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Application of traction drives as servo mechanismsThe suitability of traction drives for a wide class of aerospace control mechanisms is examined. Potential applications include antenna or solar array drive positioners, robotic joints, control moment gyro (CMG) actuators and propeller pitch change mechanisms. In these and similar applications the zero backlash, high torsional stiffness, low hysteresis and torque ripple characteristics of traction drives are of particular interest, as is the ability to run without liquid lubrication in certain cases. Wear and fatigue considerations for wet and dry operation are examined along with the tribological performance of several promising self lubricating polymers for traction contracts. The speed regulation capabilities of variable ratio traction drives are reviewed. A torsional stiffness analysis described suggests that traction contacts are relatively stiff compared to gears and are significantly stiffer than the other structural elements in the prototype CMG traction drive analyzed. Discussion is also given of an advanced turboprop propeller pitch change mechanism that incorporates a traction drive.
Document ID
19850025207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Loewenthal, S. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Rohn, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Steinetz, B. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: NASA. Ames Research Center 19th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
85N33520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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