发明名称 FLUID INJECTOR FOR COOLING A GAS TURBINE ENGINE COMPONENT
摘要 An example method of cooling a compressor of a gas turbine includes, among other things, diverting a flow from a compressor, and directing the flow at the compressor in a direction, the direction having a circumferential component and an axial component.
申请公布号 EP3044440(A1) 申请公布日期 2016.07.20
申请号 EP20140843887 申请日期 2014.09.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 POWELL, BRAD;BIFULCO, ANTHONY R.;CODERRE, PAUL E.;VIRTUE, JOHN P.;LUCKER, BRIAN E.
分类号 F02C7/12;F01D9/06;F01D25/12;F02C7/14;F02C7/18;F02K3/04;F04D29/54;F04D29/58 主分类号 F02C7/12
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