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A Systems Approach to the Solid Lubrication of Foil Air Bearings for Oil-Free TurbomachineryFoil air bearings are self-acting hydrodynamic bearings which rely upon solid lubricants to reduce friction and minimize wear during sliding which occurs at start-up and shut-down when surface speeds are too low to allow the formation of a hydrodynamic air film. This solid lubrication is typically accomplished by coating the non-moving foil surface with a thin, soft polymeric film. The following paper introduces a systems approach in which the solid lubrication is provided by a combination of self lubricating shaft coatings coupled with various wear resistant and lubricating foil coatings. The use of multiple materials, each providing different functions is modeled after oil-lubricated hydrodynamic sleeve bearing technology which utilizes various coatings and surface treatments in conjunction with oil lubricants to achieve optimum performance. In this study, room temperature load capacity tests are performed on journal foil air bearings operating at 14,000 rpm. Different shaft and foil coating technologies such as plasma sprayed composites, ceramic, polymer and inorganic lubricant coatings are evaluated as foil bearing lubricants. The results indicate that bearing performance is improved through the individual use of the lubricants and treatments tested. Further, combining several solid lubricants together yielded synergistically better results than any material alone.
Document ID
20020090934
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
DellaCorte, Christopher
(NASA Glenn Research Center Cleveland, OH United States)
Zaldana, Antonio R.
(NASA Glenn Research Center Cleveland, OH United States)
Radil, Kevin C.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2002
Subject Category
Chemistry And Materials (General)
Report/Patent Number
E-13250
NAS 1.15:211482
ARL-TR-2867
NASA/TM-2002-211482
Report Number: E-13250
Report Number: NAS 1.15:211482
Report Number: ARL-TR-2867
Report Number: NASA/TM-2002-211482
Funding Number(s)
PROJECT: DA Proj. 1L1-61102-AH-45
PROJECT: RTOP 708-18-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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