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Thermal cyclic durability testing of ceramic materials for turbine enginesThe thermal cyclic durability of commercial ceramic materials for turbine engines was under evaluation since 1978. Ceramic materials are exposed to cyclic diesel-fired burner exhaust at either 1204 or 1371 C (2200 or 2500 F) for up to 3500 hours. The test conditions are selected to simulate the environment experienced by the hot flow path components in an automotive gas turbine engine. The silicon nitride and silicon carbide materials tested are the same ceramic materials currently used on the AGT100 and AGT101 ceramic turbine engine program.
Document ID
19880014502
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lindberg, L. J.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA, Lewis Research Center, Structural Ceramics
Subject Category
Quality Assurance And Reliability
Accession Number
88N23886
Funding Number(s)
CONTRACT_GRANT: DEN3-27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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