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Fabrication process development of SiC/superalloy composite sheet for exhaust system componentsA chemical compatibility study was conducted between SiC filament and the following P/M matrix alloys: Waspaloy, Hastelloy-X, NiCrAlY, Ha-188, S-57, FeCrAlY, and Incoloy 800. None of the couples demonstrated sufficient chemical compatibility to withstand the minimum HIP consolidation temperatures (996 C) or intended application temperature of the composite (982 C). However, Waspaloy, Haynes 188, and Hastelloy-X were the least reactive with SiC of the candidate alloys. Chemical vapor deposited tungsten was shown to be an effective diffusion barrier between the superalloy matrix and SiC filament providing a defect-free coating of sufficient thickness. However, the coating breaks down when the tungsten is converted into intermetallic compounds by interdiffusion with matrix constituents. Waspaloy was demonstrated to be the most effective matrix alloy candidate in contact with the CVD tungsten barrier because of its relatively low growth rate constant of the intermediate compound and the lack of formation of Kirkendall voids at the matrix-barrier interface. Fabrication methods were developed for producing panels of uniaxial and angle ply composites utilizing CVD tungsten coated filament.
Document ID
19760010114
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cornie, J. A.
(Westinghouse Electric Corp. Pittsburgh, PA, United States)
Cook, C. S.
(Westinghouse Electric Corp. Pittsburgh, PA, United States)
Anderson, C. A.
(Westinghouse Electric Corp. Pittsburgh, PA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-134958
Report Number: NASA-CR-134958
Accession Number
76N17202
Funding Number(s)
CONTRACT_GRANT: NAS3-18921
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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