公开(公告)号：US10150553B2

公开(公告)日：2018-12-11

申请号：US13533266

申请日：2012-06-26

申请人： Bruno Cacciaguerra ,  Alain Depeige ,  Jean-Claude Lacombe ,  Hélène Cazeneuve ,  Marc-Antoine Castanet

发明人： Bruno Cacciaguerra ,  Alain Depeige ,  Jean-Claude Lacombe ,  Hélène Cazeneuve ,  Marc-Antoine Castanet

IPC分类号： B64C1/06 ,  B64F5/10 ,  B64C1/00

摘要： A device and method for assembling two aircraft fuselage sections each comprising a skin and longitudinal stiffeners, the device comprising fishplates fishing couples of mutually aligned longitudinal stiffeners belonging respectively to said sections, each fishplate comprising two fishplate pieces each comprising at least one longitudinal sole plate intended to be fixed to a longitudinal stiffener, and a transverse support head, and at least one demountable connecting member able to mutually clamp the respective support heads of said fishplate pieces to allow a transmission of longitudinal forces between these fishplate pieces.

公开(公告)号：US20130181092A1

公开(公告)日：2013-07-18

申请号：US13533266

申请日：2012-06-26

申请人： Bruno Cacciaguerra ,  Alain Depeige ,  Jean-Claude Lacombe ,  Helene Cazeneuve ,  Marc-Antoine Castanet

发明人： Bruno Cacciaguerra ,  Alain Depeige ,  Jean-Claude Lacombe ,  Helene Cazeneuve ,  Marc-Antoine Castanet

IPC分类号： B64C1/06 ,  B64F5/00

CPC分类号： B64C1/069 ,  B64C1/068 ,  B64C2001/0081 ,  B64F5/10 ,  Y10T29/49622

摘要： Device for assembling two aircraft fuselage sections each comprising a skin and longitudinal stiffeners, the device comprising fishplates fishing couples of mutually aligned longitudinal stiffeners belonging respectively to said sections, each fishplate comprising two fishplate pieces each comprising at least one longitudinal sole plate intended to be fixed to a longitudinal stiffener, and a transverse support head, and at least one demountable connecting member able to mutually clamp the respective support heads of said fishplate pieces to allow a transmission of longitudinal forces between these fishplate pieces.Set of fuselage sections assembled by means of a device of the type described above.Method of assembling two fuselage sections by means of a device of the type described above.

摘要翻译： 用于组装两个飞行器机身部分的装置，每个飞行器机身部分各自包括皮肤和纵向加强件，该装置包括分别属于所述部分的相互对齐的纵向加强件的鱼板钓鱼钩，每个鱼板包括两个鱼板块，每个鱼板包括至少一个用于固定的纵向底板 纵向加强件和横向支撑头以及能够相互夹紧所述鱼板片的相应支撑头的至少一个可拆卸连接件，以允许在这些鱼片之间传递纵向力。 通过上述类型的装置组装的机身部分组。 通过上述类型的装置组装两个机身部分的方法。

公开(公告)号：US08286915B2

公开(公告)日：2012-10-16

申请号：US12400359

申请日：2009-03-09

申请人： Alain Depeige ,  Jean-Claude Lacombe

发明人： Alain Depeige ,  Jean-Claude Lacombe

IPC分类号： B64C1/14 ,  B64C1/06

CPC分类号： B64C1/1492

摘要： An aircraft having a fuselage of composite type and more particularly to that of aircraft fuselage panels bearing cabin windows. The invention thus concerns a fuselage panel bearing a window comprising a composite structure cast in one piece, the structure comprising a main portion and at least one opening to accommodate a window, the structure having, on a zone surrounding the opening, a thickness more or less constant and greater than the thickness of the main portion of the structure. The invention also concerns an aircraft comprising a composite fuselage, the latter comprising such a panel or a similar panel made of metal material.

摘要翻译： 具有复合型机身的飞机，更具体地涉及轴承舱窗的飞机机身面板的飞机。 因此，本发明涉及一种机身板，其具有包括铸造成一体的复合结构的窗，该结构包括主要部分和至少一个开口以容纳窗口，该结构在围绕开口的区域上具有更多或更多的厚度 较不恒定并且大于结构主体部分的厚度。 本发明还涉及一种包括复合机身的飞机，后者包括这种面板或由金属材料制成的类似面板。

公开(公告)号：US20090230246A1

公开(公告)日：2009-09-17

申请号：US12400359

申请日：2009-03-09

申请人： Alain Depeige ,  Jean-Claude Lacombe

发明人： Alain Depeige ,  Jean-Claude Lacombe

IPC分类号： B64C1/14 ,  B28B1/14

CPC分类号： B64C1/1492

摘要： This invention relates to the design of aircraft (100) having a fuselage (104, 106, 110) of composite type and more particularly to that of aircraft fuselage panels (110) bearing cabin windows (206, 306).The invention thus concerns a fuselage panel (110) bearing a window (206) comprising a composite structure cast in one piece (200, 212), the said structure comprising a main portion (200) and at least one opening (204) to accommodate a window (206), the said structure having, on a zone (213, 214, 216)) surrounding the said opening (204), a thickness more or less constant and greater than the thickness of the main portion (200) of the said structure.The invention also concerns an aircraft (100) comprising a composite fuselage (104, 106, 110), the latter comprising such a panel or a similar panel made of metal material (110).

摘要翻译： 本发明涉及具有复合类型的机身（104,106,110）的飞机（100）的设计，更具体地涉及承载舱窗（206,306）的飞机机身面板（110）的设计。 因此，本发明涉及一种机身板（110），其具有包括铸造成一体（200,212）的复合结构的窗口（206），所述结构包括主要部分（200）和至少一个开口（204），以容纳 窗口（206），所述结构在围绕所述开口（204）的区域（213,214,216）上具有或多或少恒定并且大于所述主体部分（200）的厚度的厚度 说结构。 本发明还涉及一种包括复合机身（104,106,110）的飞行器（100），后者包括由金属材料（110）制成的面板或类似面板。

公开(公告)号：US08511610B2

公开(公告)日：2013-08-20

申请号：US12989205

申请日：2009-03-27

申请人： Alain Depeige

发明人： Alain Depeige

IPC分类号： B64C1/14

CPC分类号： B64C1/1407 ,  B64C1/14 ,  B64C1/143 ,  B64C1/1461

摘要： An aircraft door closing device, and an aircraft incorporating such a device. The door includes a leaf and, connected to the aircraft fuselage, a frame including an opening configured to take the leaf, the leaf adopting a closed position to block the opening and another position to reveal the opening. The device includes a bearing mechanism, some on the leaf and some on the frame, each formed by a crenelated structure, two crenelated structures being arranged such that the teeth of one pass through notches of the other as the leaf moves from one position to the other, and such that the teeth of the leaf structure bear, in the closed position, on the inside face of the corresponding teeth of the frame structure.

摘要翻译： 飞机关门装置，以及装有这种装置的飞机。 门包括叶片，并且连接到飞行器机身，框架包括构造成取叶的开口，叶片采取封闭位置以阻挡开口，另一位置露出开口。 该装置包括一个轴承机构，一些在叶片上，一些在框架上，每个都由一个楔形结构形成，两个楔形结构被布置成使得当叶片从一个位置移动到另一个位置时，一个齿通过另一个的齿 并且使得叶结构的齿在关闭位置处承载在框架结构的相应齿的内表面上。

公开(公告)号：US20100308172A1

公开(公告)日：2010-12-09

申请号：US12739054

申请日：2008-11-14

申请人： Alain Depeige

发明人： Alain Depeige

IPC分类号： B64C1/12

CPC分类号： B64C1/062 ,  B64C1/12 ,  B64C1/1461

摘要： An aircraft including at least one door for passengers to board the aircraft, and at least one interconnection device connecting an aircraft internal structure component and a skin of a fuselage of the aircraft, the interconnection device being positioned near an internal periphery of the door in a region subject to external knocks and including at least one region that is weakened in terms of compression so as to absorb the knocks experienced by an external face of the skin of the fuselage, the device also being configured to withstand tensile forces applies to an internal face of the skin of the fuselage by internal pressure inside the aircraft.

摘要翻译： 一种飞机，包括至少一个门，用于乘客登上飞机，以及至少一个互连装置，其连接飞行器内部结构部件和飞行器的机身的皮肤，该互连装置位于门的内部周边附近 受到外部敲击的区域，并且包括在压缩方面被削弱的至少一个区域，以便吸收由机身的皮肤的外表面经历的敲击，该装置还被配置成承受张力施加于内表面 机身内部压力的飞机皮肤。

公开(公告)号：US06595466B2

公开(公告)日：2003-07-22

申请号：US09983469

申请日：2001-10-24

申请人： Alain Depeige ,  Jean-Luc Jarrige

发明人： Alain Depeige ,  Jean-Luc Jarrige

IPC分类号： B64D900

CPC分类号： B64D25/14 ,  B64C39/02 ,  B64C39/10 ,  B64C2039/105

摘要： Boarding device for aircraft and flying wings equipped with such a device. The boarding device consists of at least one tunnel (20) connected to the outside of the aerodynamic shell (12) of the aircraft. More precisely, the tunnel is attached to the trailing edge of the fairing (12) and it extends aft approximately parallel to the longitudinal axis of the aircraft. A door (22) closes off the opening between the passenger cabin (10) and the tunnel (20). The rear part (26) of the tunnel (20) is articulated and/or detachable. In order to evacuate the passengers in an emergency, the front, fixed part of the tunnel (24) can be fitted with an inflatable escape slide or an articulated floor.

摘要翻译： 配备有这种装置的飞机和飞翼的登机装置。登机装置由至少一个连接到飞行器的空气动力学外壳（12）的外部的隧道（20）组成。 更准确地说，隧道连接到整流罩（12）的后缘，并且其大致平行于飞行器的纵向轴线延伸。 门（22）关闭客舱（10）和隧道（20）之间的开口。 隧道（20）的后部（26）铰接和/或可拆卸。 为了在紧急情况下撤离乘客，隧道（24）的前部，固定部分可以装有可充气逃生滑道或铰接地板。

公开(公告)号：US09199714B2

公开(公告)日：2015-12-01

申请号：US12739054

申请日：2008-11-14

申请人： Alain Depeige

发明人： Alain Depeige

IPC分类号： B64C1/06 ,  B64C1/12 ,  B64C1/14

CPC分类号： B64C1/062 ,  B64C1/12 ,  B64C1/1461

摘要： An aircraft including at least one door for passengers to board the aircraft, and at least one interconnection device connecting an aircraft internal structure component and a skin of a fuselage of the aircraft, the interconnection device being positioned near an internal periphery of the door in a region subject to external knocks and including at least one region that is weakened in terms of compression so as to absorb the knocks experienced by an external face of the skin of the fuselage, the device also being configured to withstand tensile forces applies to an internal face of the skin of the fuselage by internal pressure inside the aircraft.

摘要翻译： 一种飞机，包括至少一个门，用于乘客登上飞机，以及至少一个互连装置，其连接飞行器内部结构部件和飞行器的机身的皮肤，该互连装置位于门的内部周边附近 受到外部敲击的区域，并且包括在压缩方面被削弱的至少一个区域，以便吸收由机身的皮肤的外表面经历的敲击，该装置还被配置成承受张力施加于内表面 机身内部压力的飞机皮肤。

公开(公告)号：US20110036946A1

公开(公告)日：2011-02-17

申请号：US12989965

申请日：2009-04-29

申请人： Alain Depeige ,  Christian Rivaud

发明人： Alain Depeige ,  Christian Rivaud

IPC分类号： B64C1/18

CPC分类号： B64C1/18 ,  B64F5/10

摘要： A method of fitting-out of an aircraft by laying of a floor, particularly in a cockpit of an aircraft, and such a fitted-out aircraft. The aircraft includes a fuselage part defining an interior volume and at least one internal on-board structure, the on-board structure being secured to the fuselage part and configured to accept a floor module. The method then involves introducing the floor module into the volume and attaching the floor module to the on-board structure.

摘要翻译： 通过铺设地板，特别是在飞机的驾驶舱中装配飞机的方法以及这种装配的飞机。 飞行器包括限定内部体积的机身部件和至少一个内部车载结构，车载结构固定到机身部件并且被配置为接纳地板模块。 然后，该方法包括将地板模块引入体积并将地板模块附接到车载结构。

公开(公告)号：US09422049B2

公开(公告)日：2016-08-23

申请号：US14006380

申请日：2012-03-22

申请人： Rhona Whitlock ,  Massimo Del Tin ,  Peter Dalton ,  George Ford ,  Michael John Hill ,  Adrian Huntbatch ,  Laurence Breze ,  Alain Depeige

发明人： Rhona Whitlock ,  Massimo Del Tin ,  Peter Dalton ,  George Ford ,  Michael John Hill ,  Adrian Huntbatch ,  Laurence Breze ,  Alain Depeige

IPC分类号： B64C1/06 ,  B64C3/26 ,  B64C3/18 ,  B64C23/06

CPC分类号： B64C3/26 ,  B64C3/187 ,  B64C23/069 ,  Y02T50/164

摘要： A joint comprising first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.

摘要翻译： 包括第一和第二肋部件的接头，所述第一肋具有邻接表面和邻近所述邻接表面设置的多个凸耳; 并且所述第二肋具有邻接表面的邻接表面和邻近所述邻接表面设置的多个凸耳，其中所述相应肋的邻接表面与张力接头邻接并接合，并且其中所述凸耳被固定以形成钉扎的凸耳接头，由 对准多个凸耳中的相应孔，使得第一和第二肋的凸耳交错并且具有穿过对准的凸耳孔的一个或多个销。 接头可以用于将翼尖装置附接到飞机机翼的外侧端。