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Microfog lubrication for aircraft engine bearingsAn analysis and system study was performed to provide design information regarding lubricant and coolant flow rates and flow paths for effective utilization of the lubricant and coolant in a once through bearing oil mist (microfog) and coolant air system. Both static and dynamic tests were performed. Static tests were executed to evaluate and calibrate the mist supply system. A total of thirteen dynamic step speed bearing tests were performed using four different lubricants and several different mist and air supply configurations. The most effective configuration consisted of supplying the mist and the major portion of the cooling air axially through the bearing. The results of these tests have shown the feasibility of using a once through oil mist and cooling air system to lubricate and cool a high speed, high temperature aircraft engine mainshaft bearing.
Document ID
19760021465
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rosenlieb, J. W.
(SKF Industries, Inc. King of Prussia, PA, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Mechanical Engineering
Report/Patent Number
SKF-AL75T032
NASA-CR-134977
Report Number: SKF-AL75T032
Report Number: NASA-CR-134977
Accession Number
76N28553
Funding Number(s)
CONTRACT_GRANT: NAS3-16826
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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