公开(公告)号：US6009702A

公开(公告)日：2000-01-04

申请号：US856175

申请日：1997-05-14

申请人： Patrick Gonidec ,  Gerard Pascal Rouyer ,  Bernard Guy Vauchel

发明人： Patrick Gonidec ,  Gerard Pascal Rouyer ,  Bernard Guy Vauchel

IPC分类号： B64D29/00 ,  B64D33/00 ,  F02K1/70 ,  F02R3/02

CPC分类号： F02K1/70 ,  Y02T50/671

摘要： A thrust reverser is disclosed for a turbojet engine having a cowling forming an outer boundary of a gas flow duct through which gases flow from a front to a rear, the cowling having at least one reverse thrust opening communicating with the gas flow duct and a thrust reverser door pivotally connected to the cowling so as to move between a forward thrust position wherein the thrust reverser door covers the reverse thrust opening, and a reverse thrust position wherein the reverse thrust opening is uncovered and the thrust reverser door directs at least a portion of the gases flowing through the duct through the reverse thrust opening. The thrust reverser also includes at least one panel having an inner surface, a first lateral side pivotally connected to the cowling so as to pivot about a panel pivot axis extending generally parallel to the gas flow direction through the duct and an actuating mechanism connected to a second lateral side of the panel so as to move the panel about the panel pivot axis between a first position in which the inner surface forms a portion of the outer boundary of the gas flow duct and a second position wherein the second lateral side is disposed within the gas flow duct. The actuating mechanism may include a mechanical linkage interconnecting the second lateral side of the panel to the thrust reverser door such that movement of the thrust reverser door between the forward and reverse thrust positions causes movement of the panel between the first and second positions.

摘要翻译： 公开了一种用于涡轮喷气发动机的推力反向器，其具有形成气体流动管道的外边界的整流罩，气体从前部流向后部，整流罩具有与气体流动管道连通的至少一个反向推力开口和推力 可逆转门可枢转地连接到整流罩，以便在推力反向器门覆盖反向推力开口的向前推力位置和反推力位置之间移动，其中反推力开口未被覆盖，并且推力反向器门引导至少一部分 气体通过反向推力开口流过管道。 推力反向器还包括至少一个具有内表面的面板，第一横向侧面枢转地连接到整流罩，以便围绕大致平行于气体流动方向延伸通过管道的面板枢转轴线枢转，以及致动机构，其连接到 以使面板围绕面板枢转轴线移动在第一位置和第二位置之间，在第一位置，第一位置和第二位置之间，其中内表面形成气体流动管道的外边界的一部分，其中第二侧面设置在第二位置内 气流管道。 致动机构可以包括将面板的第二侧面与推力反向器门互连的机械连杆，使得推力反向器门在正向和反向推力位置之间的运动导致面板在第一和第二位置之间的移动。

公开(公告)号：US5974783A

公开(公告)日：1999-11-02

申请号：US997241

申请日：1997-12-23

申请人： Patrick Gonidec ,  Guy Bernard Vauchel

发明人： Patrick Gonidec ,  Guy Bernard Vauchel

IPC分类号： B64D33/00 ,  F02K1/70 ,  F02K1/54 ,  F02K3/02

CPC分类号： F02K1/70

摘要： A thrust reverser is disclosed for a turbofan type turbojet engine assembly with a cowling having an inner cowling surface forming an outer boundary of a gas flow duct, and an outer cowling surface spaced from the inner cowling surface, the inner and outer cowling surfaces joining at a rearmost edge of the cowling, the thrust reverser having a thrust reverser baffle with an outer baffle surface and an inner baffle surface, a forward linkrod pivotally connected to a forward portion of a thrust reverser baffle and to the cowling, and a rear linkrod pivotally connected to the thrust reverser baffle and to the cowling. The thrust reverser baffle is movable between a forward thrust position wherein the outer baffle surface is substantially flush with the outer cowling surface, a forward portion of the thrust reverser baffle covering an inner rear cowling portion having the inner cowling surface, and a reverse thrust position in which the reverse thrust baffle is disposed rearwardly of the rearmost cowling edge so as to redirect gases flowing through the gas flow duct. When in the forward thrust position, the forward and rear linkrods are totally enclosed between the spaced apart inner and outer cowling surfaces.

摘要翻译： 公开了一种用于涡轮风扇式涡轮喷气发动机组件的推力反向器，其具有形成气体流动管道的外边界的内整流罩表面的整流罩，以及与内整流罩表面间隔开的外整流罩表面，内和外整流罩表面 整流罩的最后边缘，推力反向器具有带有外挡板表面和内挡板表面的推力反向挡板，可枢转地连接到推力反向器挡板和整流罩的前部的前连杆，以及枢轴 连接到推力反向挡板和整流罩。 推力反向器挡板可以在前推力位置之间移动，其中外挡板表面与外整流罩表面基本齐平，推力反向器挡板的前部覆盖具有内整流罩表面的内后整流罩部分和反向推力位置 其中反向推力挡板设置在最后面的整流罩边缘的后方，以便改变流过气体流动管道的气体。 当在向前推力位置时，前后连杆被完全封闭在间隔开的内和外罩表面之间。

公开(公告)号：US5947625A

公开(公告)日：1999-09-07

申请号：US997506

申请日：1997-12-23

申请人： Guy Bernard Vauchel

发明人： Guy Bernard Vauchel

IPC分类号： B64D33/00 ,  F02K1/12 ,  F02K1/70 ,  F02K1/74 ,  F16C11/06 ,  F16C11/10 ,  B64C15/06

CPC分类号： F16C11/0614 ,  F02K1/70 ,  F16C11/02 ,  Y10T403/18 ,  Y10T403/32204 ,  Y10T403/32681

摘要： A pivot system is disclosed for pivotally connecting a movable component to a fixed component, the pivot system having a swivel device mounted on one of the movable and fixed components, a headed shaft passing through a portion of the other of the movable and fixed components and engaging the swivel device, the headed shaft having a longitudinal axis forming the pivot axis between the components, an anti-rotation device engaging the shaft so as to prevent relative rotation between the shaft and the component to which it is mounted, and an anti-axial movement device engaging the shaft as to prevent relative movement between the shaft and the component to which it is mounted along the longitudinal axis of the shaft. This structure enables the shaft to be installed having access to only one end of the pivot shaft, improving over the known systems in which it is necessary to have access to both ends of the pivot shaft.

摘要翻译： 公开了一种用于将可移动部件枢转地连接到固定部件的枢转系统，该枢转系统具有安装在可移动和固定部件中的一个上的旋转装置，穿过可移动和固定部件中的另一个的一部分的头部轴， 与所述旋转装置接合，所述头部轴具有形成所述部件之间的枢转轴线的纵向轴线，与所述轴接合的防旋转装置，以防止所述轴与所述轴与所述部件之间的相对旋转， 轴向运动装置接合轴，以防止轴和沿其轴的纵向轴线安装到其上的部件之间的相对运动。 这种结构使得轴可以安装成只能接近枢转轴的一端，从而可以改进已知的需要进入枢轴的两端的系统。

公开(公告)号：US5799903A

公开(公告)日：1998-09-01

申请号：US709155

申请日：1996-09-06

申请人： Guy Bernard Vauchel

发明人： Guy Bernard Vauchel

IPC分类号： F02K1/68 ,  F02K1/70 ,  B64D33/04

CPC分类号： F02K1/68 ,  F02K1/70 ,  Y02T50/671

摘要： A thrust reverser is disclosed for a turbojet engine having an outer cowling and an inner cowling forming a generally annular gas flow duct therebetween, the thrust reverser having at least one thrust reverser door pivotally attached to the outer cowling so as to pivot about a first stationary axis to move between a forward thrust position and a reverse thrust position, a thrust reverser panel pivotally attached to the inner cowling so as to pivot about a second stationary axis to move between a forward thrust position and a reverse thrust position, and a connector connecting the thrust reverser door and the thrust reverser panel such that when the thrust reverser door is in the reverse thrust position, the thrust reverser panel is in the reverse thrust position and when the thrust reverser door is in the forward thrust position, the thrust reverser panel is also in the forward thrust position.

摘要翻译： 公开了一种用于涡轮喷气发动机的推力反向器，其具有外罩和在其间形成大致环形的气体流动管道的内罩，所述推力反向器具有至少一个推力反向器门，该推力反向器门可枢转地附接到外罩，以便围绕第一静止 轴线在前向推力位置和反向推力位置之间移动;推力反向器板，其枢转地附接到所述内部整流罩，以便围绕第二固定轴线枢转以在向前推力位置和反向推力位置之间移动;连接器连接 推力反向器门和推力反向器面板，使得当推力反向器门处于反向推力位置时，推力反向器面板处于反向推力位置，并且当推力反向器门处于向前推力位置时，推力反向器面板 也处于向前的推力位置。

公开(公告)号：US5716025A

公开(公告)日：1998-02-10

申请号：US572612

申请日：1995-12-14

申请人： Pascal J. Meyer

发明人： Pascal J. Meyer

IPC分类号： F02K1/56 ,  F02K1/70 ,  B64C33/04 ,  F02K1/64

CPC分类号： F02K1/56 ,  F02K1/70 ,  F05D2250/191 ,  Y02T50/672

摘要： The reverser includes a partition (28) exhibiting openings (19) and separating the cavity (16) which exists, when the doors (2) are in the closed position, between the front part (7) of the internal panel (11) of the door and the stream of gaseous flow (15) flowing in direct jet mode through the jet pipe CA, thus overcoming the aerodynamic losses which result from the presence of this cavity.

摘要翻译： 反向器包括一个分隔件（28），该分隔件（28）具有开口（19）并且当门（2）处于关闭位置时）在内板（11）的前部（7）之间分开存在的空腔（16） 门和气流（15）以直接喷射模式流过喷射管CA，从而克服了由于该空腔的存在而导致的空气动力学损失。

公开(公告)号：US5396762A

公开(公告)日：1995-03-14

申请号：US160424

申请日：1993-12-01

申请人： Robert R. Standish

发明人： Robert R. Standish

IPC分类号： F02K1/56 ,  F02K1/70 ,  F02K3/02

CPC分类号： F02K1/563 ,  F02K1/70

摘要： The invention relates to thrust reversers with doors for a jet engine. The upstream edge of the reverser doors is equipped with a deflecting structure consisting of a rigid frame (10, 12, 13) fixed to the door and delimiting a space (14) capped by a stiffener (15). In the space (14) are housed vanes (16) with aerodynamic profile in the form of a wing which is inclined by an angle a with respect to the plane of the frame (10, 12, 13) in order to orient laterally the flow of the gases which is diverted by the reverser. This arrangement makes it possible to reduce, or even to prevent, re-ingestion by the engine of the diverted gases, or interference of the latter with the wing structure of the aircraft.

摘要翻译： 本发明涉及具有用于喷气发动机的门的推力反向器。 反向门的上游边缘装有一个偏转结构，该偏转结构由固定在门上的刚性框架（10,12,13）组成，并限定一个由加强筋（15）盖住的空间（14）。 在空间（14）中，具有空气动力学轮廓的容纳叶片（16），其翼型形式相对于框架（10,12,13）的平面倾斜一个角度α，以便侧向地定向流动 的反向器转向的气体。 这种布置使得可以减少或甚至防止发动机重新摄入转向气体，或者使其与飞行器的机翼结构的干扰。

公开(公告)号：US5347808A

公开(公告)日：1994-09-20

申请号：US901668

申请日：1992-06-22

申请人： Robert Standish ,  Joel Frank ,  Pascal Meyer

发明人： Robert Standish ,  Joel Frank ,  Pascal Meyer

IPC分类号： F02K1/70 ,  F02K3/02

CPC分类号： F02K1/70

摘要： An improvement made to jet-engine thrust reversers and, more particularly, to reversers called tilting-door reversers. The doors are equipped, on their upstream portion, with a flow-deflecting overlay 90 which, in the open-door position, is in a position close to a line PM parallel to the axis of the engine 1, the overlay making with the inner door skin an angle B greater than 90.degree., preferably between 105.degree. and 110.degree.. The invention is more particularly applicable to dual-flow engines.

摘要翻译： 对喷气发动机推力反向器的改进，更具体地，涉及称为倾斜门反向器的反向器。 门在其上游部分配备有流动偏转覆盖层90，其在开门位置处于接近平行于发动机1的轴线的线路PM的位置，与内部 门皮B角大于90°，​​最好在105°和110°之间。 本发明更特别适用于双流引擎。

公开(公告)号：US5197693A

公开(公告)日：1993-03-30

申请号：US745533

申请日：1991-08-15

申请人： Jihad I. Remlaoui

发明人： Jihad I. Remlaoui

IPC分类号： F02K1/70

CPC分类号： F02K1/70 ,  Y02T50/671

摘要： A thrust reverser system for fan jet type aircraft gas turbine engines using a "sliding hinge" arrangement for moving blocker doors between the stowed and deployed positions. Blocker doors fill a plurality of radially arranged openings in an engine nacelle near the aft end of the nacelle. In the stowed position, each blocker door forms and inner and outer streamlined surface corresponding to the nacelle walls, with no actuator mechanisms extending into the air flow stream within the nacelle. Each blocker door is moved to the deployed position by an extensible rod, such as a hydraulic piston rod, extending between the nacelle near the forward edge of the opening and the approximate centerline of the door. As the door begins to move rearwardly, slider pins on the door edges slide along tracks on the adjacent nacelle islands between adjacent openings. Meanwhile, a hinged bar secured at its aft end to the adjacent nacelle island and at its forward end to the door edge rotates, pivoting the aft end of the door inwardly into contact with the engine core while the door forward end pivots outwardly of the opening. The doors substantially block airflow through the duct between nacelle and core and direct it in an outward, reverse or forward, direction.

摘要翻译： 用于风扇喷气式飞机燃气涡轮发动机的推力反向器系统，其使用“滑动铰链”布置，用于在收起位置和展开位置之间移动阻挡门。 阻挡门在机舱后端附近的发动机舱中填充多个径向布置的开口。 在收起位置，每个阻挡门形成并且对应于机舱壁的内部和外部流线型表面，没有致动器机构延伸到机舱内的空气流动流中。 每个阻挡门通过可伸缩的杆（例如液压活塞杆）移动到展开位置，液压活塞杆在开口的前边缘附近的机舱和门的大致中心线之间延伸。 当门开始向后移动时，门边缘上的滑块销沿相邻开口之间的相邻机舱岛上的轨道滑动。 同时，在其后端固定到相邻的机舱岛并且在其前端到门边缘的铰接杆旋转，从而将门的后端向内旋转以与发动机芯接触，同时门前端向开口的外侧枢转 。 门基本上阻挡了通过机舱和铁芯之间的管道的气流并将其引导向外，反向或向前的方向。

公开(公告)号：US5097662A

公开(公告)日：1992-03-24

申请号：US439848

申请日：1989-11-20

申请人： Gary L. Vieth

发明人： Gary L. Vieth

IPC分类号： F02K1/70

CPC分类号： F02K1/70

摘要： An apparatus for influencing a flow of air through a passageway defined between an inner wall and a double outer wall that includes first and second walls each formed with an opening, comprises a first door, a second door, vortex generation means positioned between the first and second walls and adjacent the upstream end of the opening in the first wall, and an actuator pivotally attached to the first and second doors. The actuator has a first condition wherein the first and second doors close the openings in the first and second walls respectively and has a second condition wherein the first door is at the downstream end of the opening in the first wall and extends across the passageway and directs the flow of air through the opening in the first wall, and the second door is at the down-stream end of the opening in the second wall and deflects the flow of air through that opening.

摘要翻译： 一种用于影响通过限定在内壁和双外壁之间的通道的空气流的装置，该通道包括每个形成有开口的第一和第二壁，第一门，第二门，位于第一和第二外壁之间的涡流产生装置 第二壁并且邻近第一壁中的开口的上游端，以及可枢转地附接到第一和第二门的致动器。 致动器具有第一状态，其中第一和第二门分别关闭第一和第二壁中的开口，并且具有第二状态，其中第一门处于第一壁的开口的下游端并且延伸穿过通道并引导 空气通过第一壁中的开口的流动，第二门处于第二壁的开口的下游端，并使空气流通过该开口。

公开(公告)号：US4894985A

公开(公告)日：1990-01-23

申请号：US223021

申请日：1988-07-22

申请人： Claude A. G. Dubois ,  Xavier R. Y. Lore

发明人： Claude A. G. Dubois ,  Xavier R. Y. Lore

IPC分类号： F02K1/70

CPC分类号： F02K1/70

摘要： The present invention relates to a thrust reverser system for a turbofan-type turbojet engine having thrust reverser doors with movable deflectors. The deflectors are movably attached to an upstream edge of the thrust reversing doors and are movable between retracted and extended positions. When the thrust reversing door is closed and the turbojet engine operates in its normal thrust mode, the deflectors are retracted thereby enabling the difference between the inner surface of the thrust reversing door and the theoretical aerodynamic flow line to be reduced or eliminated. When the thrust reversing door is in the thrust reversing position, the deflector is extended so as to protrude beyond the inner surface of the door so as to direct the air flow in a more forward direction to increase the thrust reversing capabilities of the system. The deflectors are mounted on the thrust reversing door such that they are automatically extended when the thrust reversing door moves to the thrust reversing position.

摘要翻译： 本发明涉及一种具有带可移动导流器的推力反向器门的涡轮风扇式涡轮喷气发动机的推力反向器系统。 偏转器可移动地附接到推力反向门的上游边缘并且可在缩回位置和伸出位置之间移动。 当推力反向门关闭并且涡轮喷气发动机以其正常推力模式运行时，导流器被缩回，从而能够减小或消除推力反向门的内表面与理论空气动力学流线之间的差异。 当推力反转门处于推力反转位置时，偏转器被延伸以便突出超过门的内表面，以便将空气流引向更向前的方向以增加系统的推力反转能力。 偏转器安装在推力反向门上，使得当推力反向门移动到推力反向位置时，它们被自动延伸。