Invention Application
US20130284398A1 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 审中-公开
气体涡轮发动机热管理系统

GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM
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.
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