrication time of up to 75 percent were the goals of the AMCC with cast jacket with vacuum plasma sprayed or platelet liner. Since the cast material for the AMCC is much weaker than the wrought material for the MCC, the AMCC is heavier and strength margins much lower in some areas. Proven hand solutions were used to size the manifolds cutout tee areas for combined pressure and applied loads. Detailed finite element strength analyses were used to size the manifolds, longitudinal ribs, and jacket for combined pressure and applied local loads. The design of the gimbal actuator strut attachment lugs were determined by finite element analyses and hand solutions.

  10. Advertisement call and morphological variation of the poorly known and endemic Bokermannohyla juiju Faivovich, Lugli, Lourenço and Haddad, 2009 (Anura: Hylidae) from Central Bahia, Brazil.

    PubMed

    Taucce, Pedro P G; Pinheiro, Paulo D P; Leite, Felipe S F; Garcia, Paulo C A

    2015-02-02

    Bokermannohyla juiju is a member of the B. martinsi species group and it was described based on one male specimen. In order to enhance the knowledge about the species, we describe its advertisement call and morphological variation, including for the first time data on females. We also provide additional comments about its natural history, geographic distribution, and conservation. The advertisement call of B. juiju consists of a single note, non-pulsed, harmonic structured call emitted several times in a row. Four out of five males were found calling in bromeliads. The female, as it is common in many Bokermannohyla species, presents some morphological features not shared with the males, like a non-hypertrophied forearm and less developed prepollex. 

  11. Reference-free fatigue crack detection using nonlinear ultrasonic modulation under various temperature and loading conditions

    NASA Astrophysics Data System (ADS)

    Lim, Hyung Jin; Sohn, Hoon; DeSimio, Martin P.; Brown, Kevin

    2014-04-01

    This study presents a reference-free fatigue crack detection technique using nonlinear ultrasonic modulation. When low frequency (LF) and high frequency (HF) inputs generated by two surface-mounted lead zirconate titanate (PZT) transducers are applied to a structure, the presence of a fatigue crack can provide a mechanism for nonlinear ultrasonic modulation and create spectral sidebands around the frequency of the HF signal. The crack-induced spectral sidebands are isolated using a combination of linear response subtraction (LRS), synchronous demodulation (SD) and continuous wavelet transform (CWT) filtering. Then, a sequential outlier analysis is performed on the extracted sidebands to identify the crack presence without referring any baseline data obtained from the intact condition of the structure. Finally, the robustness of the proposed technique is demonstrated using actual test data obtained from simple aluminum plate and complex aircraft fitting-lug specimens under varying temperature and loading variations.

  12. Multi Jet Induced Forces and Moments on VTOL Aircraft Hovering in and Out of Ground Effect

    DTIC Science & Technology

    1977-06-19

    It e01 L. h; Lilt’ IFe 1𔃺t MI 111)4t , tIpo Ia 1p ra’ue o r 11Iii (’t l I I ’ll I lit V 101 Of it I r, frinm. mit’ kd.own Fot) en us oeu t (I frOe-.1...protX 1111;1 L VIN, M( 0.25. Re fvrenru 5 de ITinus the ecl of ITle roa fcI Low rugilon andic tilL bg n 111lug Of t~he lXIsymmetnriC ca rgi a a11 I’oMtC...impIngement polnt. bC des .! gned as () Thtis dens:1ty Is used to determine NSI in Equation (31). lhe tLotti mass F-.ow il the madi a wo3. ~lcjet in an

  13. [The detection and sequence analysis of the simian T-lymphotrophic retrovirus (STLV-1 Papio) by using the polymerase chain reaction].

    PubMed

    D'iachenko, A G; Dzhalagoniia, B E; Kapanadze, B I

    1993-01-01

    The gene amplification technique was used for detection and sequence analysis of STLV-1 Papio proviral DNA. The polymerase chain reaction was performed with a primer pair at tax region of HTLV-1, 7336-7354, sense strand, and 7516-7494, antisense strand. One microgram of DNAs isolated from LUG-4 cells and autopsies was used in a reaction volume of 50 microliters involving 30 cycles of amplifications. The reaction product was blunt-end cloned into pUC19 cut with Smal. The sequence was done with T7-polymerase using 32P-dATR as a label. Our results indicate that STLV-1 Papio provirus is actually present in the cells of a lymphoid cell line and tumor cells of lymphomatous monkeys. There are some differences between STLV-1 Papio and reported sequences of HTLV-1 and STLV-1.

  14. [Evaluation of transperineal sonography for lower urinary tract symptoms after pelvic floor reconstruction].

    PubMed

    Zhong, X L; Song, J; Xu, Y L; Lyu, X L; Zhong, X H; Wang, A P; Song, Y F

    2017-09-25

    Objective: To evaluate transperineal sonography for lower urinary tract symptoms after pelvic floor reconstruction. Methods: Eighty-three patients with severe pelvic organ prolapse received surgeries in Fuzhou General Hospital from September 2014 to September 2015, dividing into two groups: 27 patients were selected to receive transvaginal mesh (TVM) pelvic floor reconstruction surgery with tension-free vaginal tape-Abbrevo (TVT-Abbrevo) incontinence surgery, named TVM+TVT-Abbrevo group; 56 patients were selected to receive TVM pelvic floor reconstruction surgery only, named TVM group. The ultrasonic parameters at rest, on contraction and Valsalva condition respectively were observed and measured, including the bladder neck descent (BND), urethral rotation angle, retrovesical angle, levator urethra gap (LUG), the existence of bladder neck funneling, position of the tape, by using 2D and 3D transperineal ultrasound. Results: The two groups were compared with the ultrasonic parameters before and after operation: two groups of patients with postoperative BND [(2.3±0.5) versus (3.1±0.7) cm, (1.6±0.4) versus (3.6±0.4) cm] were significantly reduced, the difference was statistically significant ( P= 0.02, P< 0.01). The two groups of LUG before and after operation [(3.62±0.45) versus (3.26±0.92) cm, (2.96±0.47) versus (2.72±0.38) cm] both had significant difference by maximum Valsalva ( P< 0.01, P= 0.04). There was statistical significance difference of urethral rotation angle in TVM+TVT-Abbrevo group by maximum Valsalva ( P= 0.01). Observation of morphology: (1) 2 patients with difficulty in urination in TVM+TVT-Abbrevo group, ultrasound showed when the position of the bladder down the urethra discount; 4 patients with stress urinary incontinence (SUI), ultrasound showed slings off or release. (2) One patient with difficulty in urination in TVM group, but ultrasound showed lower urinary tract anatomy were normal; 5 patients with SUI, ultrasound showed the position of the bladder neck were significantly lower in 3 patients, showing high mobility, and the other 2 patients had a larger urethral diameter, showing a tendency of natural deletion. Conclusion: s Anatomy of lower urinary tract could be clearly showed by transperineal sonography. This could provide imaging support for the diagnosis of lower urinary tract symptoms after pelvic floor reconstruction.

  15. Requirements of Inconel 718 alloy for aeronautical applications

    NASA Astrophysics Data System (ADS)

    Ghiban, Brandusa; Elefterie, Cornelia Florina; Guragata, Constantin; Bran, Dragos

    2018-02-01

    The main requirements imposed by aviation components made from super alloys based on Nickel are presented in present paper. A significant portion of fasteners, locking lugs, blade retainers and inserts are manufactured from Inconel 718 alloy. The thesis describes environmental factors (corrosion), conditions of external aggression (salt air, intense heat, heavy industrial pollution, high condensation, high pressure), mechanical characteristics (tensile strength, creep, density, yield strength, fracture toughness, fatigue resistance) and loadings (tensions, compression loads) that must be satisfied simultaneously by Ni-based super alloy, compared to other classes of aviation alloys (as egg. Titanium alloys, Aluminum alloys). For this alloy the requirements are strength, durability, damage tolerance, fail safety and so on. The corrosion can be an issue, but the fatigue under high-magnitude cyclic tensile loading it what limits the lifetime of the airframe. The excellent malleability and weldability characteristics of the 718 system make the material physical properties tolerant of manufacturing processes. These characteristics additionally continue to provide new opportunities for advanced manufacturing methods.

  16. Aeronautical requirements for Inconel 718 alloy

    NASA Astrophysics Data System (ADS)

    Elefterie, C. F.; Guragata, C.; Bran, D.; Ghiban, B.

    2017-06-01

    The project goal is to present the requirements imposed by aviation components made from super alloys based on Nickel. A significant portion of fasteners, locking lugs, blade retainers and inserts are manufactured from Alloy 718. The thesis describes environmental factors (corrosion), conditions of external aggression (salt air, intense heat, heavy industrial pollution, high condensation, high pressure), mechanical characteristics (tensile strength, yield strength and fatigue resistance) and loadings (tensions, compression loads) that must be satisfied simultaneously by Ni-based super alloy, compared to other classes of aviation alloys (as egg. Titanium alloys, Aluminum alloys). For this alloy the requirements are strength durability, damage tolerance, fail safety and so on. The corrosion can be an issue, but the fatigue under high-magnitude cyclic tensile loading it’s what limits the lifetime of the airframe. Also, the excellent malleability and weldability characteristics of the 718 system make the material physical properties tolerant of manufacturing processes. These characteristics additionally continue to provide new opportunities for advanced manufacturing methods.

  17. A Statistical Method for One-to Three-Day Tropical Cyclone Track Prediction.

    DTIC Science & Technology

    1984-01-01

    J WUUlcto j( .) U .3m I Ma5 52 0 .0o3 30005 37 0.064 3010 71. 0.052 3oo005 6 0.073 300 80 0.132 0010 75 0.055 30010 75 0O.0S) O05 37 O.OU 3005 65 0...IM’ weS (k.31 L 8 0M7M9 3 U-0 -2fl79 lug5 n ~q 1-f tr KV ?-i....P z-l t R Prv:, Etaor Fv IPeltr lV 0.167 40.2 L0 0.2% 3205 0.237 30005 65 0.25 JU5,05...0058’ 3O00 61 0.0 30010 61 O.oL6 30005 65 0.02 5 321.05 56 0.3 30007 61 0.054 t 0005 65 0.00. 1005 66 0.0107 10010 0 0.061’, 06 32ro0550 0.028 3O0 6O1

  18. HIGH FREQUENCY POWER TRANSMISSION LINE FOR CYCLOTRONS AND THE LIKE

    DOEpatents

    Armstrong, W.J.

    1954-04-20

    High-frequency power transmission systems, particularly a stacked capacitance alternating power current transmission line wherein maximum utilization of the effective conductios skin of the line conductors is achieved while enabling a low impedance to be obtained are reported. The transmission line consists of a number of flat metal strips with interleaved dielectric strips. The metal dielectric strips are coiled spirally with the axis of the spiral extending along the length of the strips, and the alternating metal strips at the output end have outwardly extending aligned lugs which are directly strapped together and connected to the respective terminals on the load. At the input end of the transmission line, similarly, the alternate metal strips are directly strapped together and connected to an altereating current source. With the arrangement described each metal strip conducts on both sides, so that the metal strips are designed to have a thickness corresponding to twice the depth of the "skin effect" conducting lamina of each conductor at the source frequency.

  19. The p-version of the finite element method in incremental elasto-plastic analysis

    NASA Technical Reports Server (NTRS)

    Holzer, Stefan M.; Yosibash, Zohar

    1993-01-01

    Whereas the higher-order versions of the finite elements method (the p- and hp-version) are fairly well established as highly efficient methods for monitoring and controlling the discretization error in linear problems, little has been done to exploit their benefits in elasto-plastic structural analysis. Aspects of incremental elasto-plastic finite element analysis which are particularly amenable to improvements by the p-version is discussed. These theoretical considerations are supported by several numerical experiments. First, an example for which an analytical solution is available is studied. It is demonstrated that the p-version performs very well even in cycles of elasto-plastic loading and unloading, not only as compared to the traditional h-version but also in respect to the exact solution. Finally, an example of considerable practical importance - the analysis of a cold-worked lug - is presented which demonstrates how the modeling tools offered by higher-order finite element techniques can contribute to an improved approximation of practical problems.

  20. Technology Insertion (TI)/Industrial Process Improvement (IPI). Task Order no. 1 (Misc Manufacturing). Book 2. Database Documentation Book for OO-ALC MANPWW. Analysis of the 80/20 Listing

    DTIC Science & Technology

    1989-12-15

    60000000000C c 0 000 C 0*0,0� 0’ ’Ci0 0 00 cacao 0 0 &MUM~i .44OO N NOiO N "- aN"n~n~VW4 N Me cV-.4mo "MOONOMMV-M40N0 i) 0-Ŕ VOONMm00o ftV- N t- a*WV-i 444...105 ROLL BURNISH MOUNTING FLANGE BOLT 001 MNF RAHOLI.ES ( AFI END) 0󈧆 04 *::C/P MOVE 003 DE 𔃻 4 56’ 110 AFT DOOR LEVER LUG HOLE (RIGF SITE 001 MiNR...TO DE ACCOMPLISHED MECHANIC p.... 󈧞 -275 PRIOR TO CAD PI..ATE, GRIT I’I. A"sT "I .L 001 MN IR C ’ A S REAS TO BE CAD PLA’T’ED *CIP MOVE 002 01 6

  1. State Tracking and Fault Diagnosis for Dynamic Systems Using Labeled Uncertainty Graph.

    PubMed

    Zhou, Gan; Feng, Wenquan; Zhao, Qi; Zhao, Hongbo

    2015-11-05

    Cyber-physical systems such as autonomous spacecraft, power plants and automotive systems become more vulnerable to unanticipated failures as their complexity increases. Accurate tracking of system dynamics and fault diagnosis are essential. This paper presents an efficient state estimation method for dynamic systems modeled as concurrent probabilistic automata. First, the Labeled Uncertainty Graph (LUG) method in the planning domain is introduced to describe the state tracking and fault diagnosis processes. Because the system model is probabilistic, the Monte Carlo technique is employed to sample the probability distribution of belief states. In addition, to address the sample impoverishment problem, an innovative look-ahead technique is proposed to recursively generate most likely belief states without exhaustively checking all possible successor modes. The overall algorithms incorporate two major steps: a roll-forward process that estimates system state and identifies faults, and a roll-backward process that analyzes possible system trajectories once the faults have been detected. We demonstrate the effectiveness of this approach by applying it to a real world domain: the power supply control unit of a spacecraft.

  2. Nonlinear ultrasonic wave modulation for online fatigue crack detection

    NASA Astrophysics Data System (ADS)

    Sohn, Hoon; Lim, Hyung Jin; DeSimio, Martin P.; Brown, Kevin; Derriso, Mark

    2014-02-01

    This study presents a fatigue crack detection technique using nonlinear ultrasonic wave modulation. Ultrasonic waves at two distinctive driving frequencies are generated and corresponding ultrasonic responses are measured using permanently installed lead zirconate titanate (PZT) transducers with a potential for continuous monitoring. Here, the input signal at the lower driving frequency is often referred to as a 'pumping' signal, and the higher frequency input is referred to as a 'probing' signal. The presence of a system nonlinearity, such as a crack formation, can provide a mechanism for nonlinear wave modulation, and create spectral sidebands around the frequency of the probing signal. A signal processing technique combining linear response subtraction (LRS) and synchronous demodulation (SD) is developed specifically to extract the crack-induced spectral sidebands. The proposed crack detection method is successfully applied to identify actual fatigue cracks grown in metallic plate and complex fitting-lug specimens. Finally, the effect of pumping and probing frequencies on the amplitude of the first spectral sideband is investigated using the first sideband spectrogram (FSS) obtained by sweeping both pumping and probing signals over specified frequency ranges.

  3. Fine gravel controls hydrologic and erodibility responses to trampling disturbance for coarse-textured soils with weak cyanobacterial crusts

    USGS Publications Warehouse

    Herrick, J.E.; Van Zee, J. W.; Belnap, J.; Johansen, J.R.; Remmenga, M.

    2010-01-01

    We compared short-term effects of lug-soled boot trampling disturbance on water infiltration and soil erodibility on coarse-textured soils covered by a mixture of fine gravel and coarse sand over weak cyanobacterially-dominated biological soil crusts. Trampling significantly reduced final infiltration rate and total infiltration and increased sediment generation from small (0.5m2) rainfall simulation plots (p<0.01). Trampling had no effect on time to runoff or time to peak runoff. Trampling had similar effects at sites with both low and very low levels of cyanobacterial biomass, as indicated by chlorophyll a concentrations. We concluded that trampling effects are relatively independent of differences in the relatively low levels of cyanobacterial biomass in this environment. Instead, trampling appears to reduce infiltration by significantly reducing the cover of gravel and coarse sand on the soil surface, facilitating the development of a physical crust during rainfall events. The results of this study underscore the importance of carefully characterizing both soil physical and biological properties to understand how disturbance affects ecosystem processes. ?? 2010.

  4. Calcareous nannofossil events in the pre-evaporitic Messinian

    NASA Astrophysics Data System (ADS)

    Negri, Alessandra; Lozar, Francesca

    2017-04-01

    During the Messinian (7.2 to 5.3 Ma) the Mediterranean area experienced fast and deep climatic and eustatic structural changes. The stratigraphic framework for this interval is relatively well constrained and the beginning of the Messinian salinity crisis dated at 5.97 Ma determine a duration of at least 1.2 Ma for the pre-evaporitic Messinian that is object of this study. Several sites (Faneromeni, Pissouri, Polemi Fanantello borehole, Lemme, Pollenzo, Govone, Moncalvo; Wade and Bown, 2006; Kouwenhoven et al 2006, Morigi et al 2007, Lozar et al 2010, Dela Pierre et al 2011) show similar calcareous nannofossil record behavior, with several Sphenolithus spp. peaks recognised at different quotes in each of the sections. Aim of the present work is to compare the calcareous nannofossil data achieved in the above mentioned sections: interestingly, the occurrence of strongly oligotypic assemblages related to high salinity and unstable environments, appear to correlate precisely among the investigated sites and occur immediately before the onset of the Messinian salinity crisis, then offering the possibility to use them as bioevents for regional correlation. References Dela Pierre, F., Bernardi, E., Cavagna, S., Clari, P., Gennari, R., Irace, A., Lozar, F., Lugli, S., Manzi, V., Natalicchio, M., Roveri, M., Violanti, D., 2011. The record of the Messinian salinity crisis in the Tertiary Piedmont Basin (NW Italy): The Alba section revisited. Palaeogeography, Palaeoclimatology, Palaeoecology 310, 238-255. Kouwenhoven, T.J., Morigi, C., Negri, A., Giunta, S., Krijgsman, W., Rouchy, J.M., 2006 Paleoenvironmental evolution of the eastern Mediterranean during the Messinian: Constraints from integrated microfossil data of the Pissouri Basin (Cyprus). Marine Micropaleontology 60, 17-44. Lozar, F., Violanti, D., Dela Pierre, F., Bernardi, E., Cavagna, S., Clari, P., Irace, A., Martinetto, E., Trenkwalder, S., 2010. Calcareous nannofossils and foraminifers herald the Messinian salinity crisis: the Pollenzo section (Alba, Cuneo; NW Italy). Geobios 43, 21-32. Manzi, V., Roveri, M., Gennari, R., Bertini, A., Biffi, U., Giunta, S., Iaccarino, S., Lanci, L., Lugli, S., Negri, A., Riva, A., Rossi, M.E., Taviani, M., 2007. The deep-water counterpart of the Messinian Lower Evaporites in the Apennine foredeep: The Fanantello section (Northern Apennines, Italy). Palaeogeography, Palaeoclimatology, Palaeoecology 251, 470-499. Morigi C., Negri A., Giunta S. , Kouwenhoven T., Krijgsman W., Blanc-Valleron M., Orszag-Sperber F., Rouchy J.M.. 2007. Integrated quantitative biostratigraphy of the latest Tortonian-early Messinian Pissouri section (Cyprus): An evaluation of calcareous plankton bioevents. Biostratigraphie intégrée du passage Tortonien-Messinien dans le bassin de Pissouri (Chypre) : une evaluation des bio-evenements dans le plancton calcaire. Geobios 40 : 267-279. Wade B.S. and Bown P.2006, Calcareous nannofossils in extreme environments: The Messinian Salinity Crisis, Polemi Basin, Cyprus. Palaeogeography, Palaeoclimatology, Palaeoecology 233 (2006) 271- 286

  5. Optimal sensor placement for active guided wave interrogation of complex metallic components

    NASA Astrophysics Data System (ADS)

    Coelho, Clyde K.; Kim, Seung Bum; Chattopadhyay, Aditi

    2011-04-01

    With research in structural health monitoring (SHM) moving towards increasingly complex structures for damage interrogation, the placement of sensors is becoming a key issue in the performance of the damage detection methodologies. For ultrasonic wave based approaches, this is especially important because of the sensitivity of the travelling Lamb waves to material properties, geometry and boundary conditions that may obscure the presence of damage if they are not taken into account during sensor placement. The framework proposed in this paper defines a sensing region for a pair of piezoelectric transducers in a pitch-catch damage detection approach by taking into account the material attenuation and probability of false alarm. Using information about the region interrogated by a sensoractuator pair, a simulated annealing optimization framework was implemented in order to place sensors on complex metallic geometries such that a selected minimum damage type and size could be detected with an acceptable probability of false alarm anywhere on the structure. This approach was demonstrated on a lug joint to detect a crack and on a large Naval SHM test bed and resulted in a placement of sensors that was able to interrogate all parts of the structure using the minimum number of transducers.

  6. The Messinian Salinity Crisis: what can we expect from drilling the perched basins from the Balearic Promontory?

    NASA Astrophysics Data System (ADS)

    Johanna, Lofi; Angelo, Camerlenghi; Agnès, Maillard; Diana, Ochoa

    2015-04-01

    In spite of 40 years of multi-disciplinary research conducted on the Messinian Salinity Crisis (MSC) event, modalities, timing, causes, chronology and consequence at local and planetary scale of this event are still not yet fully understood, and the MSC event remains one of the longest-living controversies in Earth Science. A key factor for the controversy is certainly the lack of a complete record of the MSC deposits preserved in the deepest Mediterranean basins. Anywhere else, on the continental shelves and slopes, the MSC mostly generated a sedimentary/time lag corresponding to a widespread erosional surface. Correlations with the depositional units locally preserved onshore are thus complex, preventing the construction of a coherent scenario linking the outcropping MSC evaporites, the erosion on the margins, and the deposition of clastics and evaporites in the abyssal plains. Recent works based on seismic profile interpretations and conducted on the Balearic promontory allowed to evidence a series of small perched basins presently lying in different water depths stepped from the coast line down to the deep basin. These topographic lows trapped sedimentary series up to 500m thick, interpreted as MSC in age (Maillard et al., 2014; Mocnik et al., 2014; Driussi et al., in press). In the most proximal basins, these deposits have been drilled and logged for industriel purposes and consist of gypsum beds interbedded with marls. Ochoa et al. (submitted) demonstrated that these MSC deposits correlate with the Primary Lower Gypsum sequence deposited in marginal settings before the drawdown phase (Lugli et al., 2010) and that are now observed onshore in tectonically active areas. The basins located in more distal locations also contain MSC deposits (including <200m thick salt layers) but these have not been drilled. The relative age and chronology of the MSC deposits from one basin to another thus still need to be defined. The Balearic Promontory is probably the only place in the Mediterranean area potentially bearing some records of the MSC event that have been accumulated and preserved at various water depths in which post/Messinian tectonic deformation is low. A complete shallow-to-deep transect of sites across these stepped basins, provides a unique opportunity to quantify the amplitude of the Messinian draw-down and to test the hypotheses of a stratified water column and of a diachronous/synchronous onset and end of the salinity crisis. In order to address these persistent open questions, we propose to drill, core and log a shallow-to-deep transect on the Balearic Promontory as part of a daughter proposal (DREAM proposal) of a Multi-phase IODP Drilling Project entitled "Uncovering A Salt Giant" (857-MDP, coord. A. Camerlenghi). The DREAM Team: A. Giovanni, H. Christian, G. deLangeGert, R. Flecker, D. Garcia-Castellanos, Z. Gvirtzman, W. Krijgsman, S. Lugli, MakowskyItzik, M. Vinicio, T. McGenity, G. Panieri, M. Rabineau, M. Roveri, F.J. Sierro, N. Waldman.

  7. Mission safety evaluation report for STS-39, postflight edition

    NASA Technical Reports Server (NTRS)

    Hardie, Kenneth O.; Hill, William C.; Finkel, Seymour I.

    1991-01-01

    After a delay of approximately 2 months due to a rollback from the pad to replace the External Tank door lug housing, Space Shuttle Discovery was launched from NASA-Kennedy at 7:33 a.m. Eastern Daylight Time on 28 April 1991. STS-39 was the first unclassified DoD Shuttle mission. On 28 April, countdown proceeded normally through the T-20 minute hold. No significant problems were encountered except for the Operations Sequence-2 recorder starting unexpectedly; it was stopped by an uplink command. Discovery landed on KSC runway 15 at 2:55 p.m. EDT on 6 May 1991. This was the second time in 6 months that the Space Shuttle was diverted to KSC for landing because of high winds at Edwards AFB, Calif. This was also the 7th of 40 Shuttle missions to land at KSC in the history of the Space Shuttle Program. The Main Landing Gear outer right tire shredded 3 of the 16 cords due to either an uneven landing or a maximum force breaking test during rollout. Contributing factors to the tire cord shredding were the development of last minute crosswinds and reluctance of the ground controllers to distract the Shuttle pilots with warnings of the low flight path. As a corrective action, communication procedures will be modified for future flights.

  8. Neurodegenerative disease and magnetic field exposure in UK electricity supply workers.

    PubMed

    Sorahan, T; Mohammed, N

    2014-09-01

    Previous research has suggested a possible link between neurodegenerative disease and exposure to extremely low-frequency electric and magnetic fields. To investigate whether risks of Alzheimer's, motor neurone or Parkinson's disease are related to occupational exposure to magnetic fields. The mortality experienced by a cohort of 73051 employees of the former Central Electricity Generating Board of England and Wales was investigated for the period 1973-2010. All employees were hired in the period 1952-82, were employed for at least 6 months and had some employment after 1 January 1973. Detailed calculations had been performed by others to enable an assessment to be made of exposures to magnetic fields. Poisson regression was used to calculate relative risks (rate ratios) of developing any of the three diseases under investigation for categories of lifetime, distant (lagged) and recent (lugged) exposure. No statistically significant trends were shown for risks of any of these diseases to increase with estimates of lifetime, recent or distant exposure to magnetic fields. There is no convincing evidence that UK electricity generation and transmission workers have suffered elevated risks from neurodegenerative diseases as a consequence of exposure to magnetic fields. © The Author 2014. Published by Oxford University Press on behalf of the Society of Occupational Medicine. All rights reserved. For Permissions, please email: journals.permissions@oup.com.

  9. On-line prognosis of fatigue crack propagation based on Gaussian weight-mixture proposal particle filter.

    PubMed

    Chen, Jian; Yuan, Shenfang; Qiu, Lei; Wang, Hui; Yang, Weibo

    2018-01-01

    Accurate on-line prognosis of fatigue crack propagation is of great meaning for prognostics and health management (PHM) technologies to ensure structural integrity, which is a challenging task because of uncertainties which arise from sources such as intrinsic material properties, loading, and environmental factors. The particle filter algorithm has been proved to be a powerful tool to deal with prognostic problems those are affected by uncertainties. However, most studies adopted the basic particle filter algorithm, which uses the transition probability density function as the importance density and may suffer from serious particle degeneracy problem. This paper proposes an on-line fatigue crack propagation prognosis method based on a novel Gaussian weight-mixture proposal particle filter and the active guided wave based on-line crack monitoring. Based on the on-line crack measurement, the mixture of the measurement probability density function and the transition probability density function is proposed to be the importance density. In addition, an on-line dynamic update procedure is proposed to adjust the parameter of the state equation. The proposed method is verified on the fatigue test of attachment lugs which are a kind of important joint components in aircraft structures. Copyright © 2017 Elsevier B.V. All rights reserved.

  10. BASIC PENTACYSTEINE Proteins Mediate MADS Domain Complex Binding to the DNA for Tissue-Specific Expression of Target Genes in Arabidopsis[W

    PubMed Central

    Simonini, Sara; Roig-Villanova, Irma; Gregis, Veronica; Colombo, Bilitis; Colombo, Lucia; Kater, Martin M.

    2012-01-01

    BASIC PENTACYSTEINE (BPC) transcription factors have been identified in a large variety of plant species. In Arabidopsis thaliana there are seven BPC genes, which, except for BPC5, are expressed ubiquitously. BPC genes are functionally redundant in a wide range of developmental processes. Recently, we reported that BPC1 binds to guanine and adenine (GA)–rich consensus sequences in the SEEDSTICK (STK) promoter in vitro and induces conformational changes. Here we show by chromatin immunoprecipitation experiments that in vivo BPCs also bind to the consensus boxes, and when these were mutated, expression from the STK promoter was derepressed, resulting in ectopic expression in the inflorescence. We also reveal that SHORT VEGETATIVE PHASE (SVP) is a direct regulator of STK. SVP is a floral meristem identity gene belonging to the MADS box gene family. The SVP-APETALA1 (AP1) dimer recruits the SEUSS (SEU)-LEUNIG (LUG) transcriptional cosuppressor to repress floral homeotic gene expression in the floral meristem. Interestingly, we found that GA consensus sequences in the STK promoter to which BPCs bind are essential for recruitment of the corepressor complex to this promoter. Our data suggest that we have identified a new regulatory mechanism controlling plant gene expression that is probably generally used, when considering BPCs’ wide expression profile and the frequent presence of consensus binding sites in plant promoters. PMID:23054472

  11. Photovoltaic stand-alone modular systems, phase 2

    NASA Technical Reports Server (NTRS)

    Naff, G. J.; Marshall, N. A.

    1983-01-01

    The final hardware and system qualification phase of a two part stand-alone photovoltaic (PV) system development is covered. The final design incorporated modular, power blocks capable of expanding incrementally from 320 watts to twenty kilowatts (PK). The basic power unit (PU) was nominally rated 1.28 kWp. The controls units, power collection buses and main lugs, electrical protection subsystems, power switching, and load management circuits are housed in a common control enclosure. Photo-voltaic modules are electrically connected in a horizontal daisy-chain method via Amp Solarlok plugs mating with compatible connectors installed on the back side of each photovoltaic module. A pair of channel rails accommodate the mounting of the modules into a frameless panel support structure. Foundations are of a unique planter (tub-like) configuration to allow for world-wide deployment without restriction as to types of soil. One battery string capable of supplying approximately 240 ampere hours nominal of carryover power is specified for each basic power unit. Load prioritization and shedding circuits are included to protect critical loads and selectively shed and defer lower priority or noncritical power demands. The baseline system, operating at approximately 2 1/2 PUs (3.2 kW pk.) was installed and deployed. Qualification was successfully complete in March 1983; since that time, the demonstration system has logged approximately 3000 hours of continuous operation under load without major incident.

  12. Photovoltaic stand-alone modular systems, phase 2

    NASA Astrophysics Data System (ADS)

    Naff, G. J.; Marshall, N. A.

    1983-07-01

    The final hardware and system qualification phase of a two part stand-alone photovoltaic (PV) system development is covered. The final design incorporated modular, power blocks capable of expanding incrementally from 320 watts to twenty kilowatts (PK). The basic power unit (PU) was nominally rated 1.28 kWp. The controls units, power collection buses and main lugs, electrical protection subsystems, power switching, and load management circuits are housed in a common control enclosure. Photo-voltaic modules are electrically connected in a horizontal daisy-chain method via Amp Solarlok plugs mating with compatible connectors installed on the back side of each photovoltaic module. A pair of channel rails accommodate the mounting of the modules into a frameless panel support structure. Foundations are of a unique planter (tub-like) configuration to allow for world-wide deployment without restriction as to types of soil. One battery string capable of supplying approximately 240 ampere hours nominal of carryover power is specified for each basic power unit. Load prioritization and shedding circuits are included to protect critical loads and selectively shed and defer lower priority or noncritical power demands. The baseline system, operating at approximately 2 1/2 PUs (3.2 kW pk.) was installed and deployed. Qualification was successfully complete in March 1983; since that time, the demonstration system has logged approximately 3000 hours of continuous operation under load without major incident.

  13. Development and hydrology of biological soil crusts -- first results from a surface inoculation experiment

    NASA Astrophysics Data System (ADS)

    Mykhailova, Larysa; Raab, Thomas; Gypser, Stella; Fischer, Thomas

    2016-04-01

    Representing a set of various micro-biocoenoses, biocrusts often reside in adjacent patches, which not necessarily relate to structural elements of the habitat, like (micro-) topography or vegetational patterns. Such biocrust patches may become more stable through the formation of mutually dependent ecohydrological regimes. For example, algal patches inhibiting infiltration and generating runoff alternate with runoff-receiving moss patches possessing high water holding capacities. Here, we preliminarily report on a lysimeter field experiment where natural biocrust isolates were used for surface inoculation to (I) prove stochastic vs. deterministic biocrust development and (II) to quantitatively relate biocrust development to soil hydrology. Lysimeter sand was collected from 3-4 m below surface at natural dune outcrops in south-eastern Brandenburg, Germany (Glashütte (GLA) and Neuer Lugteich (LUG)), where biocrust samples were collected at the respective dune bases. The lysimeters were designed to prevent runoff. In a completely randomized full-factorial design, three factors were considered. (A) Inocolum in three treatments (bare control, mosses, algae), (B) mineral substrate texture in two treatments (GLA: 55% and LUG: 79% particles >630 μm), and (C) surface compaction in two treatments (control, 41.5 kN m-2 for 30 seconds). The samples were kept dry and re-moistened to -60 hPa two days before inoculation. After a species inventory, the inoculate was isolated by gently washing off sand particles from the biocrust samples. Algal/lichen crusts were dominated by Zygogonium ericetorum and Cladonia sp. at both sites. All moss crusts were dominated by Polytrichum piliferum and Ceratodon purpureus, whereas Brachythecium albicans was present at GLA only. 20 g of homogenized moist inoculate were spread over the surface of each lysimeter (Ø 19 cm, 22 cm depth). We performed autochthonous inoculation, i.e. biocrust isolates collected from GLA were used for inoculation of GLA substrate etc. The experiment started at 12.02.2015 and was located at an open area in the vicinity of a meteorological station, where all relevant for HYDRUS modeling data, as well as global radiation have been recorded every 10 min. Crust development was monitored by non-destructive NDVI imaging and a per lysimeter determination of the areal share of biocrust developmental stages: mineral surface (NDVI ≤ 0), BSC1 (0 < NDVI ≤ 0.15), BSC2 (0.15 < NDVI ≤ 0.40) and BSC3 (NDVI > 0.40). The general water balance equation and the amount of lysimeter leachate were used to determine evaporation and changes in water stocks by regular weighing. Biomass growth was inhibited in summer compared to autumn, where mosses developed faster than algae. Finer grained substrate promoted biocrust growth. Evapotranspiration increased with biomass development, presumably because the amount of water held close to the surface increased with biomass. It can be expected that this effect strengthens with increasing amounts of silt and clay. Biodiversity studies are pending, but incipient biocrust growth in the controls points to atmogenic superinfection. So far, it can be concluded that availability of water, depending on both precipitation and substrate texture, were the driving factors of biocrust development. Apart from runoff losses in hillslope conditions, biocrusts are hypothesized to take advantage over their vascular competitors by preventing water infiltration into deeper soil through increased evapotranspiration.

  14. Innovative Ballasted Flat Roof Solar PV Racking System

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Peek, Richard T.

    2014-12-15

    The objective of this project was to reduce the cost of racking for PV solar on flat commercial rooftops. Cost reductions would come from both labor savings and material savings related to the installation process. The rack would need to accommodate the majority of modules available on the market. Cascade Engineering has a long history of converting traditional metal type applications over to plastic. Injection molding of plastics have numerous advantages including selection of resin for the application, placing the material exactly where it is needed, designing in features that will speed up the installation process, and weight reduction ofmore » the array. A plastic rack would need to meet the requirements of UL2703, Mounting systems, mounting devices, clamping/retention devices, and ground lugs for use with flat-plate photovoltaic modules and panels. Comparing original data to the end of project racking design, racking material costs were reduced 50% and labor costs reduced 64%. The racking product accommodates all 60 and 72 cell panels on the market, meets UL2703 requirements, contributes only 1.3 pounds per square foot of weight to the array, requires little ballast to secure the array, automatically grounds the module when the module is secured, stacks/nests well for shipping/fewer lifts to the roof, provides integrated wire routing, allows water to drain on the roof, and accommodates various seismic roof connections. Project goals were achieved as noted in the original funding application.« less

  15. Magnetic fields and leukaemia risks in UK electricity supply workers.

    PubMed

    Sorahan, T

    2014-04-01

    To investigate whether leukaemia risks are related to occupational exposure to low-frequency magnetic fields. Leukaemia risks experienced by 73 051 employees of the former Central Electricity Generating Board of England and Wales were investigated for the period 1973-2010. All employees were hired in the period 1952-82 and were employed for at least 6 months with some employment in the period 1973-82. Detailed calculations had been performed by others to enable an assessment to be made of exposures to magnetic fields. Poisson regression was used to calculate relative risks (rate ratios) of developing leukaemia or leukaemia subtypes for categories of lifetime, distant (lagged) and recent (lugged) exposure. Findings for all leukaemias combined were unexceptional; risks were close to unity for all exposure categories and there was no suggestion of risks increasing with cumulative (or recent or distant) magnetic field exposures. There were no statistically significant dose-response effects shown for acute myeloid leukaemia, chronic myeloid leukaemia or chronic lymphocytic leukaemia. There was a significant positive trend for acute lymphocytic leukaemia (ALL), but this was based, in the main, on unusually low risks in the lowest exposure category. This study found no convincing evidence to support the hypothesis that exposure to magnetic fields is a risk factor for leukaemia, and the findings are consistent with the hypotheses that both distant and recent magnetic field exposures are not causally related to the generality of leukaemia. The limited positive findings for ALL may well be chance findings.

  16. Structural Analysis for the American Airlines Flight 587 Accident Investigation: Global Analysis

    NASA Technical Reports Server (NTRS)

    Young, Richard D.; Lovejoy, Andrew E.; Hilburger, Mark W.; Moore, David F.

    2005-01-01

    NASA Langley Research Center (LaRC) supported the National Transportation Safety Board (NTSB) in the American Airlines Flight 587 accident investigation due to LaRC's expertise in high-fidelity structural analysis and testing of composite structures and materials. A Global Analysis Team from LaRC reviewed the manufacturer s design and certification procedures, developed finite element models and conducted structural analyses, and participated jointly with the NTSB and Airbus in subcomponent tests conducted at Airbus in Hamburg, Germany. The Global Analysis Team identified no significant or obvious deficiencies in the Airbus certification and design methods. Analysis results from the LaRC team indicated that the most-likely failure scenario was failure initiation at the right rear main attachment fitting (lug), followed by an unstable progression of failure of all fin-to-fuselage attachments and separation of the VTP from the aircraft. Additionally, analysis results indicated that failure initiates at the final observed maximum fin loading condition in the accident, when the VTP was subjected to loads that were at minimum 1.92 times the design limit load condition for certification. For certification, the VTP is only required to support loads of 1.5 times design limit load without catastrophic failure. The maximum loading during the accident was shown to significantly exceed the certification requirement. Thus, the structure appeared to perform in a manner consistent with its design and certification, and failure is attributed to VTP loads greater than expected.

  17. Development and field application of a nonlinear ultrasonic modulation technique for fatigue crack detection without reference data from an intact condition

    NASA Astrophysics Data System (ADS)

    Lim, Hyung Jin; Kim, Yongtak; Koo, Gunhee; Yang, Suyoung; Sohn, Hoon; Bae, In-hwan; Jang, Jeong-Hwan

    2016-09-01

    In this study, a fatigue crack detection technique, which detects a fatigue crack without relying on any reference data obtained from the intact condition of a target structure, is developed using nonlinear ultrasonic modulation and applied to a real bridge structure. Using two wafer-type lead zirconate titanate (PZT) transducers, ultrasonic excitations at two distinctive frequencies are applied to a target inspection spot and the corresponding ultrasonic response is measured by another PZT transducer. Then, the nonlinear modulation components produced by a breathing-crack are extracted from the measured ultrasonic response, and a statistical classifier, which can determine if the nonlinear modulation components are statistically significant in comparison with the background noise level, is proposed. The effectiveness of the proposed fatigue crack detection technique is experimentally validated using the data obtained from aluminum plates and aircraft fitting-lug specimens under varying temperature and loading conditions, and through a field testing of Yeongjong Grand Bridge in South Korea. The uniqueness of this study lies in that (1) detection of a micro fatigue crack with less than 1 μm width and fatigue cracks in the range of 10-20 μm in width using nonlinear ultrasonic modulation, (2) automated detection of fatigue crack formation without using reference data obtained from an intact condition, (3) reliable and robust diagnosis under varying temperature and loading conditions, (4) application of a local fatigue crack detection technique to online monitoring of a real bridge.

  18. Messinian Salinity Crisis - DREAM (Deep-sea Record of Mediterranean Messinian events) drilling projects

    NASA Astrophysics Data System (ADS)

    Lofi, Johanna; Camerlenghi, Angelo

    2014-05-01

    About 6 My ago the Mediterranean Sea was transformed into a giant saline basin. This event, commonly referred to as the Messinian salinity crisis (MSC), changed the chemistry of the global ocean and had a permanent impact on both the terrestrial and marine ecosystems of a huge area surrounding the Mediterranean area. The first fascinating MSC scenario was proposed following DSDP Leg XIII in 1970 and envisaged an almost desiccated deep Mediterranean basin with a dramatic ~1,500 m drop of sea level, the incision of deep canyons by rivers on the continental margins, and a final catastrophic flooding event when the connections between the Mediterranean Sea and the Atlantic were re-established ~5.33 My ago. In spite of 40 years of multi-disciplinary research conducted on the MSC, modalities, timing, causes, chronology and consequence at local and planetary scale are still not yet fully understood, and the MSC event remains one of the longest-living controversies in Earth Science. Key factor for the controversy is the lack of a complete record of the MSC preserved in the deepest Mediterranean basins. Anywhere else, the MSC mostly generated a sedimentary/time lag corresponding to a widespread erosion surface. Correlations with the offshore depositional units are thus complex, preventing the construction of a coherent scenario linking the outcropping MSC evaporites, the erosion on the margins, and the deposition of clastics and evaporites in the abyssal plains. Recent activity by various research groups in order to identify locations for multiple-site drilling (including riser-drilling) in the Mediterranean Sea that would contribute to solve the open questions still existing about the MSC has culminated in two DREAM Magellan+ Workshops held in 2013 and 2014. A strategy and work plan have been established in order to submit an IODP Multi-phase Drilling Project("Uncovering A Salt Giant")including several site-specific drilling proposals addressing different scientific objectives related to the MSC. Among these proposals, one will be fully dedicated to the MSC event. Improved quality of seismic data has allowed important advances in the recognition and understanding of MSC seismic markers (surfaces and depositional units) and lithological and stratigraphical calibrations are now critical. Therefore, the drilling strategy must include multiple sites covering representative locations of both Western and Eastern Mediterranean basins. A series of critical drilling targets were thus identified as follows: - A first set of drilling targets, dedicated to shallow water (< 2500 m water depth) MSC markers, includes the Messinian clastic wedges, the erosion surfaces and the MSC deposits (including thin salt bodies) trapped in small topographic lows observed at various water depths between the shoreline and the abyssal plain. Up to 10 sites, presented in this work, could be drilled with the riserless R/V Joides Resolution, provided the safety conditions are met; - Another critical drilling target is the full recovering of undeformed MSC sequence (including the Tortonian-Messinian and the Messinian-Zanclean boundaries) in the deep water (>2500m) of both the eastern and western Mediterranean basins. This will be possible thanks to R/V Chikyu riser drilling vessel and will be the scope of a second MSC IODP proposal. DREAM Team: A. Giovanni galod@locean-ipsl.upmc.fr, H. Christian huebscher@zmaw.de, G. deLangeGert gdelange@geo.uu.nl, R. Flecker r.flecker@bristol.ac.uk, D. Garcia-Castellanos danielgc@ictja.csic.es, C. Gorini gorini@upmc.fr, Z. Gvirtzman zohar@gsi.gov.il, W. Krijgsman krijgsma@geo.uu.nl, S. Lugli lugli@unimore.it, I. Makowsky yizhaq@univ.haifa.ac.il, M. Vinicio vinicio.manzi@unipr.it, T. McGenity tjmcgen@essex.ac.uk, G. Panieri giuliana.panieri@uit.no, M. Rabineau rabineau@univ-brest.fr, M. Roveri marco.roveri@unipr.it, F.J. Sierro sierro@usal.es, N. Waldman nwaldmann@univ.haifa.ac.il

  19. Identifying mechanical property parameters of planetary soil using in-situ data obtained from exploration rovers

    NASA Astrophysics Data System (ADS)

    Ding, Liang; Gao, Haibo; Liu, Zhen; Deng, Zongquan; Liu, Guangjun

    2015-12-01

    Identifying the mechanical property parameters of planetary soil based on terramechanics models using in-situ data obtained from autonomous planetary exploration rovers is both an important scientific goal and essential for control strategy optimization and high-fidelity simulations of rovers. However, identifying all the terrain parameters is a challenging task because of the nonlinear and coupling nature of the involved functions. Three parameter identification methods are presented in this paper to serve different purposes based on an improved terramechanics model that takes into account the effects of slip, wheel lugs, etc. Parameter sensitivity and coupling of the equations are analyzed, and the parameters are grouped according to their sensitivity to the normal force, resistance moment and drawbar pull. An iterative identification method using the original integral model is developed first. In order to realize real-time identification, the model is then simplified by linearizing the normal and shearing stresses to derive decoupled closed-form analytical equations. Each equation contains one or two groups of soil parameters, making step-by-step identification of all the unknowns feasible. Experiments were performed using six different types of single-wheels as well as a four-wheeled rover moving on planetary soil simulant. All the unknown model parameters were identified using the measured data and compared with the values obtained by conventional experiments. It is verified that the proposed iterative identification method provides improved accuracy, making it suitable for scientific studies of soil properties, whereas the step-by-step identification methods based on simplified models require less calculation time, making them more suitable for real-time applications. The models have less than 10% margin of error comparing with the measured results when predicting the interaction forces and moments using the corresponding identified parameters.

  20. Simulations and Experiments of Hot Forging Design and Evaluation of the Aircraft Landing Gear Barrel Al Alloy Structure

    NASA Astrophysics Data System (ADS)

    Ram Prabhu, T.

    2016-04-01

    In the present study, the hot forging design of a typical landing gear barrel was evolved using finite element simulations and validated with experiments. A DEFORM3D software was used to evolve the forging steps to obtain the sound quality part free of defects with minimum press force requirements. The hot forging trial of a barrel structure was carried out in a 30 MN hydraulic press based on the simulation outputs. The tensile properties of the part were evaluated by taking samples from all three orientations (longitudinal, long transverse, short transverse). The hardness and microstructure of the part were also investigated. To study the soundness of the product, fluorescent penetrant inspection and ultrasonic testing were performed in order to identify any potential surface or internal defects in the part. From experiments, it was found that the part was formed successfully without any forging defects such as under filling, laps, or folds that validated the effectiveness of the process simulation. The tensile properties of the part were well above the specification limit (>10%) and the properties variation with respect to the orientation was less than 2.5%. The part has qualified the surface defects level of Mil Std 1907 Grade C and the internal defects level of AMS 2630 Class A (2 mm FBh). The microstructure shows mean grain length and width of 167 and 66 µm in the longitudinal direction. However, microstructure results revealed that the coarse grain structure was observed on the flat surface near the lug region due to the dead zone formation. An innovative and simple method of milling the surface layer after each pressing operation was applied to solve the problem of the surface coarse grain structure.

  1. Prosthetic elbow joint

    NASA Technical Reports Server (NTRS)

    Weddendorf, Bruce C. (Inventor)

    1994-01-01

    An artificial, manually positionable elbow joint for use in an upper extremity, above-elbow, prosthetic is described. The prosthesis provides a locking feature that is easily controlled by the wearer. The instant elbow joint is very strong and durable enough to withstand the repeated heavy loadings encountered by a wearer who works in an industrial, construction, farming, or similar environment. The elbow joint of the present invention comprises a turntable, a frame, a forearm, and a locking assembly. The frame generally includes a housing for the locking assembly and two protruding ears. The forearm includes an elongated beam having a cup-shaped cylindrical member at one end and a locking wheel having a plurality of holes along a circular arc on its other end with a central bore for pivotal attachment to the protruding ears of the frame. The locking assembly includes a collar having a central opening with a plurality of internal grooves, a plurality of internal cam members each having a chamfered surface at one end and a V-shaped slot at its other end; an elongated locking pin having a crown wheel with cam surfaces and locking lugs secured thereto; two coiled compression springs; and a flexible filament attached to one end of the elongated locking pin and extending from the locking assembly for extending and retracting the locking pin into the holes in the locking wheel to permit selective adjustment of the forearm relative to the frame. In use, the turntable is affixed to the upper arm part of the prosthetic in the conventional manner, and the cup-shaped cylindrical member on one end of the forearm is affixed to the forearm piece of the prosthetic in the conventional manner. The elbow joint is easily adjusted and locked between maximum flex and extended positions.

  2. Parallels Between Antarctic Travel in 1950 and Planetary Travel in 2050 (to Accompany Notes on "The Norwegian British-Swedish Antarctic Expedition 1949-52")

    NASA Technical Reports Server (NTRS)

    Swithinbank, Charles

    2012-01-01

    Objectives (Slides 2, 12, 21-22) To explore as much as possible of 1 million km2 of unexplored territory. We were the first expedition to winter in Antarctica between 95 E and 57 W - nearly half the coastline of Antarctica. It was understood that we must be self-sufficient in every respect for 2 years. There could be no firm or detailed plans for inland exploration until we found where it was possible to make a landing. Geology (Slide 20) Our two geologists traveled far from the Advance Base during both field seasons. Carrying fuel supplies (dog food) for a month, man food (dehydrated) and rock specimens acquired along the way, they covered a vast area. The surveyor drove his own dogs with the geophysicist as assistant. While the geologists were hacking away at rocks, the survey team lugged a theodolite up peaks to extend a triangulation network. Glaciology (Slides 21-22) The glaciologists each had an assistant from the support staff, so they could either travel together or divided into two parties to cover more ground. At each camp they dug a pit to determine the rate of snow accumulation, drilled (by hand) to a depth of 10 m to measure ice temperatures, and in places set up and surveyed ice-movement markers to be resurveyed the following season. Geophysics (Slides 33, 34-36, 38) The principal object was to determine the thickness of ice by seismic sounding the only means known at the time. After experiments as far as the Advance Base in the 1950-51 summer, both Weasels were devoted to a seismic sounding traverse in 1951-52 as far inland as supplies would allow. The party reached 620 km inland and found ice thicknesses of 2,500 m.

  3. COMPILATION OF DISPOSABLE SOLID WASTE CASK EVALUATIONS

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    THIELGES, J.R.; CHASTAIN, S.A.

    The Disposable Solid Waste Cask (DSWC) is a shielded cask capable of transporting, storing, and disposing of six non-fuel core components or approximately 27 cubic feet of radioactive solid waste. Five existing DSWCs are candidates for use in storing and disposing of non-fuel core components and radioactive solid waste from the Interim Examination and Maintenance Cell, ultimately shipping them to the 200 West Area disposal site for burial. A series of inspections, studies, analyses, and modifications were performed to ensure that these casks can be used to safely ship solid waste. These inspections, studies, analyses, and modifications are summarized andmore » attached in this report. Visual inspection of the casks interiors provided information with respect to condition of the casks inner liners. Because water was allowed to enter the casks for varying lengths of time, condition of the cask liner pipe to bottom plate weld was of concern. Based on the visual inspection and a corrosion study, it was concluded that four of the five casks can be used from a corrosion standpoint. Only DSWC S/N-004 would need additional inspection and analysis to determine its usefulness. The five remaining DSWCs underwent some modification to prepare them for use. The existing cask lifting inserts were found to be corroded and deemed unusable. New lifting anchor bolts were installed to replace the existing anchors. Alternate lift lugs were fabricated for use with the new lifting anchor bolts. The cask tiedown frame was modified to facilitate adjustment of the cask tiedowns. As a result of the above mentioned inspections, studies, analysis, and modifications, four of the five existing casks can be used to store and transport waste from the Interim Examination and Maintenance Cell to the disposal site for burial. The fifth cask, DSWC S/N-004, would require further inspections before it could be used.« less

  4. Nutritional status, nutrient intake and use of enzyme supplements in paediatric patients with Cystic Fibrosis; a European multicentre study with reference to current guidelines.

    PubMed

    Calvo-Lerma, Joaquim; Hulst, Jessie M; Asseiceira, Inês; Claes, Ine; Garriga, Maria; Colombo, Carla; Fornés, Victoria; Woodcock, Sandra; Martins, Tiago; Boon, Mieke; Ruperto, Mar; Walet, Sylvia; Speziali, Chiara; Witters, Peter; Masip, Etna; Barreto, Celeste; de Boeck, Kris; Ribes-Koninckx, Carmen

    2017-07-01

    The New European guidelines have established the most updated recommendations on nutrition and pancreatic enzyme replacement therapy (PERT) in CF. In the context of MyCyFAPP project - a European study in children with CF aimed at developing specific tools for improvement of self-management - the objective of the current study was to assess nutritional status, daily energy and macronutrient intake, and PERT dosing with reference to these new guidelines. Cross sectional study in paediatric patients with CF from 6 European centres. SD-scores for weight-for-age (WFA), height-for-age (HFA) and body mass index-for-age (BMI) were obtained. Through a specific 4-day food and enzyme-dose record, energy and macronutrients intake and PERT-use (LU/g lipids) were automatically calculated by the MyCyFAPP system. Comparisons were made using linear regression models. The lowest quartiles for BMI and HFA were between 0 and -1SD in all the centres with no significant differences, and 33.5% of the patients had a SD-score <0 for all three parameters. The minimum energy intake recommendation was not reached by 40% of the children and mean nutrients intake values were 14%, 51% and 34% of the total energy for protein, carbohydrates and lipids respectively. When assessed per centre, reported PERT doses were in the recommended range in only 13.8% to 46.6% of the patients; from 5.6% up to 82.7% of children were above the recommended doses and 3.3% to 75% were below. Among the 6 centres, a large variability and inconsistency with new guidelines on nutrition and PERT-use was found. Our findings document the lack of a general criterion to adjust PERT and suggest the potential benefit of educational and self-managerial tools to ensure adherence to therapies, both for clinical staff and families. They will be taken into account when developing these new tools during the next stages of MyCyFAPP Project. Copyright © 2017 European Cystic Fibrosis Society. Published by Elsevier B.V. All rights reserved.

  5. Hermes Transposon Mutagenesis Shows [URE3] Prion Pathology Prevented by a Ubiquitin-Targeting Protein: Evidence for Carbon/Nitrogen Assimilation Cross-Talk and a Second Function for Ure2p in Saccharomyces cerevisiae.

    PubMed

    Edskes, Herman K; Mukhamedova, Maryam; Edskes, Bouke K; Wickner, Reed B

    2018-05-16

    [URE3] is an amyloid-based prion of Ure2p, a regulator of nitrogen catabolism. While most variants of the [URE3] prion are toxic, mild variants that only slightly slow growth are more widely studied. The existence of several anti-prion systems suggests that some components may be protecting cells from potential detrimental effects of mild [URE3] variants. Our extensive Hermes transposon mutagenesis showed that disruption of YLR352W dramatically slows growth of [URE3-1] strains. Ylr352wp is an F-box protein, directing selection of substrates for ubiquitination by a cullin-containing E- 3 ligase. For efficient ubiquitylation, cullin-dependent E 3 ubiquitin ligases must be NEDDylated, modified by a ubiquitin-related peptide called NEDD8 (Rub1p in yeast). Indeed, we find that disruption of NEDDylation-related genes, RUB1, ULA1, UBA3 and UBC12 is also counterselected in our screen. We find that like ylr352w Δ [URE3] strains, ylr352w Δ ure2 Δ strains do not grow on non-fermentable carbon sources. Overexpression of Hap4p, a transcription factor stimulating expression of mitochondrial proteins, or mutation of GLN1 , encoding glutamine synthetase, allow growth of ylr352w Δ [URE3] strains on glycerol media. Supplying proline as a nitrogen source shuts off the nitrogen catabolite repression (NCR) function of Ure2p, but does not slow growth of ylr352w Δ strains, suggesting a distinct function of Ure2p in carbon catabolism. Also, gln1 mutations impair NCR, but actually relieve the growth defect of ylr352w Δ [URE3] and ylr352w Δ ure2 Δ strains, again showing that loss of NCR is not producing the growth defect and suggesting Ure2p has another function. YLR352W largely protects cells from the deleterious effects of otherwise mild [URE3] variants, or of a ure2 mutation (the latter a rarer event), and we name it LUG1 (lets [URE3]/ ure2 grow). Copyright © 2018, Genetics.

  6. Novel technique to ensure battery reliability in 42-V PowerNets for new-generation automobiles

    NASA Astrophysics Data System (ADS)

    Lam, L. T.; Haigh, N. P.; Phyland, C. G.; Huynh, T. D.

    The proposed 42-V PowerNet in automobiles requires the battery to provide a large number of shallow discharge-charge cycles at a high rate. High-rate discharge is necessary for engine cranking, while high-rate charge is associated with regenerative braking. The battery will therefore operate at these high rates in a partial-state-of-charge condition — 'HRPSoC duty'. Under simulated HRPSoC duty, it is found that the valve-regulated lead-acid (VRLA) battery fails prematurely due to the progressive accumulation of lead sulfate mainly on the surfaces of the negative plates. This is because the lead sulfate layer cannot be converted efficiently back to sponge lead during charging either from the engine or from the regenerative braking. Eventually, this layer of lead sulfate develops to such extent that the effective surface area of the plate is reduced markedly and the plate can no longer deliver the high-cranking current demanded by the automobile. The objective of this study is to develop and optimize a pulse-generation technique to minimize the development of lead sulfate layers on negative plates of VRLA batteries subjected to HRPSoC duty. The technique involves the application of sets of charging pulses of different frequency. It is found that the cycle-life performance of VRLA batteries is enhanced markedly when d.c. pulses of high frequency are used. For example, battery durability is raised from ˜10 600 cycles (no pulses) to 32 000 cycles with pulses of high frequency. Two key factors contribute to this improvement. The first factor is localization of the charging current on the surfaces of the plates — the higher the frequency, the greater is the amount of current concentrated on the plate surface. This phenomenon is known as the 'skin effect' as only the outer 'skin' of the plate is effectively carrying the current. The second factor is delivery of sufficient charge to the Faradaic resistance of the plate to compensate for the energy loss to inductance and double-layer capacitance effects. The Faradaic resistance represents the electrochemical reaction, i.e., conversion of lead sulfate to lead. The inductance simply results from the connection either between the cables and the terminals of the battery or between the terminals, bus-bars, and the lugs of the plates. The capacitance arises from the double layer which exists at the interface between the plate and the electrolyte solution. These findings have provided a demonstration and a scientific explanation of the benefit of superimposed pulsed current charging in suppressing the sulfation of negative plates in VRLA batteries operated under 42-V PowerNet and hybrid electric vehicle duties. A Novel Pulse™ device has been developed by the CSIRO. This device has the capability to be programmable to suite various applications and can be miniaturized to be encapsulated in the battery cover.

  7. The complete mitochondrial genomes of two rice planthoppers, Nilaparvata lugens and Laodelphax striatellus: conserved genome rearrangement in Delphacidae and discovery of new characteristics of atp8 and tRNA genes.

    PubMed

    Zhang, Kai-Jun; Zhu, Wen-Chao; Rong, Xia; Zhang, Yan-Kai; Ding, Xiu-Lei; Liu, Jing; Chen, Da-Song; Du, Yu; Hong, Xiao-Yue

    2013-06-22

    Nilaparvata lugens (the brown planthopper, BPH) and Laodelphax striatellus (the small brown planthopper, SBPH) are two of the most important pests of rice. Up to now, there was only one mitochondrial genome of rice planthopper has been sequenced and very few dependable information of mitochondria could be used for research on population genetics, phylogeographics and phylogenetic evolution of these pests. To get more valuable information from the mitochondria, we sequenced the complete mitochondrial genomes of BPH and SBPH. These two planthoppers were infected with two different functional Wolbachia (intracellular endosymbiont) strains (wLug and wStri). Since both mitochondria and Wolbachia are transmitted by cytoplasmic inheritance and it was difficult to separate them when purified the Wolbachia particles, concomitantly sequencing the genome of Wolbachia using next generation sequencing method, we also got nearly complete mitochondrial genome sequences of these two rice planthoppers. After gap closing, we present high quality and reliable complete mitochondrial genomes of these two planthoppers. The mitogenomes of N. lugens (BPH) and L. striatellus (SBPH) are 17, 619 bp and 16, 431 bp long with A + T contents of 76.95% and 77.17%, respectively. Both species have typical circular mitochondrial genomes that encode the complete set of 37 genes which are usually found in metazoans. However, the BPH mitogenome also possesses two additional copies of the trnC gene. In both mitochondrial genomes, the lengths of the atp8 gene were conspicuously shorter than that of all other known insect mitochondrial genomes (99 bp for BPH, 102 bp for SBPH). That two rearrangement regions (trnC-trnW and nad6-trnP-trnT) of mitochondrial genomes differing from other known insect were found in these two distantly related planthoppers revealed that the gene order of mitochondria might be conservative in Delphacidae. The large non-coding fragment (the A+T-rich region) putatively corresponding responsible for the control of replication and transcription of mitochondria contained a variable number of tandem repeats (VNTRs) block in different natural individuals of these two planthoppers. Comparison with a previously sequenced individual of SBPH revealed that the mitochondrial genetic variation within a species exists not only in the sequence and secondary structure of genes, but also in the gene order (the different location of trnH gene). The mitochondrial genome arrangement pattern found in planthoppers was involved in rearrangements of both tRNA genes and protein-coding genes (PCGs). Different species from different genera of Delphacidae possessing the same mitochondrial gene rearrangement suggests that gene rearrangements of mitochondrial genome probably occurred before the differentiation of this family. After comparatively analyzing the gene order of different species of Hemiptera, we propose that except for some specific taxonomical group (e.g. the whiteflies) the gene order might have diversified in family level of this order. The VNTRs detected in the control region might provide additional genetic markers for studying population genetics, individual difference and phylogeographics of planthoppers.

  8. The "DREAM" IODP project to drill the Mediterranean Salt Giant on the Balearic Promontory

    NASA Astrophysics Data System (ADS)

    Lofi, Johanna; Camerlenghi, Angelo; Aloisi, Giovanni; Maillard, Agnès; Garcia-Castellanos, Daniel; Huebscher, Christian; Kuroda, Junichiro

    2017-04-01

    Salt giants preserving kilometer-thick evaporite layers are the sedimentary expression of extreme environmental events of global relevance. Despite their global occurrence and general importance on Earth, there is currently no complete stratigraphic record through an un-deformed salt giant of marine origin. Similarly, there is a significant lack of knowledge about the factors controlling salt giants deposition, their early evolution, the impact they exert on the isostatic response of continental margins and on sub-salt formations, and the unprecedented deep biosphere they may harbor. The Mediterranean Messinian salt giant, which formed 5.5 Myrs ago, is one of the youngest salt giant on Earth and is currently lying below the Plio-Quaternary cover in a relatively un-deformed state close to its original depositional configuration. This salt giant is thus accessible by drilling and forms an ideal case study that could be used as a reference for older salt giants. However, since its discovery in 1970 during the DSDP Leg XIII, and despite 40 years or multi-disciplinary researches, this salt giant is still not fully understood and remains one of the longest-living controversies in Earth Science. In this context, the IODP DREAM project aims at exploring the Mediterranean salt giant by drilling with the JOIDES Resolution a transect of 4 sites on the southern margin of the Balearic promontory (Western Mediterranean). We identified this area as likely the only place in the Mediterranean where we could implement a shallow-to-deep transect of non-riser drilling sites. Due to the geological history and pre-structuration of the Promontory, MSC deposits are found preserved in a series of sedimentary basins lying at different water depths between the present-day coastline and the deep central salt basins. DREAM thus offers a unique opportunity to sample several hundred of meters of material forming the Mediterranean salt giant in varied water depths. This unique sedimentary record should allow testing 1) the contradictory emplacement models that explain its genesis and 2) the presence of halophilic micro-organisms it may host/feed. DREAM is a part of a bigger Multi-phase IODP Drilling Project entitled "Uncovering a Salt Giant" (857-MDP, coord. A. Camerlenghi) born out of a series of workshops and international initiatives carried out since 2014. The DREAM pre-proposal P857B has been accepted by the IODP Science Evaluation Panel in January 2016. The full-proposal will be submitted after the acquisition of complementary Site Survey Data in 2017. The DREAM project is performed in close link with various international initiatives including the COST Action CA15103 and ANR Project MEDSALT (Camerlenghi et al., this congress) and the IMMAGE ICDP-IODP amphibious proposal (Flecker et al., this congress). DREAM co-proponents: J. Anton, M.A. Bassetti, D. Birgel, R. Bourillot, A. Caruso, H. Daigle, G. DeLange, F. Dela Pierre, R. Flecker, V. Gaullier, D. Hodell, F. Jimenez-Espejo, W. Krijgsman, L. Lourens, S. Lugli, V. Manzi, T. McGenity, J. McKenzie, P. Meijer, H. Moreno, A. Moscariello, P. Munch, N. Ohkouchi, J. Peckmann, P. Pezard, J. Poort, M. Roveri, F. Sierro, K. Takai, T. Treude.

  9. The complete mitochondrial genomes of two rice planthoppers, Nilaparvata lugens and Laodelphax striatellus: conserved genome rearrangement in Delphacidae and discovery of new characteristics of atp8 and tRNA genes

    PubMed Central

    2013-01-01

    Background Nilaparvata lugens (the brown planthopper, BPH) and Laodelphax striatellus (the small brown planthopper, SBPH) are two of the most important pests of rice. Up to now, there was only one mitochondrial genome of rice planthopper has been sequenced and very few dependable information of mitochondria could be used for research on population genetics, phylogeographics and phylogenetic evolution of these pests. To get more valuable information from the mitochondria, we sequenced the complete mitochondrial genomes of BPH and SBPH. These two planthoppers were infected with two different functional Wolbachia (intracellular endosymbiont) strains (wLug and wStri). Since both mitochondria and Wolbachia are transmitted by cytoplasmic inheritance and it was difficult to separate them when purified the Wolbachia particles, concomitantly sequencing the genome of Wolbachia using next generation sequencing method, we also got nearly complete mitochondrial genome sequences of these two rice planthoppers. After gap closing, we present high quality and reliable complete mitochondrial genomes of these two planthoppers. Results The mitogenomes of N. lugens (BPH) and L. striatellus (SBPH) are 17, 619 bp and 16, 431 bp long with A + T contents of 76.95% and 77.17%, respectively. Both species have typical circular mitochondrial genomes that encode the complete set of 37 genes which are usually found in metazoans. However, the BPH mitogenome also possesses two additional copies of the trnC gene. In both mitochondrial genomes, the lengths of the atp8 gene were conspicuously shorter than that of all other known insect mitochondrial genomes (99 bp for BPH, 102 bp for SBPH). That two rearrangement regions (trnC-trnW and nad6-trnP-trnT) of mitochondrial genomes differing from other known insect were found in these two distantly related planthoppers revealed that the gene order of mitochondria might be conservative in Delphacidae. The large non-coding fragment (the A+T-rich region) putatively corresponding responsible for the control of replication and transcription of mitochondria contained a variable number of tandem repeats (VNTRs) block in different natural individuals of these two planthoppers. Comparison with a previously sequenced individual of SBPH revealed that the mitochondrial genetic variation within a species exists not only in the sequence and secondary structure of genes, but also in the gene order (the different location of trnH gene). Conclusion The mitochondrial genome arrangement pattern found in planthoppers was involved in rearrangements of both tRNA genes and protein-coding genes (PCGs). Different species from different genera of Delphacidae possessing the same mitochondrial gene rearrangement suggests that gene rearrangements of mitochondrial genome probably occurred before the differentiation of this family. After comparatively analyzing the gene order of different species of Hemiptera, we propose that except for some specific taxonomical group (e.g. the whiteflies) the gene order might have diversified in family level of this order. The VNTRs detected in the control region might provide additional genetic markers for studying population genetics, individual difference and phylogeographics of planthoppers. PMID:23799924

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