An apparatus and method are disclosed for a gas turbine engine including an offtake located within the air flow of the engine. The offtake has an inlet and a louver covering the inlet. The louver has multiple airfoils arranged to direct the air flow into the inlet of the offtake.
Gas turbine engine with an offtake
2019-12-10
Patent
Electronic Resource
English
DESIGN TO MINIMISE TANKER OFFTAKE HAZARDS
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