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Electrical rotary joint apparatus for large space structuresA structural array and electrical rotary joint for transmitting an electrical power between large space structures having relative rotational movement is disclosed which includes large support framework structures which rotate relative to one another about a common axis of rotation. A rotary interface joint is defined between the structures. A cylindrical hub member is carried by one structure and a cylindrical hub member is carried by a support structure with a third hub member being concentrically within a fourth hub member for relative rotation. Tension connecting cables connect hub members with their associated outer structures whereby relative rotational movement between the structures is transmitted to the cylindrical hub members for unitary motion therewith. Electrical conductor brush members are carried by one hub and electrical contact rings are carried by another hub member in sliding electrical contact with the brushes for transmission of electrical power during relative rotational movement between the two support structures.
Document ID
19830012673
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Belew, R. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Boehme, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
February 4, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-231543
Patent Number: US-PATENT-4,377,266
Patent Number: NASA-CASE-MFS-23981-1
Accession Number
83N20944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,377,266|NASA-CASE-MFS-23981-1
Patent Application
US-PATENT-APPL-SN-231543
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