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Method of making carbon fiber-carbon matrix reinforced ceramic compositesA method of making a carbon fiber-carbon matrix reinforced ceramic composite wherein the result is a carbon fiber-carbon matrix reinforcement is embedded within a ceramic matrix. The ceramic matrix does not penetrate into the carbon fiber-carbon matrix reinforcement to any significant degree. The carbide matrix is a formed in situ solid carbide of at least one metal having a melting point above about 1850 degrees centigrade. At least when the composite is intended to operate between approximately 1500 and 2000 degrees centigrade for extended periods of time the solid carbide with the embedded reinforcement is formed first by reaction infiltration. Molten silicon is then diffused into the carbide. The molten silicon diffuses preferentially into the carbide matrix but not to any significant degree into the carbon-carbon reinforcement. Where the composite is intended to operate between approximately 2000 and 2700 degrees centigrade for extended periods of time such diffusion of molten silicon into the carbide is optional and generally preferred, but not essential.
Document ID
20080009444
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Williams, Brian
Benander, Robert
Date Acquired
August 24, 2013
Publication Date
November 20, 2007
Subject Category
Composite Materials
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-10/824,746
Patent Number: US-Patent-7,297,368
Funding Number(s)
CONTRACT_GRANT: NAS8-99093
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,297,368
Patent Application
US-Patent-Appl-SN-10/824,746
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