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Spring control of wire harness loopsNegator spring control guides wire harness between movable and fixed structure. It prevents electrical wire harness loop from jamming or being severed as wire moves in response to changes in position of aircraft rudder. Spring-loaded coiled cable controls wire loop regardless of rudder movement.
Document ID
19780000411
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Curcio, P. J.
(Fairchild Republic Co.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MSC-18246
Accession Number
78B10411
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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