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Two gimbal bearing case studies: Some lessons learnedTwo troublesome, torque related problems associated with gimbal actuators are discussed. Large, thin section angular contact bearings can have a surprisingly high torque sensitivity to radial thermal gradients. A predictive thermal-mechanical bearing analysis, as described, was helpful in establishing a safe temperature operating envelope. In the second example, end-of-travel torque limits of an oscillatory gimbal bearing appoached motor stall during limit cycling life tests. Bearing modifications required to restore acceptable torque performance are described. The lessons learned from these case studies should benefit designers of precision gimbals where singular bearing torque related problems are not uncommon.
Document ID
19880012103
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Loewenthal, Stuart H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA. Langley Research Center, The 22nd Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
88N21487
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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