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Graphite/Epoxy Deicing HeaterHeat applied close to surface protected. One ply of highly electrically- and thermally-conductive brominated-graphite fiber composite laminated between two plies of electrically-insulating composite material, with michel foil making contact with end portions of graphite fibers. Part of foil exposed beyond composite to serve as electrical contact. Graphite/Epoxy composite heater developed to prevent and reverse formation of ice on advanced composite surfaces of aircraft.
Document ID
19880000377
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Hung, Ching-Cheh
(NASA Lewis Research Center, Cleveland, Ohio.)
Dillehay, Michael E.
(Cleveland State University)
Stahl, Mark
(Cleveland State University)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 7
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-14551
Accession Number
88B10377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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