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Flexible Robotic ArmA plurality of identical modules are serially connected together with each module including a base plate and a top plate interconnected by a universal joint assembly so that the top plate is adapted to pivotally nutate around the base plate to describe a cone in space. An array of twenty-four electromagnets, sequentially energized in sets of three, are arranged in a ring around the periphery of the base plate. Selective energization of the eight sets of electromagnets causes the rim of the top plate to be magnetically attracted to the energized electromagnets. The tilt of the top pivot plate is detected and controlled over a range of 360°, thus permitting a series string of modules to assume any desired elongated configuration.
Document ID
19920024390
Acquisition Source
Goddard Space Flight Center
Document Type
Other - Patent
External Source(s)
GSC-13161-1
Authors
Israel A Moya
(Goddard Space Flight Center Greenbelt, United States)
Philip A Studer
(Goddard Space Flight Center Greenbelt, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1992
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Mechanical Engineering
Accession Number
92N33634
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,142,932
Patent Application
US-PATENT-APPL-SN-754828
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