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1. 发明申请

WO1997043536A1 THRUST REVERSER FOR A TURBO-JET ENGINE WITH DOORS ASSOCIATED TO AN UPSTREAM PANEL 审中-公开
标题翻译：用于具有与上游面板相关的门的涡轮喷气发动机的扭矩反转器
公开(公告)号：WO1997043536A1
公开(公告)日：1997-11-20
申请号：PCT/FR1997000862
申请日：1997-05-15
申请人： SOCIETE HISPANO SUIZA
发明人： SOCIETE HISPANO SUIZA , GONIDEC, Patrick , ROUYER, Pascal, Gérard , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/70 , F05D2250/34 , Y02T50/671
摘要： A thrust reverser for a twin flow turbo-jet engine comprises pivoting doors (7) integrated in the direct jet pod wall in and forming obstacles for deviating the flow in the reverse jet mode. Each upstream portion of the door (7) is internally lined with an upstream panel (22) providing for a smoothing of the direct jet air flow. The upstream panel (22) is supported and connected by at least one rod (30, 34, 35) to the fixed structure (1) of the reverser and to the door (7).
摘要翻译：用于双流涡轮喷气发动机的推力反向器包括集成在直接喷射舱壁中的枢转门（7），并且形成用于以反向喷射模式偏移流动的障碍物。门（7）的每个上游部分内部具有提供直接喷射空气流平滑化的上游面板（22）。上游面板（22）由至少一个杆（30,34,35）支撑并连接到反向器的固定结构（1）和门（7）。

2. 发明申请

WO1997043535A1 TURBOFAN THRUST REVERSER WITH DOORS EQUIPPED WITH DEFLECTING BLADES 审中-公开
标题翻译： TURBOFAN用带有偏转刀片的门进行反转
公开(公告)号：WO1997043535A1
公开(公告)日：1997-11-20
申请号：PCT/FR1997000817
申请日：1997-05-07
申请人： SOCIETE HISPANO SUIZA
发明人： SOCIETE HISPANO SUIZA , GONIDEC, Patrick , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/70 , Y02T50/671
摘要： The invention features a turbofan thrust reverser comprising pivoting doors (7) integrated in direct jet flow in the external pod wall and constituting thrust reversing flow deviation obstacles after pivoting by an actuator (8). Each door (7) bears at least one deflecting blade (22) aerodynamically profiled in wing shape, set in contact with the flow in the ring-shaped channel (21) such that the flow exerts an action on the said blade (22) which tends to maintain the door (7) in its closed direct jet position.
摘要翻译：本发明的特征在于涡轮风扇推力反向器，包括枢转门（7），其集成在外部舱壁中的直接喷射流中，并在由致动器（8）枢转之后构成推力反向流动偏离障碍物。每个门（7）承载至少一个在机翼形状上空气动力学分布的偏转叶片（22），其设置成与环形通道（21）中的流体接触，使得流动对所述叶片（22）施加作用，倾向于将门（7）保持在其闭合的直接喷射位置。

3. 发明申请

WO1997002419A1 SINGLE-CLAMSHELL TURBOJET THRUST REVERSER 审中-公开
标题翻译：单声道旋转扭矩反转器
公开(公告)号：WO1997002419A1
公开(公告)日：1997-01-23
申请号：PCT/FR1996001039
申请日：1996-07-04
申请人： SOCIETE HISPANO-SUIZA
发明人： SOCIETE HISPANO-SUIZA , METEZEAU, Fabrice, Henri, Emile , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/56
CPC分类号： F02K1/563 , Y02T50/671
摘要： A turbojet thrust reverser comprising a fixed upstream structure (10) with a downstream end having a tapered edge (14) that does not lie in a plane perpendicular to the reverser axis (15), and a movable portion consisting of a single clamshell (16) which, when in the closed position, forms the downstream portion of the direct-flow exhaust nozzle, and may be pivoted about two side pivots (22) on the fixed structure (10) by a control system comprising at least one actuator (23) mounted between a pivot secured to the fixed structure and a pivot secured to the clamshell, so that, in the deployed position, said clamshell forms a bucket for deflecting the gas flow (13a) to reverse the thrust.
摘要翻译：一种涡轮喷气推进反向器，包括固定的上游结构（10），其下游端具有不位于垂直于反向轴线（15）的平面中的锥形边缘（14），以及可移动部分，由单个蛤壳），当处于关闭位置时，其形成直流排气喷嘴的下游部分，并且可以通过包括至少一个致动器（23）的控制系统围绕固定结构（10）上的两个侧枢轴（22）枢转），其安装在固定到固定结构的枢轴和固定到蛤壳之间的枢轴之间，使得在展开位置，所述蛤壳形成用于使气流（13a）偏转以逆转推力的铲斗。

4. 发明申请

WO1997009526A1 TURBOJET THRUST REVERSER HAVING DOORS COMBINED WITH AN UPSTREAM SCOOP PANEL 审中-公开
标题翻译：具有与上海地板组合的门的TURBOJET THRUST REVERSER
公开(公告)号：WO1997009526A1
公开(公告)日：1997-03-13
申请号：PCT/FR1996001359
申请日：1996-09-05
申请人： SOCIETE HISPANO-SUIZA
发明人： SOCIETE HISPANO-SUIZA , GONIDEC, Patrick , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/68 , F02K1/70
摘要： A dual flow turbojet thrust reverser has pivoting doors (7) forming deflection members when operating in thrust reversing mode. Each door (7) is lined on its inner surface, in a closed position thereof, with an upstream panel (22) smoothing the fluid stream in direct jet mode. The upstream panel (22) which is not connected to the door (7) can rotate, when in thrust reversing mode, in a direction opposite to that of the door (7) so that its upstream edge is radially closer to the duct axis than its downstream edge, thus forming a scoop that picks up an inner portion of the stream to control the reverse flow layers and to provide for efficient thrust reversal.
摘要翻译：双流涡轮喷气推进反向器具有枢转门（7），其在推力反向模式下操作时形成偏转构件。每个门（7）在其内表面上处于其关闭位置，上游面板（22）以直接喷射模式平滑流体流。未连接到门（7）的上游面板（22）可以在推力反转模式下以与门（7）的方向相反的方向旋转，使得其上游边缘径向地更靠近管道轴线比其下游边缘，从而形成舀起流的内部以控制反向流动层并提供有效的推力反转。

5. 发明申请

WO1997003284A1 TURBOFAN ENGINE THRUST REVERSER WITH ASYMMETRICAL DOORS 审中-公开
标题翻译：涡轮发动机用不对称门扭转反作用力
公开(公告)号：WO1997003284A1
公开(公告)日：1997-01-30
申请号：PCT/FR1996001078
申请日：1996-07-11
申请人： SOCIETE HISPANO SUIZA
发明人： SOCIETE HISPANO SUIZA , LARDY, Pascal , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/563 , F02K1/70
摘要： A turbofan engine thrust reverser comprising pivotable doors (27, 37) that are integrated into the outer wall of the flow duct behind the fan when the flow is undeflected, and can be pivoted to form flow deflecting obstacles in thrust reversal mode. The width (25) of the doors (27) on one side is smaller than the width (26) of the doors (37) on the opposite side relative to the turbojet axis.
摘要翻译：涡轮风扇发动机推力反向器，其包括可旋转的门（27,37），当所述流动不被偏转时，所述可旋转门（27,37）被集成到所述风扇后面的所述流动管道的外壁中，并且可以枢转以在推力反转模式下形成流动偏转障碍物。门（27）的一侧的宽度（25）小于相对于涡轮喷气轴线的相对侧的门（37）的宽度（26）。

6. 发明申请

WO1997043537A1 THRUST REVERSER FOR A TURBO-JET ENGINE WITH DOORS ASSOCIATED TO AN UPSTREAM PANEL 审中-公开
标题翻译：用于具有与上游面板相关的门的涡轮喷气发动机的扭矩反转器
公开(公告)号：WO1997043537A1
公开(公告)日：1997-11-20
申请号：PCT/FR1997000863
申请日：1997-05-15
申请人： SOCIETE HISPANO SUIZA
发明人： SOCIETE HISPANO SUIZA , GONIDEC, Patrick , ROUYER, Pascal, Gérard , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/70 , Y02T50/671
摘要： A thrust reverser for a twin flow turbo-jet engine comprises pivoting doors (7) integrated in the direct jet pod wall and forming obstacles for deviating the reverse jet flow. Each upstream part of the doors (7) is internally lined with an upstream panel (22) thereby providing a smoothing of the direct jet air flow. The upstream panel (22) is supported along one side by means of a longitudinal rotary shaft integral with the fixed structure (1) and is driven by a set of rods (24, 26, 28) comprising a hinge (27) to the door (7), a hinge (23) to the fixed structure (1) and a hinge (29) to the upstream panel (22) so that the latter (22) is moved in lateral pivoting with respect to said rotary shaft (40).
摘要翻译：用于双流涡轮喷气发动机的推力反向器包括集成在直接喷射舱壁中的枢转门（7）并且形成用于偏离反向喷射流的障碍物。门（7）的每个上游部分内部具有上游面板（22），从而提供直接喷射空气流的平滑化。上游板（22）通过与固定结构（1）成一体的纵向旋转轴沿着一侧支撑，并由一组杆（24,26,28）驱动，所述杆包括铰链（27）到门（7），到固定结构（1）的铰链（23）和到上游面板（22）的铰链（29），使得后者（22）相对于所述旋转轴（40）横向枢转地移动，。

7. 发明申请

WO1997010425A1 TURBOJET THRUST REVERSER HAVING DOORS COMBINED WITH A PRIMARY PANEL 审中-公开
标题翻译： TURBOJET THRUST REVERSER具有与主面板组合的门
公开(公告)号：WO1997010425A1
公开(公告)日：1997-03-20
申请号：PCT/FR1996001402
申请日：1996-09-12
申请人： SOCIETE HISPANO SUIZA
发明人： SOCIETE HISPANO SUIZA , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/70
CPC分类号： F02K1/68 , F02K1/70 , Y02T50/671
摘要： A dual flow turbojet thrust reverser has pivoting doors (7) integrated in direct jet mode with the outer wall of the blower duct (14) and capable of forming deflection members in thrust reversing mode. Each door (7) is coupled to a primary panel (21), integrated in direct jet mode in the outer cowling (19) of the turbojet and continuous with the inner wall of the blower duct (14), and capable of being displaced, in thrust reversing mode, so as to be located inside the annular duct (14) to co-operate with said door (7) and deviate the stream.
摘要翻译：双流涡轮喷气推进反向器具有以直接喷射模式与鼓风机管道（14）的外壁集成的枢转门（7），并且能够在推力反向模式下形成偏转构件。每个门（7）联接到主面板（21），其在涡轮喷气发动机的外罩（19）中以直接喷射模式集成，并与鼓风机通道（14）的内壁连续并且能够被移位，在推力反转模式中，以便位于环形管道（14）的内部以与所述门（7）配合并偏离所述流。

8. 发明申请

WO1997044577A1 TURBOFAN THRUST REVERSER WITH OBSTACLES LINKED TO THE PRIMARY COWLING 审中-公开
标题翻译： TURBOFAN扭转与主要连接的障碍
公开(公告)号：WO1997044577A1
公开(公告)日：1997-11-27
申请号：PCT/FR1997000903
申请日：1997-05-23
申请人： SOCIETE HISPANO-SUIZA
发明人： SOCIETE HISPANO-SUIZA , VAUCHEL, Guy, Bernard
IPC分类号： F02K01/68
CPC分类号： F02K1/68 , Y02T50/671
摘要： A turbofan thrust reverser comprises movable elements (6, 7) integrated in direct jet into the wall of the turbofan primary cowling (10) and forming flow deviation obstacles in reverse jet. Each movable element supported by pivoting axes (12) formed integrally with the fixed structure is constituted by an external panel (6) pivoting by the action of an actuator (13) fixed on the primary cowling (10) and ensuring in direct jet the aerodynamic profile of the primary cowling (10) and an internal panel (7) superimposed in direct jet under the said external panel (6) and capable, in thrust reversal, of sliding in the extension of the external panel (6) ensuring the deviation of the reverse flow.
摘要翻译：涡轮风扇推力反向器包括集成在涡轮风扇主罩（10）的壁中的直接喷射的可移动元件（6,7），并在反向喷射中形成流动偏差障碍物。由与固定结构一体形成的枢转轴线（12）支撑的每个可移动元件由固定在主罩（10）上的致动器（13）的作用枢转的外部板（6）构成，并且确保直接喷射空气动力所述主罩（10）的轮廓和在所述外部板（6）下方直接喷射的内部板（7），并且能够在推力反向中在外部板（6）的延伸部中滑动，从而确保偏差反向流动。

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