Issue 10 Volume 41 May 16, 2003
Issue 10 Volume 41 May 16, 2003
Issue 10 Volume 41 May 16, 2003
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PoRTIA, a small CdZnTe balloon instrument that was flown three times in three different shielding configurations. PoRTIA<br />
was passively shielded during its first flight from Palestine, Texas and actively shielded as a piggyback instrument on the GRIS<br />
balloon experiment during its second and third flights from Alice Springs, Australia, using the thick GRIS Nal anticoincidence<br />
shield. A significant CdZnTe background reduction was achieved during the third flight with PoRTIA placed completely inside<br />
the GRIS shield and blocking crystal, and thus completely surrounded by 15 cm of Nal. A unique balloon altitude background<br />
data set is provided by CdZnTe and Ge detectors simultaneously surrounded by the same thick anticoincidence shield; the<br />
presence of a single coxial Ge detector inside the shield next to PoRTIA allowed a measurement of the ambient neutron flux<br />
inside the shield throughout the flight. These neutrons interact with the detector material to produce isomeric states of the Cd,<br />
Zn and Te nuclei that radiatively decay; calculations are presented that indicate that these decays may explain most of the fully<br />
shielded CdZnTe background.<br />
Author<br />
Balloon-Borne Instruments; Gamma Rays; X Rays; Anticoincidence Detectors; Electromagnetic Shielding; Sensitivity<br />
Analysis; Measuring Instruments<br />
<strong>2003</strong>0034606 NASA Glenn Research Center, Cleveland, OH, USA<br />
Effects on Diagnostic Parameters After Removing Additional Synchronous Gear Meshes<br />
Decker, Harry J.; April <strong>2003</strong>; 14 pp.; In English; 57th Meeting of the Society for Machinery Failure Prevention Technology<br />
(MFPT), 14-18 Apr. <strong>2003</strong>, Virginia Beach, VA, USA; Original contains color illustrations<br />
Contract(s)/Grant(s): WBS-22-708-87-12; DA Proj. 1L1-61<strong>10</strong>2-AF-20<br />
Report No.(s): NASA/TM-<strong>2003</strong>-212312; NAS 1.15:212312; E-13899; ARL-TR-2933; No Copyright; Avail: CASI; A03,<br />
Hardcopy<br />
Gear cracks are typically difficult to diagnose with sufficient time before catastrophic damage occurs. Significant damage<br />
must be present before algorithms appear to be able to detect the damage. Frequently there are multiple gear meshes on a<br />
single shaft. Since they are all synchronous with the shaft frequency, the commonly used synchronous averaging technique<br />
is ineffective in removing other gear mesh effects. Carefully applying a filter to these extraneous gear mesh frequencies can<br />
reduce the overall vibration signal and increase the accuracy of commonly used vibration metrics. The vibration signals from<br />
three seeded fault tests were analyzed using this filtering procedure. Both the filtered and unfiltered vibration signals were then<br />
analyzed using commonly used fault detection metrics and compared. The tests were conducted on aerospace quality spur<br />
gears in a test rig. The tests were conducted at speeds ranging from 2500 to 5000 revolutions per minute and torques from<br />
184 to 228 percent of design load. The inability to detect these cracks with high confidence results from the high loading which<br />
is causing fast fracture as opposed to stable crack growth. The results indicate that these techniques do not currently produce<br />
an indication of damage that significantly exceeds experimental scatter.<br />
Author<br />
Systems Health Monitoring; Gear Teeth; Fracture Mechanics; Synchronous Motors; Crack Propagation; Grid Generation<br />
(Mathematics)<br />
<strong>2003</strong>0036936 National Inst. of Standards and Technology (CSTL), Gaithersburg, MD<br />
Wear Mechanisms of Valves and Valve Seat Inserts in a Gas-Fired Reciprocating Engine<br />
Lacey, P. I.; Hsu, S. M.; Gates, R. S.; Lee, S.; Ives, L.; Jun. 1990; 80 pp.; In English<br />
Report No.(s): PB<strong>2003</strong>-<strong>10</strong>14<strong>10</strong>; NISTIR-90-4264; No Copyright; Avail: CASI; A05, Hardcopy<br />
The objective of the report is to quantitatively measure wear and to identify the dominant wear mechanisms experienced<br />
by selected valve and valve seat insert combinations during operation in a natural gas-fueled reciprocating engine.<br />
NTIS<br />
Valves; Wear Tests; Piston Engines<br />
<strong>2003</strong>0037026 National Renewable Energy Lab., Golden, CO<br />
Durability of Solar Reflective Materials with an Alumina Hard Coat Produced by Ion-Bean-Assisted Deposition<br />
Kennedy, C. E.; Smilgys, R. V.; Oct. 2002; In English<br />
Report No.(s): DE2002-15002207; No Copyright; Avail: National Technical Information Service (NTIS)<br />
A promising low-cost reflector material for solar concentrating power (CSP) generation is a silvered substrate protected<br />
by an alumina coating several microns thick. The alumina hard coat is deposited under high vacuum by ion-beam-assisteddeposition<br />
(IBAD). Samples of this material have been produced both by batch and continuous roll-coating processes. The<br />
substrate materials investigated were polyethylene terephthalate (PET), PET laminated to stainless-steel foil, and chrome-<br />
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