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
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