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公开(公告)号：US6148607A
公开(公告)日：2000-11-21
申请号：US113323
申请日：1998-07-10
摘要： A thrust reverser for aircraft gas-turbine engines includes latch devices that display a tell-tale visible indication when thrust reverser shutters (doors, etc.) are ajar. A latch of the lock at least partly projects from a wall (13, 14) radially bounding the annular structure (12) of the thrust reverser (10) when the latch (37) is in the open mode.
摘要翻译： 用于飞机燃气涡轮发动机的推力反向器包括闩锁装置，当推力反向开关（门等）为止时，该装置显示出可见的指示。 当闩锁（37）处于打开模式时，锁的闩锁至少部分地从径向地包围推力反向器（10）的环形结构（12）的壁（13,14）突出。
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公开(公告)号：US5967460A
公开(公告)日：1999-10-19
申请号：US942912
申请日：1997-10-02
CPC分类号： F02K1/70 , Y02T50/671
摘要： An actuating mechanism is disclosed for a thrust reverser of a turbojet engine having an engine cowling with a reverse thrust opening, a thrust reverser door pivotally connected to the engine cowling so as to pivot between forward and reverse thrust positions, and a linear actuator having a casing with an extendable and retractable piston rod. The piston rod is connected to the thrust reverser by a first connection forming a first connection point. An interface bracket is fixedly attached to the turbojet engine structure and engages a mounting flange in a connector affixed to the actuator casing at a second connection point, the mounting flange being in contact with the interface bracket at a third connection point, the first, second and third connection points lying in a straight line.
摘要翻译： 公开了一种用于涡轮喷气发动机的推力反向器的致动机构，其具有具有反向推力开口的发动机整流罩，可枢转地连接到发动机整流罩以便在正向和反向推力位置之间枢转的推力反向器门以及具有 外壳具有可伸缩的活塞杆。 活塞杆通过形成第一连接点的第一连接件连接到推力反向器。 接口支架固定地连接到涡轮喷气发动机结构，并且在第二连接点处与固定到致动器壳体的连接器中的安装凸缘接合，安装凸缘在第三连接点与接口支架接触，第一，第二 并且第三连接点位于直线上。
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公开(公告)号：US6145786A
公开(公告)日：2000-11-14
申请号：US53776
申请日：1998-04-02
摘要： A latching mechanism is disclosed for a jet engine thrust reverser having a thrust reverser door movably connected to an engine cowling with a reverse thrust opening, the thrust reverser door being movable between a forward thrust position, in which the thrust reverser door covers the reverse thrust opening, and a reverse thrust position, in which the reverse thrust opening is uncovered. The latching mechanism has a lock bar mounted on the thrust reverser door, the lock bar having a distal end, and a latch member pivotally located on the cowling, the latch member having a slot engaged by the distal end of the lock bar when the thrust reverser door is in the forward thrust position. The latch member is movable between a latched position, in which the latch member prevents disengagement of the distal end of the lock bar from the slot, so as to lock the thrust reverser door in the forward thrust position, and an unlatched position which permits disengagement of the distal end of the lock bar from the slot. The latching mechanism also includes a hook member connected to the cowling and located so as to engage the distal end of the lock bar upon relative movement between the cowling and the thrust reverser door away from each other in a direction generally parallel to a longitudinal axis of the cowling, such engagement preventing disengagement of the distal end of the lock bar from the slot and displacement of the thrust reverser door from the forward thrust position.
摘要翻译： 公开了一种用于喷气发动机推力反向器的闩锁机构，其具有可逆转地连接到具有反推力开口的发动机整流罩的推力反向器门，推力反向器门可在向前推力位置之间移动，推力反向器门覆盖反向推力 开启和反推力位置，其中反推力开口未被覆盖。 闩锁机构具有安装在推力反向器门上的锁杆，锁定杆具有远端，并且枢转地位于整流罩上的闩锁构件，闩锁构件具有与锁定杆的远端接合的槽，当推力 反向门处于向前推力位置。 闩锁构件可以在闩锁位置之间移动，在该闩锁位置中，闩锁构件防止锁定杆的远端从槽中脱离，以便将推力反向器门锁定在向前推力位置，并且允许脱开的解锁位置 的锁定杆的远端与狭槽。 闩锁机构还包括连接到整流罩的钩构件，并且定位成在整流罩和推力反向器门之间相对运动时在大致平行于纵向轴线的方向上彼此远离的方向上与锁定杆的远端接合 整流罩，这种接合防止锁定杆的远端脱离槽并且推力反向器门从向前的推力位置移位。
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4.发明授权Linear telescopic actuator for moving a first and a second element relative to a stationary element 有权用于相对于静止元件移动第一和第二元件的线性伸缩致动器公开(公告)号：US08943794B2
公开(公告)日：2015-02-03
申请号：US12681219
申请日：2008-07-04
CPC分类号： F16H25/20 , F02K1/08 , F02K1/72 , F02K1/763 , F05D2220/36 , F05D2250/41 , F16H25/2056 , F16H25/2204 , Y02T50/671 , Y10T74/18568 , Y10T74/18672
摘要： The invention relates to a linear telescopic actuator for moving a first (10b) and a second (10a) element relative to a stationary element (102). Said actuator comprises a base (101) that is to be connected to the stationary element (102) and is used as a cavity for a first rotationally locked rod (106) which can be translated by a drive shaft (104) that is to be connected to rotational driving means (107). One end (108) of said first rod is to be connected to the first element that is to be moved. The actuator is characterized in that the first rod (106) supports a second rod (117) which is aligned therewith and one end (118) of which is to be connected to the second element that is to be moved. Said second rod (117) can be rotationally locked and can be translated by a second drive shaft (112, 115) which extends through the base and is connected to rotational driving means (113, 111).
摘要翻译： 本发明涉及一种用于相对于固定元件（102）移动第一（10b）和第二（10a）元件的线性伸缩致动器。 所述致动器包括要连接到固定元件（102）的基座（101），并且用作用于第一旋转锁定杆（106）的空腔，所述第一旋转锁定杆（106）能够被驱动轴（104）平移 连接到旋转驱动装置（107）。 所述第一杆的一端（108）将连接到待移动的第一元件。 致动器的特征在于，第一杆（106）支撑与其对准的第二杆（117），并且其一端（118）将被连接到待移动的第二元件。 所述第二杆（117）可被旋转地锁定并且可以通过延伸穿过基座并连接到旋转驱动装置（113,111）的第二驱动轴（112,115）平移。
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5.发明授权公开(公告)号：US08931253B2
公开(公告)日：2015-01-13
申请号：US12681416
申请日：2008-08-20
CPC分类号： F02K1/763 , F02K1/72 , H02K7/06 , Y10T74/18568 , Y10T74/18672
摘要： A thrust reverser for a turbojet engine includes a telescopic linear actuator for a moving cowl and a nozzle-forming end part. The telescopic linear actuator has a base attached to a fixed frame, acting as a housing for a first rod prevented from rotating but able to be translationally driven by a first drive shaft connected to a rotational-driver. The first rod is attached by one end to the moving cowl and supports a second rod, which is attached by one end to the nozzle-forming end part that is to be moved. The second rod is prevented from rotating and translationally driven by a second drive shaft passing through the base and connected to a rotational-driver. In particular, the rotational-driver of the rods includes a motor to drive an input shaft of a differential having two output shafts.
摘要翻译： 用于涡轮喷气发动机的推力反向器包括用于移动整流罩的伸缩线性致动器和喷嘴形成端部。 伸缩线性致动器具有附接到固定框架的基座，用作第一杆的壳体，其防止旋转，但是能够由连接到旋转驱动器的第一驱动轴平移地驱动。 第一杆通过一端连接到移动整流罩，并支撑第二杆，第二杆通过一端连接到待移动的喷嘴形成端部。 第二杆被防止由穿过基座的第二驱动轴旋转和平移地驱动，并连接到旋转驱动器。 特别地，杆的旋转驱动器包括用于驱动具有两个输出轴的差速器的输入轴的马达。
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公开(公告)号：US20080168762A1
公开(公告)日：2008-07-17
申请号：US11882669
申请日：2007-08-03
申请人： Michel Philippe Dehu , Fabrice Henri Emile Metezeau , Pierre Andre Marcel Baudu , Vincent Pierre Germain Le-Coq
发明人： Michel Philippe Dehu , Fabrice Henri Emile Metezeau , Pierre Andre Marcel Baudu , Vincent Pierre Germain Le-Coq
IPC分类号： F02K1/54
CPC分类号： F02K1/566 , F02K1/763 , Y10T74/20067
摘要： A method for opening a mobile cowl actuated by a motor and equipping a turbojet thrust reverser that includes at the start of the opening phase, a bridling step whereby the speed of the mobile cowl is maintained lower or equal to a predetermined threshold speed.
摘要翻译： 一种用于打开由电动机驱动的移动整流罩并装备涡轮喷气推力反向器的方法，该涡轮喷气推进反向器包括在开启阶段开始时的桥接步骤，由此将移动整流罩的速度维持在预定阈值速度以下。
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公开(公告)号：US08677732B2
公开(公告)日：2014-03-25
申请号：US12446704
申请日：2007-09-26
IPC分类号： F02K3/02
CPC分类号： F02K1/72 , F02K1/763 , F05D2260/50 , Y02T50/671 , Y10T74/18808
摘要： The invention relates to a thrust reverser (1) comprising an opening with fixed grids (4) that is closed by a sliding lid (2) in case of direct thrust, and opened by the downstream longitudinal translation displacement of the lid (2) in case of thrust reversal. A flap (20) is pivotally mounted at one upstream end on the lid (2) and can move between a retracted position and an expanded position in which, in case of thrust reversal, it blocks an annular channel (10) in order to redirect a gas flow towards the grid opening (4). A slider (24) for driving the flap (20) is mounted so as to be capable of displacement in at least one translation guiding rail (33) provided in the structure of the lid (2), and is connected to a downstream end of the flap (20) through a driving connecting rod (30) so that a translation movement of the slider (24) in the guiding rail (33) results in a pivoting of the connecting rod (30) and of the flap (20). Actuation means (22) are provided for driving the slider (24) in a translation movement in the guiding rail (33) when the lid (2) is in a downstream translation phase.
摘要翻译： 本发明涉及一种推力反向器（1），其包括具有固定格栅（4）的开口，该开口在直接推力的情况下由滑动盖（2）封闭，并且由盖（2）的下游纵向平移位移开启 推力反转的情况。 翼片（20）枢转地安装在盖（2）上的一个上游端，并且可以在缩回位置和展开位置之间移动，在缩回位置和扩展位置中，在推力反转的情况下，挡板（20）阻挡环形通道（10）以便重定向 朝向格栅开口（4）的气流。 用于驱动翼片（20）的滑块（24）安装成能够在设置在盖（2）的结构中的至少一个平移导轨（33）中移位，并且连接到 所述翼片（20）穿过驱动连杆（30），使得所述滑块（24）在所述导轨（33）中的平移运动导致所述连杆（30）和所述翼片（20）的枢转。 驱动装置（22）用于当盖（2）处于下游平移阶段时，在导轨（33）中的平移运动中驱动滑块（24）。
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公开(公告)号：US20110085897A1
公开(公告)日：2011-04-14
申请号：US12995344
申请日：2009-03-30
IPC分类号： F04D29/42
CPC分类号： F02C7/04 , F01D21/045 , F01D25/24 , F01D25/28 , F05D2300/603 , Y02T50/672
摘要： The present invention relates to a casing (5) for a rotor of a turbomachine, more particularly for a fan (1) of a turbojet engine (2), comprising a peripheral shroud (6) designed to form a clamping collar around the casing, characterized in that the shroud has at least one fitting (12, 13) or flange for the attachment of equipment.
摘要翻译： 本发明涉及一种用于涡轮机的转子的壳体（5），更具体地说，涉及一种涡轮喷气发动机（2）的风扇（1），其包括设计成围绕壳体形成夹紧轴环的外围罩（6） 其特征在于，所述护罩具有用于附接设备的至少一个配件（12,13）或凸缘。
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公开(公告)号：US20100139242A1
公开(公告)日：2010-06-10
申请号：US12446704
申请日：2007-09-26
CPC分类号： F02K1/72 , F02K1/763 , F05D2260/50 , Y02T50/671 , Y10T74/18808
摘要： The invention relates to a thrust reverser (1) comprising an opening with fixed grids (4) that is closed by a sliding lid (2) in case of direct thrust, and opened by the downstream longitudinal translation displacement of the lid (2) in case of thrust reversal. A flap (20) is pivotally mounted at one upstream end on the lid (2) and can move between a retracted position and an expanded position in which, in case of thrust reversal, it blocks an annular channel (10) in order to redirect a gas flow towards the grid opening (4). A slider (24) for driving the flap (20) is mounted so as to be capable of displacement in at least one translation guiding rail (33) provided in the structure of the lid (2), and is connected to a downstream end of the flap (20) through a driving connecting rod (30) so that a translation movement of the slider (24) in the guiding rail (33) results in a pivoting of the connecting rod (30) and of the flap (20). Actuation means (22) are provided for driving the slider (24) in a translation movement in the guiding rail (33) when the lid (2) is in a downstream translation phase.
摘要翻译： 本发明涉及一种推力反向器（1），其包括具有固定格栅（4）的开口，该开口在直接推力的情况下由滑动盖（2）封闭，并且由盖（2）的下游纵向平移位移开启 推力反转的情况。 翼片（20）枢转地安装在盖（2）上的一个上游端，并且可以在缩回位置和展开位置之间移动，在缩回位置和扩展位置中，在推力反转的情况下，挡板（20）阻挡环形通道（10）以便重定向 朝向格栅开口（4）的气流。 用于驱动翼片（20）的滑块（24）安装成能够在设置在盖（2）的结构中的至少一个平移导轨（33）中移位，并且连接到 所述翼片（20）穿过驱动连杆（30），使得所述滑块（24）在所述导轨（33）中的平移运动导致所述连杆（30）和所述翼片（20）的枢转。 驱动装置（22）用于当盖（2）处于下游平移阶段时，在导轨（33）中的平移运动中驱动滑块（24）。
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公开(公告)号：US5997054A
公开(公告)日：1999-12-07
申请号：US053501
申请日：1998-04-02
CPC分类号： F02K1/766 , F02K1/76 , Y10T292/1082 , Y10T292/699 , Y10T292/702
摘要： A device for closing and locking the shutters of an aircraft thrust reverser includes a lock having a latch which is motorized so as to complete the closure of a shutter utilizing energy supplied by the motor, thereby relieving the jack which is the prime mover of the shutter. The device includes a stop which opposes the latch and interacts with a counter-stop so as to immobilize the shutter in the closed position and thus reduce vibration and flapping of the shutter.
摘要翻译： 用于关闭和锁定飞机推力反向器的快门的装置包括具有闩锁的锁，其被电动化，以便利用由马达提供的能量完成快门的关闭，从而减轻作为快门的原动机的插孔 。 该装置包括与闩锁相对的止动件并且与止回装置相互作用，以便将活门固定在关闭位置，从而减少活门的振动和振动。
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