发明名称 COOLING CONFIGURATION FOR ENGINE COMPONENT
摘要 This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The component further includes a cooling passageway provided in part by a helical wall between the first wall and the second wall.
申请公布号 WO2015076909(A2) 申请公布日期 2015.05.28
申请号 WO2014US54730 申请日期 2014.09.09
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 SNYDER, BROOKS E.;SLAVENS, THOMAS N.
分类号 F01D25/12;F01D9/02;F02C7/18 主分类号 F01D25/12
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