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Elastohydrodynamic principles applied to the design of helicopter components.Elastohydrodynamic principles affecting the lubrication of transmission components are presented and discussed. Surface temperatures of the transmission bearings and gears affect elastohydrodynamic film thickness. Traction forces and sliding as well as the inlet temperature determine surface temperatures. High contact ratio gears cause increased sliding and may run at higher surface temperatures. Component life is a function of the ratio of elastohydrodynamic film thickness to composite surface roughness. Lubricant starvation reduces elastohydrodynamic film thickness and increases surface temperatures. Methods are presented which allow for the application of elastohydrodynamic principles to transmission design in order to increase system life and reliability.
Document ID
19730050286
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Townsend, D. P.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
AHS PREPRINT 770
Meeting Information
Meeting: Annual National Forum
Location: Washington, DC
Start Date: May 9, 1973
End Date: May 11, 1973
Sponsors: American Helicopter Society
Accession Number
73A35088
Distribution Limits
Public
Copyright
Other

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