NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Lubrication and performance of high-speed rolling-element bearingsTrends in aircraft engine operating speeds have dictated the need for rolling-element bearings capable of speeds to 3 million DN. A review of high-speed rolling-element bearing state-of-the-art performance and lubrication is presented. Through the use of under-race lubrication and bearing thermal management bearing operation can be obtained to speeds of 3 million DN. Jet lubricated ball bearings are limited to 2.5 million DN for large bore sizes and to 3 million DN for small bore sizes. Current computer programs are able to predict bearing thermal performance.
Document ID
19850013348
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zaretsky, E. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Schuller, F. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Coe, H. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-86958
NAS 1.15:86958
E-2362
Report Number: NASA-TM-86958
Report Number: NAS 1.15:86958
Report Number: E-2362
Meeting Information
Meeting: 1985 Ann. Meeting of the American Society of Lubrications Engineers
Location: Las Vegas, NV
Country: United States
Start Date: May 6, 1985
End Date: May 9, 1985
Accession Number
85N21658
Funding Number(s)
PROJECT: RTOP 505-33-7C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available