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Prestressed Composite PartsMatrix/fiber structural components strengthened by prestressing, according to proposal, increasing effective tensile strengths of components and enabling components to function in applications in which they otherwise fail. Reinforcing fibers stretched while encapsulated in matrix. After encapsulation, fibers released, placing matrix in lengthwise compression. Variety of fiber/matrix combinations fabricated this way. Prestressed quartz fibers encapsulated in ceramic matrix. Resulting composite used to make blade for gas turbine. Ceramic, normally weak in tension, has high strength and endures high temperature.
Document ID
19930000251
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Surls, Michael M.
(United Technologies Corp.)
Date Acquired
August 16, 2013
Publication Date
May 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 5
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
ISSN: 0145-319X
Report Number: MFS-28676
MFS-28676
Accession Number
93B10251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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