NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Operating limitations of high speed jet lubricated ball bearingsA parametric study was performed with 120-mm bore angular-contact ball bearings having a nominal contact angle of 20 degrees. The bearings had either an inner- or an outer-race land riding cage, and lubrication was by recirculating oil jets which had either a single or dual orifice. Thrust load, speed, and lubricant flow rate were varied. Test results were compared with those previously reported and obtained from bearings of the same design which were under-race lubricated but run under the same conditions. Jet lubricated ball bearings were limited to speeds less than 2,500,000 DN, and bearings having inner-race land riding cages produced lower temperatures than bearings with outer-race land riding cages. For a given lubricant flow rate dual orifice jets produced lower bearing temperatures than single orifice jets, but under-race lubrication produced lower bearing temperatures under all conditions of operation with no apparent bearing speed limitation.
Document ID
19750021356
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zaretsky, E. V.
(NASA Lewis Research Center Cleveland, OH, United States)
Signer, H.
(Industrial Tectonics, Inc. Cincinnati, United States)
Bamberger, E. N.
(GE Co.)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Mechanical Engineering
Report/Patent Number
E-8400
NASA-TM-X-71678
Report Number: E-8400
Report Number: NASA-TM-X-71678
Meeting Information
Meeting: Lubrication Conf.
Location: Miami Beach, FL
Country: United States
Start Date: October 21, 1975
End Date: October 23, 1975
Sponsors: Am. Soc. of Mechanical Engr., Am. Soc. of Lubrication Engr.
Accession Number
75N29429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available