NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design and Operating Characteristics of High-Speed, Small-Bore, Angular-Contact Ball BearingsThe computer program SHABERTH was used to analyze 35-mm-bore, angular-contact ball bearings designed and manufactured for high-speed turbomachinery applications. Parametric tests of the bearings were conducted on a high-speed, high-temperature bearing tester and were compared with the computer predictions. Four bearing and cage designs were studied. The bearings were lubricated either by jet lubrication or through the split inner ring with and without outer-ring cooling. The predicted bearing life decreased with increasing speed because of increased operating contact stresses caused by changes in contact angle and centrifugal load. For thrust loads only, the difference in calculated life for the 24 deg. and 30 deg. contact-angle bearings was insignificant. However, for combined loading, the 24 deg. contact-angle bearing gave longer life. For split-inner-ring bearings, optimal operating conditions were obtained with a 24 deg. contact angle and an inner-ring, land-guided cage, using outer-ring cooling in conjunction with low lubricant flow rates. Lower temperature and power losses were obtained with a single-outer-ring, land-guided cage for the 24 deg. contact-angle bearing having a relieved inner ring and partially relieved outer ring. Inner-ring temperatures were independent of lubrication mode and cage design. In comparison with measured values, reasonably good engineering correlation was obtained using the computer program SHABERTH for predicted bearing power loss and for inner- and outer-ring temperatures. The Parker formula for XCAV (used in SHABERTH, a measure of oil volume in the bearing cavity) may need to be refined to reflect bearing lubrication mode, cage design, and location of cage-controlling land.
Document ID
19980234239
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pinel, Stanley I.
(Pinel Engineering Placentia, United States)
Signer, Hans R.
(Signer Technical Services Fullerton, CA United States)
Zaretsky, Erwin V.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1998
Subject Category
Mechanical Engineering
Report/Patent Number
NASA/TM-1998-206981
E-10702
NAS 1.15:206981
Report Number: NASA/TM-1998-206981
Report Number: E-10702
Report Number: NAS 1.15:206981
Funding Number(s)
PROJECT: RTOP 523-22-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available