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Carbon-Carbon Piston ArchitecturesAn improved structure for carbon-carbon composite piston architectures is disclosed. The improvement consists of replacing the knitted fiber, three-dimensional piston preform architecture described in U.S. Pat.No. 4,909,133 (Taylor et al.) with a two-dimensional lay-up or molding of carbon fiber fabric or tape. Initially, the carbon fabric of tape layers are prepregged with carbonaceous organic resins and/or pitches and are laid up or molded about a mandrel, to form a carbon-fiber reinforced organic-matrix composite part shaped like a "U" channel, a "T"-bar, or a combination of the two. The molded carbon-fiber reinforced organic-matrix composite part is then pyrolized in an inert atmosphere, to convert the organic matrix materials to carbon. At this point, cylindrical piston blanks are cored from the "U"-channel, "T"-bar, or combination part. These blanks 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 billets are machined to final piston dimensions; coated with oxidation sealants; and/or coated with a catalyst. When compared to conventional steel or aluminum alloy pistons, the use of carbon-carbon composite pistons reduces the overall weight of the engine; allows for operation at higher temperatures without a loss of strength; allows for quieter operation; reduces the heat loss; and reduces the level of hydrocarbon emissions.
Document ID
20010008192
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)
Schwind, Francis A.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
September 12, 2000
Subject Category
Composite Materials
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-012930
Patent Application Number: US-Patent-Appl-SN-291717
Patent Application Number: US-Patent-Appl-SN-805195
Patent Number: NASA-Case-LAR-15492-2
Patent Number: US-Patent-6,116,202
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-LAR-15492-2|US-Patent-6,116,202
Patent Application
US-Patent-Appl-SN-012930|US-Patent-Appl-SN-291717|US-Patent-Appl-SN-805195
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