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Analytical and experimental spur gear tooth temperature as affected by operating variablesA gear tooth temperature analysis was performed using a finite element method combined with a calculated heat input, calculated oil jet impingement depth, and estimated heat transfer coefficients. Experimental measurements of gear tooth average surface temperatures and instanteous surface temperatures were made with a fast response infrared radiometric microscope. Increased oil jet pressure had a significant effect on both average and peak surface temperatures at both high load and speeds. Increasing the speed at constant load and increasing the load at constant speed causes a significant rise in average and peak surface temperatures of gear teeth. The oil jet pressure required for adequate cooling at high speed and load conditions must be high enough to get full depth penetration of the teeth. Calculated and experimental results were in good agreement with high oil jet penetration but showed poor agreement with low oil jet penetration depth.
Document ID
19800010129
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Townsend, D. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Akin, L. S.
(Western Gear Corp. Industry, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Mechanical Engineering
Report/Patent Number
E-342
NASA-TM-81419
Report Number: E-342
Report Number: NASA-TM-81419
Meeting Information
Meeting: Intern. Power Transmission and Gearing Conf.
Location: San Francisco, CA
Country: United States
Start Date: August 18, 1980
End Date: August 22, 1980
Sponsors: Am. Soc. of Mech. Engr.
Accession Number
80N18403
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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