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Future Trends for U.S. Naval Aviation Propulsion System Lubricants Naval Air Propulsion Center Trenton, NJ

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Shimski, John T., author.
Conference Name:
Aerospace Technology Conference & Exposition (1985-10-14 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1985
Summary:
Although present performance of aircraft gas turbine engine lubricants is satisfactory, two major areas have been targeted for improvement: static bearing corrosion and thermal stability of the oil. Trends in future engine designs indicate that waste heat rejection will be the limiting factor in the development of high temperature lubricants.Field experience has shown that present performance of aircraft gas turbine engine lubricants in helicopter gearbox systems is marginal. A three-phase program has been initiated to develop a separate lubricant with improved load-carrying capacity and corrosion inhibition. Future design requirements will have to incorporate new materials and lubricants concurrently
Notes:
Vendor supplied data
Publisher Number:
851835
Access Restriction:
Restricted for use by site license

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