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Method of fabricating composite structuresA method of fabricating structures formed from composite materials by positioning the structure about a high coefficient of thermal expansion material, wrapping a graphite fiber overwrap about the structure, and thereafter heating the assembly to expand the high coefficient of thermal expansion material to forcibly compress the composite structure against the restraint provided by the graphite overwrap. The high coefficient of thermal expansion material is disposed about a mandrel with a release system therebetween, and with a release system between the material having the high coefficient of thermal expansion and the composite material, and between the graphite fibers and the composite structure. The heating may occur by inducing heat into the assembly by a magnetic field created by coils disposed about the assembly through which alternating current flows. The method permits structures to be formed without the use of an autoclave.
Document ID
19910006020
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Sigur, W. A.
(Martin Marietta Corp. New Orleans, LA., United States)
Date Acquired
September 6, 2013
Publication Date
September 15, 1990
Subject Category
Composite Materials
Report/Patent Number
NAS 1.71:MFS-28390-1
Report Number: NAS 1.71:MFS-28390-1
Patent Application Number: US-PATENT-APPL-SN-578043
Patent Number: NASA-CASE-MFS-28390-1
Accession Number
91N15333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MFS-28390-1
Patent Application
US-PATENT-APPL-SN-578043
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