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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 />

97

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