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Strengthening of oxidation resistant materials for gas turbine applicationsSilicon nitride and silicon carbide ceramics were treated to form compressive surface layers. On the silicon carbide, quenching and thermal exposure treatments were used, and on the silicon nitride, quenching, carburizing, and a combination of quenching and carburizing were used. In some cases substantial improvements in impact resistance and/or flexural strength were observed. The presence of compressive surface stresses was demonstrated by slotted rod tests.
Document ID
19750002020
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kirchner, H. P.
(Ceramic Finishing Co. State College, PA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-134661
Report Number: NASA-CR-134661
Accession Number
75N10092
Funding Number(s)
CONTRACT_GRANT: NAS3-16788
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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