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Computerized life and reliability modelling for turboprop transmissionsA generalized life and reliability model is presented for parallel shaft geared prop-fan and turboprop aircraft transmissions. The transmission life and reliability model is a combination of the individual reliability models for all the bearings and gears in the main load paths. The bearing and gear reliability models are based on classical fatigue theory and the two parameter Weibull failure distribution. A computer program was developed to calculate the transmission life and reliability. The program is modular. In its present form, the program can analyze five different transmission arrangements. However, the program can be modified easily to include additional transmission arrangements. An example is included which compares the life of a compound two-stage transmission with the life of a split-torque, parallel compound two-stage transmission as calculated by the comaputer program.
Document ID
19880060804
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Savage, M.
(Akron, University OH, United States)
Radil, K. C.
(Akron Univ. Akron, OH, United States)
Lewicki, D. G.
(U.S. Army, Propulsion Directorate, Cleveland OH, United States)
Coy, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 88-2979
Accession Number
88A48031
Distribution Limits
Public
Copyright
Other

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