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High frequency drive mechanism for an active controls systems aircraft control surfaceThe mechanism was successfully utilized on a wind tunnel model tested in the transonic blow down tunnel. The mechanism is also applicable to a flying aircraft. Several interrelated mechanical subsystems were utilized, including a low inertia antibacklash drive mechanism for high frequency oscillation and a compact antibacklash drive mechanism for conversion of rotary motion to linear motion.
Document ID
19810013869
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, H. E. (Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: NASA. Marshall Space Flight Center The 15th Aerospace Mech. Symp.
Subject Category
Aircraft Stability And Control
Accession Number
81N22400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19810013857Collected Works15th Aerospace Mechanisms Symposium
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