NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Hybrid hydrostatic/ball bearings in high-speed turbomachineryA high speed, high pressure liquid hydrogen turbopump was designed, fabricated, and tested under a previous contract. This design was then modified to incorporate hybrid hydrostatic/ball bearings on both the pump end and turbine end to replace the original conventional ball bearing packages. The design, analysis, turbopump modification, assembly, and testing of the turbopump with hybrid bearings is presented here. Initial design considerations and rotordynamic performance analysis was made to define expected turbopump operating characteristics and are reported. The results of testing the turbopump to speeds of 9215 rad/s (88,000 rpm) using a wide range of hydrostatic bearing supply pressures are presented. The hydrostatic bearing test data and the rotordynamic behavior of the turbopump was closely analyzed and are included in the report. The testing of hybrid hydrostatic/ball bearings on a turbopump to the high speed requirements has indicated the configuration concept is feasible. The program has presented a great deal of information on the technology requirements of integrating the hybrid bearing into high speed turbopump designs for improved bearing life.
Document ID
19830018942
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nielson, C. E.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-168124
NAS 126:168124
RI/RD83-104
NAS 1.26:168124
Report Number: NASA-CR-168124
Report Number: NAS 126:168124
Report Number: RI/RD83-104
Report Number: NAS 1.26:168124
Accession Number
83N27213
Funding Number(s)
CONTRACT_GRANT: NAS3-22480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available