发明名称 Apparatus for cooling an airfoil for a gas turbine engine
摘要 A hollow airfoil is provided which includes a body, a trench, and a plurality of cooling apertures disposed within the trench. The body extends chordwise between a leading edge and a trailing edge, and spanwise between an outer radial surface and an inner radial surface, and includes an external wall surrounding a cavity. The trench is disposed in the external wall along the leading edge, extends in a spanwise direction, and is aligned with a stagnation line extending along the leading edge.
申请公布号 US6210112(B1) 申请公布日期 2001.04.03
申请号 US20000480956 申请日期 2000.01.11
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 TABBITA MARTIN G.;DOWNS JAMES P.;SOECHTING FRIEDRICH O.;AUXIER THOMAS A.
分类号 F01D5/18;(IPC1-7):F01D5/18;F01D9/06 主分类号 F01D5/18
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