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Method of Fabricating Chopped-Fiber Composite PistonA three-dimensional piston molding is fabricated from a mixture of chopped, carbon tow filaments of variable length, which are prepregged with carbonaceous organic resins and/or pitches and molded by conventional molding processes into a near net shape, to form a carbon-fiber reinforced organic-matrix composite part. Continuous reinforcement in the form of carbon-carbon composite tapes or pieces of fabric can be also laid in the mold before or during the charging of the mold with the chopped-fiber mixture, to enhance the strength in the crown and wrist-pin areas. The molded chopped-fiber reinforced organic-matrix composite parts are then pyrolized in an inert atmosphere, to convert the organic matrix materials to carbon. These pyrolized parts are then densified by reimpregnation with resins or pitches, which are subsequently carbonized. Densification is also accomplished by direct infiltration with carbon by vapor deposition processes. Once the desired density has been achieved, the piston molds are machined to final piston dimensions, and piston ring grooves are added. To prevent oxidation and/or to seal the piston surface or near surface, the chopped-fiber piston is coated with ceramic and/or metallic sealants: and/or coated with a catalyst.
Document ID
19990111588
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Rivers, H. Kevin
(NASA Langley Research Center Hampton, VA United States)
Ransone, Philip O.
(NASA Langley Research Center Hampton, VA United States)
Northam, G. Burton
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 19, 2013
Publication Date
September 7, 1999
Subject Category
Composite Materials
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-816403
Patent Application Number: US-Patent-Appl-SN-012930
Patent Number: US-Patent-5,948,330
Patent Number: NASA-Case-LAR-15643-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-5,948,330|NASA-Case-LAR-15643-1
Patent Application
US-Patent-Appl-SN-816403|US-Patent-Appl-SN-012930
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