F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 5/18 (2006.01) C23C 28/00 (2006.01) F01D 5/28 (2006.01) F01D 9/02 (2006.01)
Patent
CA 2372016
The present invention provides a turbine moving blade, a turbine stationary blade, and a turbine split ring which are capable of restraining the deterioration and peeling-off of a thermal barrier coating easily and surely, and a gas turbine capable of enhancing the energy efficiency by increasing the temperature of combustion gas. The turbine moving blade provided in a turbine constituting the gas turbine includes a platform having a gas path surface extending in the combustion gas flow direction, and a blade portion erecting on the platform. The thermal barrier coating covering the gas path surface is formed so as to go around from the gas path surface to an upstream-side end face and a downstream-side end face of the outer peripheral faces of the platform.
Kaneko Hideaki
Ohshima Kotaro
Shiozaki Shigehiro
Tomita Yasuoki
Yamaguchi Kengo
Fetherstonhaugh & Co.
Mitsubishi Heavy Industries Ltd.
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