Gas turbine engine with trailing edge heat exchanger
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United States of America Patent
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May 23, 2023
Grant Date -
Oct 8, 2020
app pub date -
Apr 8, 2019
filing date -
Apr 8, 2019
priority date (Note) -
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Abstract
A gas turbine engine includes a fan assembly, a compressor assembly, a combustion chamber, a turbine assembly, a bypass duct conveying rearward a bypass airstream driven by the fan assembly when the gas turbine engine is in use, a fairing extending across at least a portion of the bypass duct downstream of the fan assembly, and a heat exchanger having an inlet fluidly connected to the compressor assembly and an outlet fluidly connected to a pneumatic actuator of the gas turbine engine. The fairing has a leading edge and a trailing edge. The heat exchanger is disposed adjacent the trailing edge of the fairing.
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