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Liquid hydrogen turbopump foil bearingSpace transfer vehicles and other power and propulsion systems require long-life turbopumps. Rolling element bearings used in current turbopumps do not have sufficient life for these applications. Process fluid foil bearings have established long life, with exceptional reliability, over a wide range of temperatures and fluids in many high-speed turbomachinery applications. However, liquid hydrogen turbopumps require high-load capacity bearings. An experimental study was conducted to measure foil journal bearing load capacity in liquid hydrogen, using a bearing designed specifically for cryogenic hydrogen turbopump applications. Additional performance parameters such as power loss, stability, cooling flow requirements, and bearing life were measured. These tests showed a load capacity safety factor of approximately 10 for liquid hydrogen turbopump applictions. These tests also demonstrated good rotor stability, low power loss and cooling flow, and long life.
Document ID
19910057078
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saville, M.
(Allied-Signal Aerospace Co. Torrance, CA, United States)
Gu, A.
(Allied-Signal Aerospace Co., Airesearch Los Angeles Div., Torrance CA, United States)
Capaldi, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 91-2108
Accession Number
91A41701
Distribution Limits
Public
Copyright
Other

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