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New innovations in compositesProcedures for manufacturing metal clad graphite resin structural elements applicable to optical systems requiring precisely controlled thermal and mechanical properties are described. Analytical estimates were made of the material properties that can be obtained for various ratios of graphite epoxy and aluminum cladding. Three graphite fiber systems were evaluated. Two manufacturing processes are described. One method is a procedure for manufacturing long tubes by wrapping aluminum foil over dry graphite fiber. Resin was applied by spreading before applying the aluminum wrap. A second approach, offering the opportunity for precise tuning of the coefficient of expansion, is by die flattening metal tubing through which a measured amount of fiber has been drawn. Prior to flattening, resin is injected, and after flattening or shaping the part is cured. This latter procedure offers the opportunity to fine tune the structure to achieve a CTE with a precision equal to that of the measuring systems-by modifying the number of fiber tows prior to manufacturing or by etching the metal after manufacturing. Experimental verification and demonstration data are presented for Gr/E bars with aluminum and steel skins.
Document ID
19850033895
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bluck, R. M.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Johnson, R. R.
(Lockheed Missiles and Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Composite Materials
Meeting Information
Meeting: Technology vectors
Location: Reno, NV
Start Date: April 3, 1984
End Date: April 5, 1984
Accession Number
85A16046
Funding Number(s)
CONTRACT_GRANT: NAS1-14887
Distribution Limits
Public
Copyright
Other

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