发明名称 Translating variable area fan nozzle providing an upstream bypass flow exit
摘要 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.
申请公布号 US8402765(B2) 申请公布日期 2013.03.26
申请号 US20090485551 申请日期 2009.06.16
申请人 AMKRAUT DANIEL M.;LAYLAND MICHAEL JOHN;JAMES NORMAN JOHN;ROHR, INC. 发明人 AMKRAUT DANIEL M.;LAYLAND MICHAEL JOHN;JAMES NORMAN JOHN
分类号 F02K1/09;F02K1/70;F02K3/075 主分类号 F02K1/09
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