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Bearing tester data compilation, analysis, and reporting and bearing math modelingThe Shaberth bearing analysis computer program was developed for the analysis of jet engine shaft/bearing systems operating above room temperature with normal hydrocarbon lubricants. It is also possible to use this tool to evaluate the shaft bearing systems operating in cryogenics. Effects such as fluid drag, radial temperature gradients, outer race misalignments and clearance changes were simulated and evaluated. In addition, the speed and preload effects on bearing radial stiffness was evaluated. The Shaberth program was also used to provide contact stresses from which contact geometry was calculated to support other analyses such as the determination of cryogenic fluid film thickness in the contacts and evaluation of surface and subsurface stresses necessary for bearing failure evaluation. This program was a vital tool for the thermal analysis of the bearing in that it provides the heat generation rates at the rolling element/race contacts for input into a thermal model of the bearing/shaft assembly.
Document ID
19830026058
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
August 10, 1983
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-170856
SRS/SE-TR83-117
NAS 1.26:170856
Report Number: NASA-CR-170856
Report Number: SRS/SE-TR83-117
Report Number: NAS 1.26:170856
Accession Number
83N34329
Funding Number(s)
CONTRACT_GRANT: NAS8-34686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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