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Design, fabrication, and performance of foil journal bearing for the brayton rotating unitFoil bearings were designed and manufactured to replace pivoted-shoe journal bearings in an existing Brayton Cycle turbo-alternator-compressor. The design of this unconventional rotor support was accomplished within the constraints and space limitations imposed by the present machine, and the substitution of foil bearings was effected without changes or modification other machine components. A housing and a test rig were constructed to incorporate the new foil-bearing support into a unified assemble with an air-driven rotor and the gimbal-mounted thrust bearing, seals, and shrouds of an actual Brayton Rotating Unit. The foil bearing required no external pressure source, and stable self-acting rotation was achieved at all speeds up to 43,200 rpm. Excellent wipe-wear characteristics of the foil bearing permitted well over 1000 start-stop cycles with no deterioriation of performance in the entire speed range.
Document ID
19730019797
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Licht, L.
(Ampex Corp. Redwood City, CA, United States)
Branger, M.
(Ampex Corp. Redwood City, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1973
Publication Information
Publisher: NASA
Subject Category
Machine Elements And Processes
Report/Patent Number
RR-72-25
NASA-CR-2243
Report Number: RR-72-25
Report Number: NASA-CR-2243
Accession Number
73N28529
Funding Number(s)
CONTRACT_GRANT: NAS3-15341
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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