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Evaluation of a high-torque backlash-free roller actuatorThe results are presented of a test program that evaluated the stiffness, accuracy, torque ripple, frictional losses, and torque holding capability of a 16:1 ratio, 430 N-m (320 ft-lb) planetary roller drive for a potential space vehicle actuator application. The drive's planet roller supporting structure and bearings were found to be the largest contributors to overall drive compliance, accounting for more than half the total. In comparison, the traction roller contacts themselves contributed only 9 percent of the drive's compliance based on an experimentally verified stiffnesss model. Torque ripple tests showed the drive to be extremely smooth, actually providing some damping of input torsional oscillations. The drive also demonstrated the ability to hold static torque with drifts of 7 arc sec or less over a 24-hour period at 35 percent of full load.
Document ID
19880013855
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Steinetz, Bruce M.
(Army Aviation Systems Command Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA, Lewis Research Center, Lewis Structures Technology, 1988. Volume 1: Structural Dynamics
Subject Category
Mechanical Engineering
Accession Number
88N23239
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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