发明名称 GAS TURBINE ENGINE DUCT ASSEMBLY
摘要 A duct assembly according to an exemplary aspect of the present disclosure includes, among other things, a casing body that extends between a flange and a wall, a first discrete cooling passage formed in the casing body and a second discrete cooling passage circumferentially spaced from the first discrete cooling passage. At least one of the first discrete cooling passage and the second discrete cooling passage includes an axial portion and a tangential portion configured to turn a cooling fluid communicated in each of the first and second discrete cooling passages.
申请公布号 EP3036418(A1) 申请公布日期 2016.06.29
申请号 EP20140837738 申请日期 2014.08.13
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BLANEY, KEN F.;STEVENS, MICHAEL S.
分类号 F02C7/12;F01D25/12;F02C7/18;F04D29/58 主分类号 F02C7/12
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