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New methodology for shaft design based on life expectancyThe design of power transmission shafting for reliability has not historically received a great deal of attention. However, weight sensitive aerospace and vehicle applications and those where the penalties of shaft failure are great, require greater confidence in shaft design than earlier methods provided. This report summarizes a fatigue strength-based, design method for sizing shafts under variable amplitude loading histories for limited or nonlimited service life. Moreover, applications factors such as press-fitted collars, shaft size, residual stresses from shot peening or plating, corrosive environments can be readily accommodated into the framework of the analysis. Examples are given which illustrate the use of the method, pointing out the large life penalties due to occasional cyclic overloads.
Document ID
19860018189
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Loewenthal, S. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
E-3109
NASA-TM-87354
NAS 1.15:87354
Report Number: E-3109
Report Number: NASA-TM-87354
Report Number: NAS 1.15:87354
Meeting Information
Meeting: International Original Equipment Manufacturers Design Conference
Location: New York, NY
Country: United States
Start Date: December 9, 1986
End Date: December 11, 1986
Accession Number
86N27661
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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