发明名称 GAS TURBINE ENGINE COMPONENT HAVING VARIABLE WIDTH FEATHER SEAL SLOT
摘要 A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a mate face and a feather seal slot axially extending along the mate face, the feather seal slot having a variable width along a portion of its axial length.
申请公布号 EP2964934(A4) 申请公布日期 2016.11.23
申请号 EP20140760315 申请日期 2014.03.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BOEKE, MARK A.;RAJCHEL, KEVIN;SALZILLO,RICHARD M.;DEGRAY, JEFFREY J.;MAINELLI, ALLISON
分类号 F02C7/28;F01D5/22;F01D9/04;F01D11/00;F02C9/16 主分类号 F02C7/28
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