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
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