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Maximum life spur gear designOptimization procedures allow one to design a spur gear reduction for maximum life and other end use criteria. A modified feasible directions search algorithm permits a wide variety of inequality constraints and exact design requirements to be met with low sensitivity to initial guess values. The optimization algorithm is described, and the models for gear life and performance are presented. The algorithm is compact and has been programmed for execution on a desk top computer. Two examples are presented to illustrate the method and its application.
Document ID
19910014201
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Savage, M.
(Akron Univ. OH., United States)
Mackulin, M. J.
(Akron Univ. OH., United States)
Coe, H. H.
(NASA Lewis Research Center Cleveland, OH., United States)
Coy, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.15:104361
AD-A237143
AVSCOM-TR-90-C-024
E-6157
NASA-TM-104361
Report Number: NAS 1.15:104361
Report Number: AD-A237143
Report Number: AVSCOM-TR-90-C-024
Report Number: E-6157
Report Number: NASA-TM-104361
Meeting Information
Meeting: Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Sponsors: ASEE, SAE, AIAA, ASME
Accession Number
91N23514
Funding Number(s)
PROJECT: DA PROJ. 1L1-62211-37-A
CONTRACT_GRANT: NAG3-1047
PROJECT: RTOP 505-63-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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