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Bearing Tester Data Compilation Analysis, and Reporting and Bearing Math ModelingThe magnitude and direction of fluid induced torques and forces on the 57 mm bearing cage is considered to be a contributing factor in possible cage instabilities that can produce intermittent high heating in the bearing. Analyses of the fluid forces and torques are presented. Heat generated by viscous fluid work was estimated for two flow diverter configurations and a coolant flow of 10 lbs/sec to support the thermal evaluation of the LOX Bearing Materials Tester. Results of the analysis of the LOX turbopump turbine end bearings are discussed. Coolant velocities for the no. 4 LOX turbopump turbine end bearings were estimated as a function of shaft speed and coolant flow rate. Contact angles and track width data were developed for the 57 mm bearing as functions of shaft speed, and axial and radial loads. The Advanced Dynamics of Rolling Elements (ADORE) computer program was installed on the MSFC UNIVAC 1100 and a test case successfully run. Both the text output and the plotting output were verified. The Bearing Seal and Materials Tester - Test Condition Data Base was developed. The parametric analysis of the operating characteristics of the LOX turbopump pump end bearing using the 45 mm bearing thermal model was begun.
Document ID
19910020289
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
January 1, 1985
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-178883
SRS/STD-PR-535/11
REPT-535
NAS 1.26:178883
Report Number: NASA-CR-178883
Report Number: SRS/STD-PR-535/11
Report Number: REPT-535
Report Number: NAS 1.26:178883
Accession Number
91N29603
Funding Number(s)
CONTRACT_GRANT: NAS8-36183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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