发明名称 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
摘要 A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
申请公布号 US2013202406(A1) 申请公布日期 2013.08.08
申请号 US201313799406 申请日期 2013.03.13
申请人 UNITED TECHNOLOGIES CORPORATION;UNITED TECHNOLOGIES CORPORATION 发明人 PAPA FEDERICO;PHILLIPS THOMAS G.;PHILLIPS KATHLEEN R.;STEARNS ETHAN K.;HEISS JUSTIN W.
分类号 F01D25/12 主分类号 F01D25/12
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