公开(公告)号：US20110088242A1

公开(公告)日：2011-04-21

申请号：US12918144

申请日：2009-02-13

申请人： Etienne Luneau ,  Bastien Bellavia ,  Philipppe Prot

发明人： Etienne Luneau ,  Bastien Bellavia ,  Philipppe Prot

IPC分类号： B23P11/00 ,  F16B12/10

CPC分类号： B25B31/005 ,  B21J15/043 ,  B21J15/42 ,  F16B19/109 ,  Y10T29/49908 ,  Y10T29/49915 ,  Y10T29/49934 ,  Y10T29/49947 ,  Y10T29/53657 ,  Y10T29/53735 ,  Y10T29/5377 ,  Y10T29/53878 ,  Y10T29/53909 ,  Y10T29/53943 ,  Y10T403/557

摘要： A fastening device for preassembling structural members includes a hollow cylindrical body; a bearing ring provided at a proximal end of the hollow body and against which one of the structural members is intended to bear in a fastening position; a pulling threaded rod extending through the hollow body to be inserted into the structural members; a tightening means connected to the pulling threaded rod for maintaining the structural members against each other, the tightening means including a removable tubular end piece for mounting on a proximal threaded end of the pulling rod that can be locally axially compacted under the action of a force applied on said pulling rod in order to form a radial bead for sandwiching the structural members between the latter and the bearing ring; the fastening device including a sheath.

摘要翻译： 用于预组装结构构件的紧固装置包括中空圆柱体; 轴承环，其设置在所述中空体的近端处，并且所述结构构件中的一个旨在承受处于紧固位置; 延伸穿过所述中空体以被插入到所述结构构件中的拉杆; 连接到牵引螺纹杆的紧固装置，用于将结构构件相互抵靠，紧固装置包括可拆卸的管状端件，用于安装在拉杆的近端螺纹端部，其可以在力的作用下局部轴向压实 施加在所述拉杆上以便形成用于将结构构件夹在其间和轴承环之间的径向胎圈; 所述紧固装置包括护套。

公开(公告)号：US08869372B2

公开(公告)日：2014-10-28

申请号：US12918144

申请日：2009-02-13

申请人： Etienne Luneau ,  Bastien Bellavia ,  Philippe Prot

发明人： Etienne Luneau ,  Bastien Bellavia ,  Philippe Prot

IPC分类号： F16B13/04 ,  B23P19/02 ,  B23P19/04 ,  B25B27/00 ,  B25B27/14 ,  B21D39/00 ,  B23P11/00 ,  B21J15/42 ,  B25B31/00 ,  F16B19/10 ,  B21J15/04

CPC分类号： B25B31/005 ,  B21J15/043 ,  B21J15/42 ,  F16B19/109 ,  Y10T29/49908 ,  Y10T29/49915 ,  Y10T29/49934 ,  Y10T29/49947 ,  Y10T29/53657 ,  Y10T29/53735 ,  Y10T29/5377 ,  Y10T29/53878 ,  Y10T29/53909 ,  Y10T29/53943 ,  Y10T403/557

摘要： A fastening device for preassembling structural members includes a hollow cylindrical body; a bearing ring provided at a proximal end of the hollow body and against which one of the structural members is intended to bear in a fastening position; a pulling threaded rod extending through the hollow body to be inserted into the structural members; a tightening means connected to the pulling threaded rod for maintaining the structural members against each other, the tightening means including a removable tubular end piece for mounting on a proximal threaded end of the pulling threaded rod that can be locally axially compacted under the action of a force applied on the pulling threaded rod in order to form a radial bead for sandwiching the structural members between the latter and the bearing ring; the fastening device including a sheath.

摘要翻译： 用于预组装结构构件的紧固装置包括中空圆柱体; 轴承环，其设置在所述中空体的近端处，并且所述结构构件中的一个旨在承受处于紧固位置; 延伸穿过所述中空体以被插入到所述结构构件中的拉杆; 连接到牵引螺纹杆的紧固装置，用于将结构构件彼此抵靠，紧固装置包括可拆卸的管状端件，用于安装在牵引螺杆的近端螺纹端上，其可在局部轴向压实 施加在牵引螺纹杆上的力，以便形成用于将结构构件夹在后者和轴承环之间的径向胎圈; 所述紧固装置包括护套。

公开(公告)号：US20070029444A1

公开(公告)日：2007-02-08

申请号：US11415285

申请日：2006-05-02

申请人： Bertrand Mercier ,  Etienne Luneau

发明人： Bertrand Mercier ,  Etienne Luneau

IPC分类号： B64D11/06 ,  B60N2/42

CPC分类号： B64D11/0619 ,  B60N2/42736 ,  B64D11/062 ,  B64D25/04

摘要： The invention relates to an aircraft safety seat (1) comprising a supporting structure (5) and a bucket seat (2) supported by said structure, said bucket seat (2) comprising a seat (3) and a back (4) which are linked together, said back being installed on said structure so as to slide generally downwards, characterised in that it comprises at least one connecting rod (6) connected by its first end (6a) to said support and by its other end (6b) to said seat, said connecting rod (6) being generally horizontal when in normal use, and being suited for pivoting downwards by its first end under the effect of a force exerted downwards on said seat, against the action of a shock absorber (7).

摘要翻译： 本发明涉及一种包括支撑结构（5）和由所述结构支撑的铲斗座（2）的飞行器安全座（1），所述铲斗座（2）包括座（3）和后（4） 连接在一起，所述后部安装在所述结构上以便大致向下滑动，其特征在于，其包括至少一个连接杆（6），所述至少一个连杆通过其第一端（6a）连接到所述支撑件，并且其另一端（6b ）连接到所述座椅上，所述连杆（6）在正常使用时大致水平，并且适于在受到向下施加在所述座椅上的力的作用下由其第一端向下枢转，抵抗减震器（7 ）。

公开(公告)号：US20120151724A1

公开(公告)日：2012-06-21

申请号：US13279217

申请日：2011-10-21

申请人： Vincent DEFRANCE ,  Etienne Luneau

发明人： Vincent DEFRANCE ,  Etienne Luneau

IPC分类号： F16B45/02

CPC分类号： E05C19/145 ,  B64D29/06 ,  E05B63/06 ,  Y10T24/45435

摘要： The invention relates to a hook latch (73) configured so as to lock and unlock a mobile structure on a fixed structure of a vehicle, said latch having an adapter (69) fitted with a hook (73) capable of fastening a keeper, a handle comprising a trigger, on the handle, a second pivot connection axis, on the trigger, at least one hook capable of fastening at least one protrusion (125) of a bracket (121) connected to the adapter, a third pivot connection axis, around which the handle and the adapter are guided in rotation in relation to each other, and characterised in that it comprises an adjustment device for adjusting the flushness of the upper surface of the handle in relation to the aerodynamic surface, said device comprising the bracket (121), a screw (129) capable of being screwed and unscrewed within a first tapped recess of the adapter.

摘要翻译： 本发明涉及一种构造成在车辆的固定结构上锁定和解锁移动结构的钩闩（73），所述闩锁具有装配有能够固定保持器的钩（73）的适配器（69） 手柄，其包括在所述手柄上的触发器上的触发器上的第二枢转连接轴线，至少一个钩子，其能够紧固连接到所述适配器的托架（121）的至少一个突起（125），第三枢转连接轴线， 手柄和适配器相对于彼此旋转地引导，其特征在于，其包括调节装置，用于相对于空气动力学表面调节手柄的上表面的平齐度，所述装置包括支架（ 121），螺钉（129）能够在适配器的第一抽头凹槽内旋拧并拧下。

公开(公告)号：US08740147B2

公开(公告)日：2014-06-03

申请号：US13558291

申请日：2012-07-25

申请人： Vincent Defrance ,  Marc Roussy ,  Etienne Luneau

发明人： Vincent Defrance ,  Marc Roussy ,  Etienne Luneau

IPC分类号： B64C1/14

CPC分类号： B64D29/06 ,  E05B51/023 ,  E05B2015/0448 ,  E05C19/02 ,  Y10T292/0917 ,  Y10T292/0929 ,  Y10T292/202

摘要： The invention relates to a pressure relief latch for aircraft, able to absorb vibrations and shocks without inopportune opening, as well as to adapt to dimensional stresses during its assembly. The latch includes: a console, a lever mounted on the console, and an opening effort exerted on a fulcrum of the lever causing an angular displacement of the fulcrum between a closing position and an opening position. The latch also includes a roller able to roll against a profile of the lever and connected to an elastic return device. The latch further being provided with means able to vary the angular displacement of the fulcrum of the lever according to the opening effort, with two different slopes according to an opening effort E1.

摘要翻译： 本发明涉及一种用于飞行器的压力释放闩锁，其能够吸收振动和冲击而不会不适当地打开，以及在组装期间适应尺寸应力。 闩锁包括：控制台，安装在控制台上的杠杆，以及施加在杆的支点上的开启力，导致支点在关闭位置和打开位置之间的角位移。 闩锁还包括能够滚动抵靠杠杆的轮廓并连接到弹性返回装置的滚子。 闩锁还设置有能够根据打开力量改变杠杆的支点的角位移的装置，根据打开力量E1具有两个不同的斜率。

公开(公告)号：US09567784B2

公开(公告)日：2017-02-14

申请号：US13279217

申请日：2011-10-21

申请人： Vincent Defrance ,  Etienne Luneau

发明人： Vincent Defrance ,  Etienne Luneau

IPC分类号： E05C5/00 ,  E05C19/12 ,  E05C19/14 ,  E05C19/10 ,  B65D45/00 ,  B65D45/30 ,  B65D45/32 ,  E05B63/06 ,  B64D29/06

CPC分类号： E05C19/145 ,  B64D29/06 ,  E05B63/06 ,  Y10T24/45435

摘要： The invention relates to a hook latch (73) configured so as to lock and unlock a mobile structure on a fixed structure of a vehicle, said latch having an adapter (69) fitted with a hook (73) capable of fastening a keeper, a handle comprising a trigger, on the handle, a second pivot connection axis, on the trigger, at least one hook capable of fastening at least one protrusion (125) of a bracket (121) connected to the adapter, a third pivot connection axis, around which the handle and the adapter are guided in rotation in relation to each other, and characterised in that it comprises an adjustment device for adjusting the flushness of the upper surface of the handle in relation to the aerodynamic surface, said device comprising the bracket (121), a screw (129) capable of being screwed and unscrewed within a first tapped recess of the adapter.

摘要翻译： 锁具有配备有钩（73）的适配器（69），用于悬挂固定到固定和可移动结构的撞击。 手柄或触发器具有上表面以露出车辆的空气动力学表面，即皮肤。 调节装置调节上表面相对于空气动力学表面的露头。 该装置具有包括侧板（123）的夹具（121），并且在其中一个板上布置有突起和上板（127）。 将螺钉（129）拧紧并旋拧到适配器的空腔的螺纹中。 螺钉的头部（131）支撑在上板上。 还包括以下独立权利要求：（1）组装棘爪的方法（2）一种用于调节棘爪的手柄上表面的方法。

公开(公告)号：US07628357B2

公开(公告)日：2009-12-08

申请号：US11415285

申请日：2006-05-02

申请人： Bertrand Mercier ,  Etienne Luneau

发明人： Bertrand Mercier ,  Etienne Luneau

IPC分类号： B64D25/04

CPC分类号： B64D11/0619 ,  B60N2/42736 ,  B64D11/062 ,  B64D25/04

摘要： An aircraft safety seat that has a supporting structure and a bucket seat supported by the structure, the bucket seat has a seat and a back which are lined together, the back being installed on the structure so as to slide generally downwards, wherein at least one connection rod connected by its first end to the support and by its other end to the seat, the connecting rod being generally horizontal when in normal use, and being suited for pivoting downwards by its first end under the effect of a force exerted downwards on the seat, against the action of a shock absorber.

摘要翻译： 一种具有支撑结构的飞行器安全座椅和由所述结构支撑的铲斗座，所述铲斗座具有排列在一起的座椅和后部，所述后部安装在所述结构上以便大致向下滑动，其中至少一个 连接杆通过其第一端连接到支撑件并且通过其另一端连接到座椅，连接杆在正常使用时大体上是水平的，并且适于在其向下施加的力的作用下由其第一端向下枢转 座位，抵抗减震器的作用。