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    Flow directing element and a method of manufacturing a flow directing element
    11.
    发明授权
    Flow directing element and a method of manufacturing a flow directing element 失效
    流动引导元件和制造流动引导元件的方法

    公开(公告)号：US06725541B1

    公开(公告)日：2004-04-27

    申请号：US10396480

    申请日：2003-03-26

    申请人： Michael J Holme ,  Jeffrey C Bishop

    发明人： Michael J Holme ,  Jeffrey C Bishop

    IPC分类号： B21K2500

    CPC分类号： F02K1/70 ,  F02K1/54 ,  F05D2230/20 ,  F05D2250/183 ,  Y02T50/672 ,  Y10T29/4932 ,  Y10T29/49321 ,  Y10T29/49323 ,  Y10T29/49346 ,  Y10T29/49922

    摘要： A thrust reverser cascade flow directing element (28) for a gas turbine engine (10) comprises a plurality of plates (30) and a plurality of flow directing vanes (40). At least one vane (40) extends between each pair of plates (30), the plurality of plates (30) are formed from sheet material and a single integral piece of ductile sheet material (32) forms the plurality of flow directing vanes (40). The single integral piece of ductile sheet material (32) has a plurality of longitudinally spaced apart apertures (36) and a plurality of longitudinally spaced apart sheet material portions (38) between the apertures (36) and the ductile sheet material (32) is bent at a plurality of longitudinally spaced positions such that each sheet material portion (38) defines one of the plurality of flow directing vanes (40).

    摘要翻译： 用于燃气涡轮发动机（10）的推力反向器级联流动引导元件（28）包括多个板（30）和多个导流叶片（40）。 至少一个叶片（40）在每对板（30）之间延伸，多个板（30）由片材形成，并且单个整体的延性片材（32）形成多个导流叶片（40） ）。 延伸片材材料（32）的单个整体件具有多个纵向间隔开的孔（36），并且在孔（36）和延性片材（32）之间的多个纵向间隔开的片材部分（38） 在多个纵向间隔位置处弯曲，使得每个片材部分（38）限定多个导流叶片（40）中的一个。

    Jet engine nozzle with variable thrust vectoring and exhaust area
    12.
    发明授权
    Jet engine nozzle with variable thrust vectoring and exhaust area 失效

    公开(公告)号：US06546716B2

    公开(公告)日：2003-04-15

    申请号：US09842178

    申请日：2001-04-26

    申请人： Jean-Pierre Lair

    发明人： Jean-Pierre Lair

    IPC分类号： F02K110

    CPC分类号： B64C15/02 ,  F02K1/002 ,  F02K1/006 ,  F02K1/04 ,  F02K1/11 ,  F02K1/15 ,  F02K1/54 ,  F02K1/60 ,  F02K1/70 ,  F02K1/76 ,  F02K1/805 ,  F05D2240/55 ,  Y02T50/672

    摘要： A variable area exhaust nozzle with a variable thrust vector angle for a turbo-fan engine and mounted on the aft portion of the nacelle which wraps said engine. The nozzle may include a fixed structure having at least two lateral arms separating two radial cutouts. The cutouts are positioned one above the other, one being located above the engine axis, the other one below the engine axis. At least two shells close the fixed structure cutouts and are pivotally mounted on the fixed structure to form a portion of the exhaust nozzle of the engine. A sealing means ensures fluid tightness between the shells and the fixed structure for any angular position of said shells. Actuator means are provided for pivoting the shells either to a symmetrical configuration for changing of the value of the exhaust area of the nozzle or to an unsymmetrical configuration for changing the angle of the thrust vector of the exhaust nozzle. In operation, the value of the exhaust area and the thrust vector angle of the exhaust nozzle are varied during flight to optimize performance of the aircraft.

    Thrust reverser assembly
    13.
    发明授权
    Thrust reverser assembly 失效
    推力反向组件

    公开(公告)号：US5082209A

    公开(公告)日：1992-01-21

    申请号：US662645

    申请日：1991-03-01

    申请人： Andrew G. Keyser

    发明人： Andrew G. Keyser

    IPC分类号： F02K1/54 ,  F02K1/78

    CPC分类号： F02K1/78 ,  F02K1/54

    摘要： Ports through the wall of the exhaust duct and the wall of the surrounding cooling air duct, connect the exhaust duct and reverse thrust ducts. Door sets seal these ports. The door sets are contrarotated around the exhaust duct providing a symmetrical opening of the ports.

    摘要翻译： 端口通过排气管道的壁和周围的冷却风道的墙壁，连接排气管道和反向推力管道。 门套密封这些端口。 门排围绕排气管道对置，提供端口的对称开口。

    Antipollution jet engine with reversible auxiliary jet engines operable independently to serve as auxiliary thrusters and brakes
    14.
    发明授权
    Antipollution jet engine with reversible auxiliary jet engines operable independently to serve as auxiliary thrusters and brakes 失效
    具有可逆辅助喷气发动机的防喷射发动机可独立运行，作为辅助油门和制动器

    公开(公告)号：US3733824A

    公开(公告)日：1973-05-22

    申请号：US3733824D

    申请日：1971-07-20

    申请人： GRAINGER L

    发明人： GRAINGER L

    IPC分类号： F02K1/54 ,  F23R3/26 ,  F23R3/32 ,  F23R3/42 ,  F23R3/60 ,  F02K3/08

    CPC分类号： F02K1/54 ,  F05D2250/411 ,  F23R3/26 ,  F23R3/32 ,  F23R3/42 ,  F23R3/60

    摘要： An antipollution jet engine in which air is fed through the chamber walls of the combustion chamber downstream of the fuel oil nozzle. The air is caused to have a tangential swirling motion to assist in obtaining a complete burning mixture so as to burn all combustible material in the fuel to eliminate pollution. Additional fuel is supplied to a downstream burner similarly provided with downstream air admission ports to create a circular tangential turbulence for a complete mixing and complete burning of the combustible materials. The function of the downstream burner is to assist in completely burning all of the combustible materials resulting from the first burners. The fuel for the first burners and the downstream burner is preheated to improve ignition and burning.