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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 computer program.
Document ID
19880013836
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Savage, M.
(Akron Univ. OH., United States)
Radil, K. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Lewicki, D. G.
(Army Aviation Research and Development Command St. Louis, Mo., United States)
Coy, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:100918
NASA-TM-100918
E-4173
AIAA PAPER 88-2979
AD-A195935
AVSCOM-TR-87-C-37
Report Number: NAS 1.15:100918
Report Number: NASA-TM-100918
Report Number: E-4173
Report Number: AIAA PAPER 88-2979
Report Number: AD-A195935
Report Number: AVSCOM-TR-87-C-37
Accession Number
88N23220
Funding Number(s)
PROJECT: RTOP 505-63-71
PROJECT: DA PROJ. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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