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Centrifugal regulator for control of deployment rates of deployable elementsThe requirements, design, and performance of a centrifugal regulator aimed at limiting deployment rates of deployable elements are discussed. The overall mechanism is comprised of four distinct functional parts in a machined housing: (1) the centrifugal brake device, which checks the payout of a deployment cable; (2) the reducing gear, which produces the spin rate necesary for the braking device; (3) the payout device, which allows the unwinding of the cable; and (4) the locking device, which prevents untimely unwinding. The centrifugal regulator is set into operation by a threshold tension of the cable which unlocks the mechanism and allows unwinding. The pulley of the windout device drives the centrifugal brake with the help of the reducing gear. The centrifugal force pushes aside weights that produce friction of the studs in a cylindrical housing. The mechanism behaved well at qualification temperature and vibrations.
Document ID
19800015013
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vermalle, J. C.
(Societe Nationale Industrielle Aerospatiale Paris, France)
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
80N23504
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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