DocumentCode :
2439943
Title :
Failure Modes And Prognostic Techniques For H-60 Tail Rotor Drive System Bearings
Author :
Baker, Clint ; Marble, Sean ; Morton, Brogan P. ; Smith, Bert Joaquin
Author_Institution :
Sentient Corp., Idaho Falls
fYear :
2007
fDate :
3-10 March 2007
Firstpage :
1
Lastpage :
8
Abstract :
The failure modes and diagnostic/prognostic signatures for the oil cooler and hanger bearings used in the tail rotor drive system of the H-60 series of helicopters are being researched. The overall goal is to develop a prognosis system to track and predict bearing degradation and to integrate those technologies with the open architecture IMD-HUMS. This paper summarizes the challenges and advancements that have been experienced while improving the diagnostic capabilities for the bearings. The causes and effects of bearing contamination and lubricant exhaustion are addressed, while the focus is placed on detection methods of these failure modes. Interesting and encouraging results were found for both the oil cooler bearings and the hanger bearings, but at the present time, the potential is greatest for the development of detection methods and PHM algorithms for oil cooler bearings. The anticipated system will enable fault diagnosis, damage tracking, and the prognosis of useful life remaining.
Keywords :
aircraft maintenance; aircraft testing; failure (mechanical); failure analysis; fault diagnosis; helicopters; machine bearings; military aircraft; rotors; H-60 helicopters; IMD-HUMS; bearing contamination; damage tracking; fault diagnosis; hanger bearings; lubricant exhaustion; oil cooler; prognostic health management; prognostic techniques; tail rotor drive bearing; Condition monitoring; Fatigue; Fault diagnosis; Helicopters; Lubricants; Petroleum; Prognostics and health management; Signal processing algorithms; Tail; Vibrations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2007.352841
Filename :
4161636
Link To Document :
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