Factors contributing to the dynamic instability of ball retainers in precision bearings were investigated. A real-time, rolling-element bearing dynamics simulation was written (PADRE - Planar Analysis of a Dynamic Retainer) for rapid evaluation of key bearing design factors. This code permits economic screening of a large number of bearing geometric parameters as a prelude to other more comprehensive dynamic bearing codes. The simulation uses a recently-developed integration package to increase computational speed and accuracy, and also employs a simplified lubricant traction model due to Johnson and Tevaarwerk. Tests with precision angular-contact ball bearings verified important features of this analysis including friction threshold for instability, retainer motion, and the instability frequency. Retainer instability was found to be highly sensitive to retainer-ball friction and exhibited a constant characteristic frequency, which was independent of speed, external vibration, radial load, and preload.
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July 1992
Research Papers
An Analytical and Experimental Investigation of Ball Bearing Retainer Instabilities
E. A. Boesiger,
E. A. Boesiger
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
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A. D. Donley,
A. D. Donley
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
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S. Loewenthal
S. Loewenthal
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
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E. A. Boesiger
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
A. D. Donley
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
S. Loewenthal
Lockheed Missiles and Space Company, Sunnyvale, CA 94088
J. Tribol. Jul 1992, 114(3): 530-538 (9 pages)
Published Online: July 1, 1992
Article history
Received:
February 19, 1991
Revised:
June 1, 1991
Online:
June 5, 2008
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Boesiger, E. A., Donley, A. D., and Loewenthal, S. (July 1, 1992). "An Analytical and Experimental Investigation of Ball Bearing Retainer Instabilities." ASME. J. Tribol. July 1992; 114(3): 530–538. https://doi.org/10.1115/1.2920915
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