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1. 发明授权

US08635851B2 Grid thrust reverser cover comprising a seal support and associated seal 有权
标题翻译：网格推力反向器盖包括密封支撑件和相关密封件
公开(公告)号：US08635851B2
公开(公告)日：2014-01-28
申请号：US12594829
申请日：2008-02-29
申请人： Guy Vauchel , Eric Lecossais , Frederic Zoonekyndt
发明人： Guy Vauchel , Eric Lecossais , Frederic Zoonekyndt
IPC分类号： F02K1/72
CPC分类号： F16J15/027 , F01D11/005 , F02K1/70 , F02K1/72 , F05D2240/55 , F16J15/062
摘要： This grid thrust reverser cover comprises a seal support and a seal mounted in this support by means of two fastening lugs, this seal being capable of interacting with a diversion edge of this thrust reverser. At least one of the said lugs is turned up and the said support has a section matching that defined by the said lugs.
摘要翻译：该格栅推力反向器盖包括密封支撑件和通过两个紧固凸耳安装在该支撑件中的密封件，该密封件能够与该推力反向器的转向边缘相互作用。所述凸耳中的至少一个凸起并且所述支撑件具有由所述凸耳限定的部分。

2. 发明申请

US20100044466A1 GRID THRUST REVERSER COVER COMPRISING A SEAL SUPPORT AND ASSOCIATED SEAL 有权
标题翻译：包括密封支持和相关密封的网格扭矩反转器盖
公开(公告)号：US20100044466A1
公开(公告)日：2010-02-25
申请号：US12594829
申请日：2008-02-29
申请人： Guy Vauchel , Eric Lecossais , Frederic Zoonekyndt
发明人： Guy Vauchel , Eric Lecossais , Frederic Zoonekyndt
IPC分类号： F02K1/72 , F02K1/54
CPC分类号： F16J15/027 , F01D11/005 , F02K1/70 , F02K1/72 , F05D2240/55 , F16J15/062
摘要： This grid thrust reverser cover comprises a seal support and a seal mounted in this support by means of two fastening lugs, this seal being capable of interacting with a diversion edge of this thrust reverser. At least one of the said lugs is turned up and the said support has a section matching that defined by the said lugs.
摘要翻译：该格栅推力反向器盖包括密封支撑件和通过两个紧固凸耳安装在该支撑件中的密封件，该密封件能够与该推力反向器的转向边缘相互作用。所述凸耳中的至少一个凸起并且所述支撑件具有由所述凸耳限定的部分。

3. 发明申请

US20060005530A1 Thrust reverser comprising optimised deflector gratings 失效
标题翻译：推力反向器包括优化的偏转光栅
公开(公告)号：US20060005530A1
公开(公告)日：2006-01-12
申请号：US10536308
申请日：2003-12-22
申请人： Laurent Blin , Xavier Cazuc , Guy Vauchel
发明人： Laurent Blin , Xavier Cazuc , Guy Vauchel
IPC分类号： F02K1/54
CPC分类号： F02K1/72 , F02K1/625 , F02K3/04 , F05D2240/12 , Y02T50/671
摘要： The invention relates to a device comprising gratings, which are used to form a reverse flow from a jet engine thrust flow. The inventive device comprises a plurality of flow diverter gratings which are disposed side-by-side at the outer edge of an annular thrust flow circulation channel. Each of the gratings comprises a plurality of intersecting inner transverse blades and inner longitudinal blades, two adjacent gratings being separated by a side clearance which generates a leakage flow. The device also comprises means of re-directing the aforementioned leakage flow in a direction such as to increase the effectiveness of the reverse flow, said re-direction means comprising aerodynamic appendages which are mounted to at least one outer longitudinal edge of each grating.
摘要翻译：本发明涉及一种包括光栅的装置，其用于从喷气发动机推力流形成反向流。本发明的装置包括多个分流器光栅，它们并排设置在环形推力流通道的外边缘处。每个光栅包括多个相交的内横向叶片和内纵向叶片，两个相邻的光栅由侧间隙分开，产生泄漏流。该装置还包括在诸如增加逆流的有效性的方向上重新引导上述泄漏流的装置，所述重新方向装置包括安装在每个光栅的至少一个外部纵向边缘上的气动附加物。

4. 发明申请

US20100192715A1 MULTIPLE-ACTING LINEAR ACTUATOR 审中-公开
标题翻译：多功能线性执行器
公开(公告)号：US20100192715A1
公开(公告)日：2010-08-05
申请号：US12665158
申请日：2008-03-28
申请人： Guy Vauchel , Pierre Baudu
发明人： Guy Vauchel , Pierre Baudu
IPC分类号： F16H27/02
CPC分类号： F02K1/763 , F16H25/20 , F16H25/2056 , F16H2025/2075 , F16H2025/2084 , F16H2025/2093 , Y10T74/18672
摘要： The present invention relates to a multiple-acting linear actuator (100) intended to drive at least two elements capable of moving relative to a fixed element comprising a plurality of rod-forming concentric tubular bodies (103, 102, 104) engaged successively one inside the next via external and/or internal screw threads (105, 106, 107, 108), characterized in that one of the bodies is connected to rotational-drive means (109), the other bodies then together forming an internal and/or external transmission train, and in that said bodies are associated with selective lock-up means whereas the outermost bodies of the internal and/or external transmission trains are permanently prevented from rotating.
摘要翻译：本发明涉及一种多作用线性致动器（100），其旨在驱动至少两个能够相对于固定元件移动的元件，所述元件包括多个连续地接合一个内部的杆形同心管状体（103,102,104）下一个通过外部和/或内部螺纹（105,106,107,108），其特征在于，其中一个主体连接到旋转驱动装置（109），然后另一个主体一起形成内部和/或外部传动系，并且所述主体与选择性锁定装置相关联，而内部和/或外部传动系的最外侧主体被永久地防止旋转。

5. 发明授权

US09027708B2 Aircraft turbojet engine nacelle air intake maintenance trolley 有权
标题翻译：飞机涡轮喷气发动机机舱空气进气维护手推车
公开(公告)号：US09027708B2
公开(公告)日：2015-05-12
申请号：US12739289
申请日：2008-06-20
申请人： Guy Vauchel , Jean-Philippe Dauguet , Stephane Beilliard
发明人： Guy Vauchel , Jean-Philippe Dauguet , Stephane Beilliard
IPC分类号： E04G3/32 , B64F5/00
CPC分类号： B64F5/00 , B64F5/50
摘要： This maintenance trolley (17) for the air intake (9) of the nacelle of an aircraft turbojet engine is notable in that it comprises a base (19) and a platform (23) cantilever-mounted on this base (19) and designed to enter said air intake (9) without contact therewith.
摘要翻译：用于飞行器涡轮喷气发动机的机舱的进气口（9）的这种维护手推车（17）是显着的，因为它包括基座（19）和悬臂安装在该基座（19）上的平台（23），并被设计成进入所述进气口（9）而不与其接触。

6. 发明申请

US20100171319A1 DEVICE FOR LOCKING AN OPENING PART OF A JET ENGINE NACELLE WITH RESPECT TO A FIXED PART, AND NACELLE EQUIPPED WITH SUCH A DEVICE 有权
标题翻译：用于锁定喷气发动机的打开部分的装置，相对于固定部件，以及装备有这种装置的NACELLE
公开(公告)号：US20100171319A1
公开(公告)日：2010-07-08
申请号：US12601563
申请日：2008-03-28
申请人： Jean-Philippe Joret , Guy Vauchel
发明人： Jean-Philippe Joret , Guy Vauchel
IPC分类号： E05C19/10 , E05C19/00 , E05B47/00 , B64D29/06
CPC分类号： E05C19/145 , B64D29/06 , E05B1/00 , E05B13/00 , E05B17/22 , Y10T292/08 , Y10T292/0945 , Y10T292/1075
摘要： This device for locking an opening part (9) of a jet engine nacelle with respect to a fixed part (7, 17) comprises: means (13, 16) for locking said opening part (9) with respect to said fixed part (7, 17), means for actuating (21) these locking means that are mounted such that they can move on said opening part (9) between a closed position, in which they enable said locking means (13, 16) to be immobilized, and an open position, in which they enable these locking means (13, 16) to be released. Said actuating means comprise gripping means (21). This device comprises means (41, 43) for immobilizing, in the open position, said gripping means (21) with respect to said opening part (9) at least in the direction of movement of said opening part (9).
摘要翻译：用于锁定喷气发动机机舱相对于固定部分（7,17）的开口部分（9）的装置包括：用于相对于所述固定部分（7,17）锁定所述开口部分（9）的装置（13,16），17），用于致动（21）这些锁定装置的装置，其被安装成使得它们可以在其中使得所述锁定装置（13,16）被固定的关闭位置之间在所述开口部分（9）上移动;以及打开位置，其中它们使得能够释放这些锁定装置（13,16）。所述致动装置包括夹紧装置（21）。该装置包括至少在所述开口部分（9）的运动方向上相对于所述开口部分（9）在打开位置中固定所述夹持装置（21）的装置（41,43）。

7. 发明申请

US20100218480A1 ACTUATOR FOR AN AIRCRAFT NACELLE MOBILE STRUCTURE, AND NACELLE COMPRISING AT LEAST ONE SUCH ACTUATOR 失效
标题翻译：用于航空器移动结构的执行器，以及至少包括一个这样的致动器的起动器
公开(公告)号：US20100218480A1
公开(公告)日：2010-09-02
申请号：US12682139
申请日：2008-09-12
申请人： Guy Vauchel , Jean-Philippe Joret , Pierre Baudu , Christophe Guenadou
发明人： Guy Vauchel , Jean-Philippe Joret , Pierre Baudu , Christophe Guenadou
IPC分类号： F02K1/76 , F02K1/54
CPC分类号： F02K1/763 , B64D29/06 , F16H25/20 , F16H2025/2037
摘要： This actuator for an aircraft engine nacelle mobile structure (9) comprises a motor (1) intended to be mounted on a fixed part of the said nacelle, an endless screw (21) able to be turned by this motor (1), a slideway (5) intended to be connected to the said mobile structure (9) and comprising a nut (29) in mesh with the said endless screw, and a first ball end (15) allowing an angular offset between the axis of the said endless screw (21) and the said slideway (5). This actuator is notable in that it comprises a sleeve (19) able to accommodate the said screw (21) and extending with clearance inside the said slideway (5), the said nut (29) being mounted on that end of the said sleeve (19) that is closest to the said motor (1), and the said first ball end being interposed between the other end of the said sleeve (19) and the said slideway (5).
摘要翻译：用于飞机发动机机舱移动结构（9）的致动器包括：将要安装在所述机舱的固定部分上的电动机（1），能够被该马达（1）转动的环形螺钉（21），滑道（5），其旨在连接到所述移动结构（9）并且包括与所述环形螺钉啮合的螺母（29）和允许所述环形螺钉的轴线之间的角度偏移的第一球形端（15）（21）和所述滑道（5）。该致动器的特征在于它包括能够容纳所述螺钉（21）并且在所述滑道（5）内部的间隙延伸的套筒（19），所述螺母（29）安装在所述套筒的所述端部 19），并且所述第一球端插入在所述套筒（19）的另一端和所述滑道（5）之间。

8. 发明申请

US20060138785A1 Latch for joining two panels of an airplane structure 失效
标题翻译：用于连接飞机结构的两个面板的闩锁
公开(公告)号：US20060138785A1
公开(公告)日：2006-06-29
申请号：US10560254
申请日：2004-06-30
申请人： Guy Vauchel
发明人： Guy Vauchel
IPC分类号： E05C19/12
CPC分类号： E05C19/145 , B64D29/06 , Y10S292/31 , Y10T292/0917
摘要： The invention relates to a latch (1) provided for joining two elements to one another via, on the one hand, a hook (2) capable of coming into contact with a retaining element (18) integrally connected to the first element and, on the other, via a main pin (3) to be attached in a fixed manner to the second element. Said latch has a handle (6) that is mounted so that it can pivot about an end pin (13) and has an articulation having a pair of compression links (4) mounted in a manner that enables them to pivot about the main pin (3) and about an intermediate pin (14). The invention is characterized in that the hook is inserted between the handle and the main pin, and in that at least one compression link (4) is provided with a guiding means (21) capable of coming into contact with the surface of the hook facing the handle during the opening of the latch.
摘要翻译：本发明涉及一种用于将两个元件彼此接合的闩锁（1），一方面是能够与整体连接到第一元件的保持元件（18）接触的钩（2），并且在另一个，经由主销（3）以固定的方式附接到第二元件。所述闩锁具有手柄（6），所述手柄（6）被安装成使得其能够围绕端部销（13）枢转并且具有铰接件，所述铰接件具有一对压缩连接件（4），所述压缩连接件（4）以能够绕所述主销 3）和中间销（14）。本发明的特征在于，钩被插入在手柄和主销之间，并且至少一个压缩连杆（4）设置有能够与钩面对面接触的引导装置（21）在闩锁打开期间的手柄。

9. 发明授权

US09004548B2 Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device 有权
标题翻译：用于锁定喷气发动机机舱相对于固定部分的开口部分的装置，以及配备有这种装置的机舱
公开(公告)号：US09004548B2
公开(公告)日：2015-04-14
申请号：US12601563
申请日：2008-03-28
申请人： Jean-Philippe Joret , Guy Vauchel
发明人： Jean-Philippe Joret , Guy Vauchel
IPC分类号： E05C19/10 , E05C19/14 , B64D29/06 , E05B1/00 , E05B13/00 , E05B17/22
CPC分类号： E05C19/145 , B64D29/06 , E05B1/00 , E05B13/00 , E05B17/22 , Y10T292/08 , Y10T292/0945 , Y10T292/1075
摘要： This device for locking an opening part (9) of a jet engine nacelle with respect to a fixed part (7, 17) comprises: means (13, 16) for locking said opening part (9) with respect to said fixed part (7, 17), means for actuating (21) these locking means that are mounted such that they can move on said opening part (9) between a closed position, in which they enable said locking means (13, 16) to be immobilized, and an open position, in which they enable these locking means (13, 16) to be released. Said actuating means comprise gripping means (21). This device comprises means (41, 43) for immobilizing, in the open position, said gripping means (21) with respect to said opening part (9) at least in the direction of movement of said opening part (9).
摘要翻译：用于锁定喷气发动机机舱相对于固定部分（7,17）的开口部分（9）的装置包括：用于相对于所述固定部分（7,17）锁定所述开口部分（9）的装置（13,16），17），用于致动（21）这些锁定装置的装置，其被安装成使得它们可以在其中使得所述锁定装置（13,16）被固定的关闭位置之间在所述开口部分（9）上移动;以及打开位置，其中它们使得能够释放这些锁定装置（13,16）。所述致动装置包括夹紧装置（21）。该装置包括至少在所述开口部分（9）的运动方向上相对于所述开口部分（9）在打开位置中固定所述夹持装置（21）的装置（41,43）。

10. 发明授权

US08464512B2 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator 失效
标题翻译：用于飞机机舱移动结构的致动器，以及包括至少一个这种致动器的机舱
公开(公告)号：US08464512B2
公开(公告)日：2013-06-18
申请号：US12682139
申请日：2008-09-12
申请人： Guy Vauchel , Jean-Philippe Joret , Pierre Baudu , Christophe Guenadou
发明人： Guy Vauchel , Jean-Philippe Joret , Pierre Baudu , Christophe Guenadou
IPC分类号： F02K1/54 , F02K1/64
CPC分类号： F02K1/763 , B64D29/06 , F16H25/20 , F16H2025/2037
摘要： This actuator for an aircraft engine nacelle mobile structure (9) comprises a motor (1) intended to be mounted on a fixed part of the said nacelle, an endless screw (21) able to be turned by this motor (1), a slideway (5) intended to be connected to the said mobile structure (9) and comprising a nut (29) in mesh with the said endless screw, and a first ball end (15) allowing an angular offset between the axis of the said endless screw (21) and the said slideway (5). This actuator is notable in that it comprises a sleeve (19) able to accommodate the said screw (21) and extending with clearance inside the said slideway (5), the said nut (29) being mounted on that end of the said sleeve (19) that is closest to the said motor (1), and the said first ball end being interposed between the other end of the said sleeve (19) and the said slideway (5).
摘要翻译：用于飞机发动机机舱移动结构（9）的致动器包括：将要安装在所述机舱的固定部分上的电动机（1），能够被该马达（1）转动的环形螺钉（21），滑道（5），其旨在连接到所述移动结构（9）并且包括与所述环形螺钉啮合的螺母（29）和允许所述环形螺钉的轴线之间的角度偏移的第一球形端（15）（21）和所述滑道（5）。该致动器的特征在于它包括能够容纳所述螺钉（21）并且在所述滑道（5）内部的间隙延伸的套筒（19），所述螺母（29）安装在所述套筒的所述端部 19），并且所述第一球端插入在所述套筒（19）的另一端和所述滑道（5）之间。

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