THERMAL MANAGEMENT SYSTEM FOR GAS TURBINE ENGINE
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 throug...
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Main Author | |
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Format | Patent |
Language | English |
Published |
01.11.2012
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Subjects | |
Online Access | Get full text |
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Summary: | 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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Bibliography: | Application Number: US201113096130 |