NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
System life and reliability modeling for helicopter transmissionsA computer program which simulates life and reliability of helicopter transmissions is presented. The helicopter transmissions may be composed of spiral bevel gear units and planetary gear units - alone, in series or in parallel. The spiral bevel gear units may have either single or dual input pinions, which are identical. The planetary gear units may be stepped or unstepped and the number of planet gears carried by the planet arm may be varied. The reliability analysis used in the program is based on the Weibull distribution lives of the transmission components. The computer calculates the system lives and dynamic capacities of the transmission components and the transmission. The system life is defined as the life of the component or transmission at an output torque at which the probability of survival is 90 percent. The dynamic capacity of a component or transmission is defined as the output torque which can be applied for one million output shaft cycles for a probability of survival of 90 percent. A complete summary of the life and dynamic capacity results is produced by the program.
Document ID
19860015519
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Savage, M.
(Akron Univ. Akron, OH, United States)
Brikmanis, C. K.
(Akron Univ. Akron, OH, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:3967
E-2889
NASA-CR-3967
Report Number: NAS 1.26:3967
Report Number: E-2889
Report Number: NASA-CR-3967
Accession Number
86N24990
Funding Number(s)
CONTRACT_GRANT: NAG3-55
PROJECT: RTOP 505-62-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available