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OH-58 helicopter transmission failure analysisThe OH-58 main transmission gearbox was run at varying output torques, speeds, and oil cooling rates. The gearbox was subsequently run to destruction by draining the oil from the gearbox while operating at a speed of 6200 revs per minute and 36,000 inch-pounds output torque. Primary cause of gearbox failure was overheating and melting of the planet bearing aluminum cages. Complete failure of the gearbox occurred in 28 1/2 minutes after the oil pressure dropped to zero. The alternating and maximum stresses in the gearbox top case were approximately 10 percent of the endurance limit for the material. Deflection of the bevel gear at 67000 inch-pounds output torque indicate a marginal stiffness for the bevel gear supporting system.
Document ID
19760008977
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Townsend, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Coy, J. J.
(Army Air Mobility Res. and Develop. Lab. Cleveland, United States)
Hatvani, B. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-71867
E-8633
Report Number: NASA-TM-X-71867
Report Number: E-8633
Accession Number
76N16065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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