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Dynamic tooth loads and stressing for high contact ratio spur gearsAn analysis and computer program were developed for calculating the dynamic gear tooth loading and root stressing for high contact ratio gearing (HCRG) as well as LCRG. The analysis includes the effects of the variable tooth stiffness during the mesh, tooth profile modification, and gear errors. The calculation of the tooth root stressing caused by the dynamic gear tooth loads is based on a modified Heywood gear tooth stress analysis, which appears more universally applicable to both LCRG and HCRG. The computer program is presently being expanded to calculate the tooth contact stressing and PV values. Sample application of the gear program to equivalent LCRG (1.566 contact ratio) and HCRG (2.40 contact ratio) revealed the following: (1) the operating conditions and dynamic characteristics of the gear system an affect the gear tooth loading and root stressing, and therefore, life significantly; (2) the length of the profile modification affect the tooth loading and root stressing significantly, the amount depending on the applied load, speed, and contact ratio; and (3) the effect of variable tooth stiffness is small, shifting and increasing the response peaks slightly from those for constant tooth stiffness.
Document ID
19830011877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cornell, R. W.
(Hamilton Standard Div., United Aircraft Corp. Windsor Locks, CT, United States)
Westervelt, W. W.
(Hamilton Standard Div., United Aircraft Corp. Windsor Locks, CT, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Advanced Power Transmission Technol.
Subject Category
Mechanical Engineering
Accession Number
83N20148
Funding Number(s)
CONTRACT_GRANT: NAS3-17859
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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