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Advanced Composite PistonsNew concept involving improved configuration of reinforcing fibers and improved fabrication process proposed to improve thermal and mechanical properties of composite piston structures. Reduces amount of labor necessary to manufacture piston structures, with attendant reductions in costs. Single knitted-carbon-fiber sock used to form external surfaces of piston. Advantages include elimination of heavy dependence on inherently weak interlaminar properties of carbon-carbon; ease of automation to reduce fabrication costs; readily modifiable architecture to vary mechanical properties to desired values; and reduction in number of elements required to fabricate pistons. Advantage of piston structures lies in applications where light weight and high specific performance primary considerations.
Document ID
19900000496
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Taylor, Allan H.
(NASA Langley Research Center, Hampton, VA.)
Ransone, Philip O.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 9
ISSN: 0145-319X
Subject Category
Fabrication Technology
Report/Patent Number
LAR-13926
Accession Number
90B10496
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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