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Bearing tester data compilation, analysis, and reporting and bearing math modelingA test condition data base was developed for the Bearing and Seal Materials Tester (BSMT) program which permits rapid retrieval of test data for trend analysis and evaluation. A model was developed for the Space shuttle Main Engine (SSME) Liquid Oxygen (LOX) turbopump shaft/bearing system. The model was used to perform parametric analyses to determine the sensitivity of bearing operating characteristics and temperatures to variations in: axial preload, contact friction, coolant flow and subcooling, heat transfer coefficients, outer race misalignments, and outer race to isolator clearances. The bearing program ADORE (Advanced Dynamics of Rolling Elements) was installed on the UNIVAC 1100/80 computer system and is operational. ADORE is an advanced FORTRAN computer program for the real time simulation of the dynamic performance of rolling bearings. A model of the 57 mm turbine-end bearing is currently being checked out. Analyses were conducted to estimate flow work energy for several flow diverter configurations and coolant flow rates for the LOX BSMT.
Document ID
19860014468
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-178748
NAS 1.26:178748
SRS/STD-TR86-014-535
Report Number: NASA-CR-178748
Report Number: NAS 1.26:178748
Report Number: SRS/STD-TR86-014-535
Accession Number
86N23939
Funding Number(s)
CONTRACT_GRANT: NAS8-36183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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