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Gas turbine engine with pre-conditioned ceramic matrix composite components
A method of treating a component adapted for use in a gas turbine engine is described herein. The component may comprise ceramic matrix composite materials. The treatment to the ceramic matrix composite component may reduce or eliminate the wear or damage of crack propagation in the ceramic matrix composite component.
Gas turbine engine with pre-conditioned ceramic matrix composite components
A method of treating a component adapted for use in a gas turbine engine is described herein. The component may comprise ceramic matrix composite materials. The treatment to the ceramic matrix composite component may reduce or eliminate the wear or damage of crack propagation in the ceramic matrix composite component.
Gas turbine engine with pre-conditioned ceramic matrix composite components
WHITTLE MICHAEL J (author) / GALE LOUISE J (author) / PATTISON STEPHAN J (author) / RAZZELL ANTHONY G (author) / EDMONDS IAN M (author) / ABBOTT MICHAEL G (author)
2024-03-19
Patent
Electronic Resource
English
Gas turbine engine with pre-conditioned ceramic matrix composite components
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