发明名称 GAS TURBINE ENGINE COMPONENT HAVING CURVED TURBULATOR
摘要 A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall that forms a portion of an outer periphery of at least one cavity and at least one curved turbulator that extends from said wall.
申请公布号 EP2954168(A2) 申请公布日期 2015.12.16
申请号 EP20140787682 申请日期 2014.01.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BLAKE, MOSHESHE CAMARA-KHARY;OSBORNE, LISA K.;SLAVENS, THOMAS N.
分类号 F01D5/14;F01D5/18;F01D25/08;F02C7/12;F04D29/38;F04D29/58 主分类号 F01D5/14
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