GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
    21.
    发明申请
    GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 审中-公开
    气体涡轮发动机热管理系统

    公开(公告)号:US20130284398A1

    公开(公告)日:2013-10-31

    申请号:US13926154

    申请日:2013-06-25

    Abstract: A thermal management system according to an exemplary aspect of the present disclosure includes, among other things, a first fluid circuit that selectively communicates a first portion of a first conditioned fluid having a first temperature to a first gas turbine engine system and a second portion of the first conditioned fluid having a second temperature to a second gas turbine engine system. The second temperature is a greater temperature than the first temperature. A second fluid circuit circulates a second conditioned fluid that is different from the first conditioned fluid to a third gas turbine engine system.

    Abstract translation: 根据本公开的示例性方面的热管理系统尤其包括第一流体回路,其将具有第一温度的第一调节流体的第一部分选择性地连通到第一燃气涡轮发动机系统,第二部分 第一调节流体具有第二温度到第二燃气涡轮发动机系统。 第二温度是比第一温度更高的温度。 第二流体回路将与第一调节流体不同的第二调节流体循环到第三燃气涡轮发动机系统。

Patent Agency Ranking