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Gimbal bearing design considerations and friction controlThe design considerations of bearing selection, bearing fits, bearing installation, and thermal control are discussed for a gimbal with a high stiffness, low friction torque requirement. Tradeoffs between a quad set of small diameter spread apart or a large diameter bearing pair resulted in a cleaner, lighter, stiffer unit with the latter selection. Bearing fits were designed to eliminate clearances with tolerances of .00127 mm 00005 in) on the bearing shafts and housings. The problems in metrology are discussed and a perferred technique for measurement of small cross-section bearings described. A technique for installation to assure proper seating of the bearing is offered. Where transient thermal conditions are involved, a method of controlling bearing friction by active control of bearing temperature gradients including the use of bearing unload test curves is described.
Document ID
19790014375
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kramer, N. R.
(Hughes Aircraft Co. Culver City, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Johnson Space Center The 13th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
79N22546
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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