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Analysis of oil lubricated, fluid film, thrust bearings with allowance for temperature dependent viscosityA preliminary design study was performed to seek a fluid-film thrust bearing design intended to be part of a high-speed, hybrid (rolling element/fluid film) bearing configuration. The base line used is a design previously tested. To improve the accuracy of theoretical predictions of load capacity, flow rate, and friction power loss, an analytical procedure was developed to include curvature effects inherent in thrust bearings and to allow for the temperature rise in the fluid due to viscous heating. Also, a narrow-groove approximation in the treatment of the temperature field was formulated to apply the procedure to the Whipple thrust bearing. A comparative trade-off study was carried out assuming isothermal films; its results showed the shrouded-step design to be superior to the Whipple design for the intended application. An extensive parametric study was performed, employing isoviscous calculations, to determine the optimized design, which was subsequently recalculated allowing for temperature effects.
Document ID
19720018725
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pan, C. H. T.
(Mechanical Technology, Inc. Latham, NY, United States)
Malanoski, S. B.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Publication Information
Publisher: NASA
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-2052
MTI-71TR32
Report Number: NASA-CR-2052
Report Number: MTI-71TR32
Accession Number
72N26375
Funding Number(s)
CONTRACT_GRANT: NAS3-14399
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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