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US09010126B2 Gas turbine engine with variable area fan nozzle bladder system 有权
具有可变面积风扇喷嘴膀胱系统的燃气轮机

Gas turbine engine with variable area fan nozzle bladder system
Abstract:
A turbofan engine includes a variable area fan nozzle which effectively changes the physical area and geometry within a fan bypass flow path to manipulate the pressure ratio of the bypass flow with a multitude of bladders circumferentially located about a core cowl.
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