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
- 专利标题: Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine
- 专利标题(中): 涡轮动叶片,涡轮固定叶片,涡轮分裂环和燃气轮机
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申请号: US10067947申请日: 2002-02-08
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公开(公告)号: US06811373B2公开(公告)日: 2004-11-02
- 发明人: Yasuoki Tomita , Shigehiro Shiozaki , Kengo Yamaguchi , Hideaki Kaneko , Kotaro Ohshima
- 申请人: Yasuoki Tomita , Shigehiro Shiozaki , Kengo Yamaguchi , Hideaki Kaneko , Kotaro Ohshima
- 优先权: JP2001-062442 20010306
- 主分类号: F01D518
- IPC分类号: F01D518
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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