Invention Grant
US08402765B2 Translating variable area fan nozzle providing an upstream bypass flow exit 有权
翻译可变区域风扇喷嘴,提供上游旁路流出口

Translating variable area fan nozzle providing an upstream bypass flow exit
Abstract:
A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating nozzle segment having a forward edge and a first end. The nozzle segment is movably disposed behind the aft edge such that an upstream bypass flow exit is defined between the aft edge and the forward edge when the nozzle segment is in a deployed position. A deflector is disposed between the aft edge and the forward edge proximate to the first end. The deflector substantially prevents bypass flow from exiting the upstream bypass flow exit in a region that is proximate to the first end.
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