Invention Grant
US08127547B2 Gas turbine engine with air and fuel cooling system 有权
燃气涡轮发动机配有空气和燃油冷却系统

Gas turbine engine with air and fuel cooling system
Abstract:
A gas turbine engine is provided with a first heat exchanger associated with a cooling air flow to deliver cooling air to a turbine section. A second heat exchanger is associated with a fuel supply line for delivering fuel into a combustion section. An intermediate fluid cools air at the first heat exchanger and heats fuel at the second heat exchanger.
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