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Investigation of Bearing Fatigue Damage Life Prediction Using Oil Debris MonitoringResearch was performed to determine if a diagnostic tool for detecting fatigue damage of helicopter tapered roller bearings can be used to determine remaining useful life (RUL). The taper roller bearings under study were installed on the tail gearbox (TGB) output shaft of UH- 60M helicopters, removed from the helicopters and subsequently installed in a bearing spall propagation test rig. The diagnostic tool was developed and evaluated experimentally by collecting oil debris data during spall progression tests on four bearings. During each test, data from an on-line, in-line, inductance type oil debris sensor was monitored and recorded for the occurrence of pitting damage. Results from the four bearings tested indicate that measuring the debris generated when a bearing outer race begins to spall can be used to indicate bearing damage progression and remaining bearing life.
Document ID
20110023753
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dempsey, Paula J.
(NASA Glenn Research Center Cleveland, OH, United States)
Bolander, Nathan
(Sentient Corp. Idaho Falls, ID, United States)
Haynes, Chris
(Sentient Corp. Idaho Falls, ID, United States)
Toms, Allison M.
(GasTOPS Ltd. Pensacola, FL, United States)
Date Acquired
August 25, 2013
Publication Date
November 1, 2011
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-2011-217117
E-17804
Report Number: NASA/TM-2011-217117
Report Number: E-17804
Funding Number(s)
WBS: WBS 877868.02.07.03.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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