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Performance of gas-lubricated nonconforming pivoted-pad journal bearings and a flexibly mounted spiral-groove thrust bearingA test program was conducted to determine the performance characteristics of gas-lubricated nonconforming pivoted-pad journal bearings and a spiral-groove thrust bearing designed for the Brayton cycle rotating unit (BRU). Hydrostatic, hybrid (simultaneously hydrostatic and hydrodynamic), and hydrodynamic tests were conducted in argon gas at ambient pressure and temperature ranges representative of hydrostatic operation up to the 10.5-kWe BRU power-generating level. Performance of the gas lubricated bearings is presented, including hydrostatic gas flow rates, bearing clearances, bearing temperatures, and transient performance.
Document ID
19730015359
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ream, L. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-2765
E-7269
Accession Number
73N24086
Funding Number(s)
PROJECT: RTOP 503-35
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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