Integrated thermal management system for fuel cooling
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United States of America Patent
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Oct 25, 2022
Grant Date -
Oct 22, 2020
app pub date -
Apr 8, 2020
filing date -
Apr 17, 2019
priority date (Note) -
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Abstract
A thermal management system for a gas turbine engine includes a primary vapor compression system including a primary evaporator defining thermal communication between a primary refrigerant and a flow of fuel to cool the fuel. A boost vapor compression system includes a boost heat exchanger defining thermal communication between the primary refrigerant. A boost refrigerant cools the primary refrigerant and a boost condenser in thermal communication with an air stream cools the boost refrigerant.
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