公开(公告)号：US20130161414A1

公开(公告)日：2013-06-27

申请号：US13769599

申请日：2013-02-18

申请人： Rohr, Inc. ,  Goodrich Actuation Systems Limited

发明人： Jihad I. Ramlaoui ,  Geoffrey Pinto ,  Daniel Shetzer ,  Daniel M. Amkraut ,  Andrew Robert Hawksworth ,  John Harvey ,  Alan K. Evans ,  Vikram Chandarana ,  Roger Moorehouse

IPC分类号： F02K1/76

CPC分类号： F02K1/763 ,  F02K1/09 ,  F02K1/30 ,  F02K1/70 ,  F02K1/72 ,  F02K3/06 ,  F05D2250/34 ,  Y10T74/18576 ,  Y10T74/18648

摘要： A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.

摘要翻译： 用于涡轮风扇发动机的可变区域风扇喷嘴组件包括具有后缘的机舱和具有后缘的平移推力反向器套筒。 推力反向器套筒可移动地设置在机舱的后边缘的后部并且可以在前进位置和后部位置之间移动。 具有前边缘的平移风扇喷嘴可移动地设置在后缘的后面，并且可在收起位置和展开位置之间移动。 当风扇喷嘴处于展开位置时，在后缘和前缘之间限定上游旁路流出口。 可延伸致动系统构造成使风扇喷嘴在收起位置和展开位置之间移动。

公开(公告)号：US20160169158A9

公开(公告)日：2016-06-16

申请号：US13769599

申请日：2013-02-18

申请人： ROHR, INC. ,  GOODRICH ACTUATION SYSTEMS LIMITED

发明人： Jihad I. Ramlaoui ,  Geoffrey Pinto ,  Daniel Shetzer ,  Daniel M. Amkraut ,  Andrew Robert Hawksworth ,  John Harvey ,  Alan K. Evans ,  Vikram Chandarana ,  Roger Moorehouse

IPC分类号： F02K1/76

CPC分类号： F02K1/763 ,  F02K1/09 ,  F02K1/30 ,  F02K1/70 ,  F02K1/72 ,  F02K3/06 ,  F05D2250/34 ,  Y10T74/18576 ,  Y10T74/18648

摘要： A variable area fan nozzle assembly for a turbofan engine includes a nacelle having an aft edge and a translating thrust reverser sleeve with a trailing edge. The thrust reverser sleeve is movably disposed aft of the nacelle's aft edge and is movable between a forward position and an aft position. A translating fan nozzle having a forward edge is movably disposed behind the trailing edge, and is movable between a stowed position and a deployed position. An upstream bypass flow exit is defined between the trailing edge and the forward edge when the fan nozzle is in the deployed position. An extendable actuation system is configured to move the fan nozzle between the stowed position and the deployed position.