发明名称 TRAILING EDGE COOLING
摘要 An airfoil includes a leading edge, a trailing edge, a suction surface, a pressure surface, a cooling passageway, and a plurality of oblong pedestals. The suction surface and the pressure surface both extend axially between the leading edge and the trailing edge, as well as radially from a root section to a tip section of the airfoil. The cooling passageway is located between the suction surface and the pressure surface. The oblong pedestals connect the suction surface to the pressure surface at the trailing edge of the airfoil.
申请公布号 EP2828514(A1) 申请公布日期 2015.01.28
申请号 EP20130764958 申请日期 2013.03.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ZESS, GARY A.;SPANGLER, BRANDON W.;MONGILLO, DOMINIC J.
分类号 F02K3/00;F01D5/18;F01D25/08;F02C7/14 主分类号 F02K3/00
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