发明名称 |
Turbine airfoil and method for controlling a temperature of a turbine airfoil |
摘要 |
<p>According to one aspect of the invention, a turbine airfoil (200) includes a platform (202) and a blade (204) extending from the platform (202). The airfoil (200) also includes a slot (208) formed in a slashface (210) of the platform (202), the slot (208) being configured to receive a pressurized fluid via passages (212) and configured to direct the pressurized fluid to a selected region of the turbine airfoil (200). The pressurized fluid forms a barrier to restrict the flow of hot gas accross the slashface (210), thus improving the airfoil life. And corresponding method for controlling the temperature of the airfoil.</p> |
申请公布号 |
EP2557274(A2) |
申请公布日期 |
2013.02.13 |
申请号 |
EP20120179235 |
申请日期 |
2012.08.03 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SMITH, AARON EZEKIEL;BOYER, BRADLEY;GIGLIO, ANTHONY LOUIS;GUSTAFSON, ROSS JAMES;PENNY, CHRISTOSPHER MICHAEL |
分类号 |
F01D11/04;F01D11/00 |
主分类号 |
F01D11/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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