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The Eccentuator: A new concept in actuationA new concept in actuation for aerospace mechanisms is presented. This actuator, called an 'eccentuator', features unique output characteristics, installation and envelope efficiencies, and relative simplicity. The actuator can be powered by either hydraulic or mechanical inputs. Potential applications of the 'eccentuator' and development efforts are discussed.
Document ID
19800015010
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Musgrove, R. G. (Vought Corp. Dallas, TX, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: NASA. Langley Res. Center Proc. of the 14th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
80N23501
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800015004Collected WorksProceedings of the 14th Aerospace Mechanisms Symposium
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