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Elevated temperature durability of ceramic materialsFast fracture, stress rupture, and cyclic high temperature durability characterizations have been conducted for advanced silicon carbide and silicon nitride ceramics applicable to gas turbine hot section components. The fast fracture and stress rupture tests were conducted in four-point flexure at temperatures of up to 1540 C; the durability tests involved cycling specimens to temperatures of 1370 C and air quenching at 200 C for up to 3500 hrs. Materials with further reliability improvements are noted to be required for gas turbine hot section component applications.
Document ID
19880057516
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lindberg, Laura J.
(Allied-Signal Aerospace Co. Phoenix, AZ, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA PAPER 88-3055
Report Number: AIAA PAPER 88-3055
Accession Number
88A44743
Funding Number(s)
CONTRACT_GRANT: DEN3-167
CONTRACT_GRANT: DEN3-27
Distribution Limits
Public
Copyright
Other

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