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US08904753B2 Thermal management system for gas turbine engine 有权
燃气轮机发动机热管理系统

Thermal management system for gas turbine engine
Abstract:
A thermal management system for a gas turbine engine includes a first heat exchanger and a second heat exchanger in communication with a bypass flow through an inlet. A valve is operable to selectively communicate the bypass flow to either the first heat exchanger or the second heat exchanger through the inlet.
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