发明名称 CONTOURED BLADE OUTER AIR SEAL FOR A GAS TURBINE ENGINE
摘要 A blade outer air seal (BOAS) segment according to an exemplary aspect of the present disclosure includes, among other things, a seal body having a radially inner face that circumferentially extend between a first mate face and a second mate face and axially extend between a leading edge face and a trailing edge face, wherein a radial position of the radially inner face varies at a given axial position.
申请公布号 WO2014171997(A2) 申请公布日期 2014.10.23
申请号 WO2014US14593 申请日期 2014.02.04
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LUTJEN, PAUL M.;BRUSKOTTER, MICHAEL J.
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