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A computer solution for the dynamic load, lubricant film thickness, and surface temperatures in spiral-bevel gearsA computer method for determining the dynamic load between spiral bevel pinion and gear teeth contact along the path of contact is described. The dynamic load analysis governs both the surface temperature and film thickness. Computer methods for determining the surface temperature, and film thickness are presented along with results obtained for a pair of typical spiral bevel gears.
Document ID
19830011869
Document Type
Conference Paper
Authors
Chao, H. C.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Baxter, M.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Cheng, H. S.
(Northwestern Univ.)
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
83N20140
Funding Number(s)
CONTRACT_GRANT: NSG-2143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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