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Foil bearings for axial and radial support of high speed rotors: Design, development, and determination of operating characteristicsFlexible surface thrust and journal foil bearings were fabricated, and their performance was demonstrated, both individually and jointly as a unified rotor support system. Experimental results are documented with graphs and oscilloscopic data of trajectories, waveforms, and scans of amplitude response. At speeds of 40,000 to 45,000 rpm and a mean clearance of the order of 15 to 20 micrometers (600 to 800 micrometers, the resilient, air lubricated, spiral groove thrust bearings support a load of 127 N (29 lb; 13 kgf), equivalent to 3.0 N/sq cm (4.5 lb/sq in 0.31 kgf sq cm). Journal bearings with polygonal sections provided stable and highly damped supports at speeds up to 50,000 rpm.
Document ID
19780009445
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Licht, L.
(Licht (L.) San Mateo, TX, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-2940
Accession Number
78N17388
Funding Number(s)
CONTRACT_GRANT: N00014-76-C-0191
CONTRACT_GRANT: NASA ORDER C-75012-C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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