发明授权
US06811373B2 Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine 有权
涡轮动叶片,涡轮固定叶片,涡轮分裂环和燃气轮机

Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine
摘要:
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.
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