Turbine components with thermal barrier coatings

C - Chemistry – Metallurgy – 04 – B

Patent

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Details

C04B 41/85 (2006.01) C04B 35/565 (2006.01) C04B 35/584 (2006.01) C04B 41/87 (2006.01) C04B 41/89 (2006.01) C09D 1/00 (2006.01) C09D 7/14 (2006.01) C23C 14/30 (2006.01) F01D 5/28 (2006.01) F01D 9/02 (2006.01) F01D 25/00 (2006.01) F02C 7/00 (2006.01) F23R 3/42 (2006.01)

Patent

CA 2500753

A turbine component has a substrate formed from a ceramic material selected from the group consisting of a monolithic ceramic material and a composite ceramic material and a thermal barrier coating bonded to the substrate. In one embodiment, the ceramic material forming the substrate is selected from the group of silicon nitride and self-reinforced silicon nitride. In another embodiment, the ceramic material forming the substrate is selected from the group consisting of a silicon carbide-silicon carbide material and a carbon-carbon material. At least one bond coat layer may be interposed between the substrate and the thermal barrier coating.

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