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Tapered Roller Bearing Damage Detection Using Decision Fusion AnalysisA diagnostic tool was developed for detecting fatigue damage of tapered roller bearings. Tapered roller bearings are used in helicopter transmissions and have potential for use in high bypass advanced gas turbine aircraft engines. A diagnostic tool was developed and evaluated experimentally by collecting oil debris data from failure progression tests conducted using health monitoring hardware. Failure progression tests were performed with tapered roller bearings under simulated engine load conditions. Tests were performed on one healthy bearing and three pre-damaged bearings. During each test, data from an on-line, in-line, inductance type oil debris sensor and three accelerometers were monitored and recorded for the occurrence of bearing failure. The bearing was removed and inspected periodically for damage progression throughout testing. Using data fusion techniques, two different monitoring technologies, oil debris analysis and vibration, were integrated into a health monitoring system for detecting bearing surface fatigue pitting damage. The data fusion diagnostic tool was evaluated during bearing failure progression tests under simulated engine load conditions. This integrated system showed improved detection of fatigue damage and health assessment of the tapered roller bearings as compared to using individual health monitoring technologies.
Document ID
20060045866
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dempsey, Paula J.
(NASA Glenn Research Center Cleveland, OH, United States)
Kreider, Gary
(Timken Co. North Canton, OH, United States)
Fichter, Thomas
(Timken Co. North Canton, OH, United States)
Date Acquired
August 23, 2013
Publication Date
July 1, 2006
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2006-214380
E-15658
Funding Number(s)
WBS: WBS 581-02-07-03-03
Distribution Limits
Public
Copyright
Public Use Permitted.
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