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1. 发明授权

US09303693B2 Bush assembly 有权
标题翻译：布什总统
公开(公告)号：US09303693B2
公开(公告)日：2016-04-05
申请号：US14397699
申请日：2013-04-25
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Alan Quayle , Paul Hadley , John Colin West , Simon Carrick , John Monteith , Peter Mason
IPC分类号： F16C33/74 , F16C17/02 , B23Q1/25 , F16B43/00
CPC分类号： B25B27/0028 , B23Q1/25 , F16B43/001 , F16C17/02 , F16C33/74 , F16C2326/01
摘要： A bush assembly comprising a component having a bore, a bush fitted in the bore and having a flange that extends radially outwardly over a surface of the component surrounding the bore, and a seal assembly for sealing the interface between the flange and the surface of the component, wherein the seal assembly includes a seal member and a layer of sealant between the seal member and the interface between the flange and the surface of the component. Also a method for sealing a bush, a kit of parts for forming a bush assembly, and a clamping tool for forming a bush assembly.
摘要翻译：一种衬套组件，包括具有孔的部件，安装在所述孔中的衬套，并且具有在围绕所述孔的部件的表面上径向向外延伸的凸缘，以及密封组件，用于密封所述凸缘和所述表面之间的界面组件，其中所述密封组件包括密封构件和所述密封构件与所述凸缘与所述构件表面之间的界面之间的密封剂层。还有一种用于密封衬套的方法，用于形成衬套组件的部件套件和用于形成衬套组件的夹紧工具。

2. 发明授权

US09745049B2 Seal assembly 有权
公开(公告)号：US09745049B2
公开(公告)日：2017-08-29
申请号：US14969422
申请日：2015-12-15
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Alan Quayle , Paul Hadley
IPC分类号： B64C3/50 , B64C7/00 , B64C9/02 , B64C9/22 , B29C70/26
CPC分类号： B64C7/00 , B29C70/26 , B64C3/50 , B64C9/02 , B64C9/22 , Y02T50/43
摘要： A seal assembly for closing an aperture in an aerodynamic surface of a structure, the seal assembly comprising: a track for attachment to the structure; and a retractable seal including a flexible substrate and a plurality of rods connected to the substrate, wherein at least one of the rods is mounted for running movement along the track, and the seal is moveable between an extended position and a retracted position by moving the at least one rod along the track accompanied by folding/unfolding of the seal substrate, and wherein the seal is biased to its extended position.

3. 发明授权

US09254927B2 Retractable infill panel for high-lift device 有权
标题翻译：用于高升力装置的伸缩式填充板
公开(公告)号：US09254927B2
公开(公告)日：2016-02-09
申请号：US14084828
申请日：2013-11-20
申请人： AIRBUS OPERATIONS LIMITED
发明人： Mark Hodkisson , James Wilson , Samuel Evans
IPC分类号： B64D45/00 , B64C9/24
CPC分类号： B64D45/00 , B64C9/24
摘要： The present invention provides an aircraft assembly with a fixed structure and a high-lift device. The fixed structure has a spar, a forward part which provides a foremost edge of an aircraft wing, and a lower part which provides a lower surface of the aircraft wing. A high-lift device is downwardly movable relative to the fixed structure from a stowed configuration to a deployed configuration. The high-lift device has a forward part which provides a foremost edge of the aircraft wing and a lower part which provides a lower surface of the aircraft wing. Downward movement of the high-lift device causes progressive opening of a lateral gap between the lower part of the high-lift device and the lower part of the fixed structure. A retractable infill panel is arranged to progressively extend from a retracted configuration to an extended configuration to fill the lateral gap.
摘要翻译：本发明提供一种具有固定结构和高升力装置的飞行器组件。固定结构具有翼梁，提供飞机机翼的最前缘的前部，以及提供飞机机翼下表面的下部。高升降装置相对于固定结构从收起的构型向下移动到展开构型。高升力装置具有提供飞行器机翼的最前缘的前部，以及提供飞机机翼的下表面的下部。高升力装置的向下运动导致高升降装置的下部与固定结构的下部之间的横向间隙的逐渐打开。可伸缩填充板被布置成从缩回构型逐渐延伸到延伸构型以填充横向间隙。

4. 发明申请

US20150086143A1 BUSH ASSEMBLY 有权
标题翻译：布什组装
公开(公告)号：US20150086143A1
公开(公告)日：2015-03-26
申请号：US14397699
申请日：2013-04-25
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Alan Quayle , Paul Hadley , John Colin West , Simon Carrick , John Monteith , Peter Mason
IPC分类号： F16C33/74 , F16C17/02
CPC分类号： B25B27/0028 , B23Q1/25 , F16B43/001 , F16C17/02 , F16C33/74 , F16C2326/01
摘要： A bush assembly comprising a component having a bore, a bush fitted in the bore and having a flange that extends radially outwardly over a surface of the component surrounding the bore, and a seal assembly for sealing the interface between the flange and the surface of the component, wherein the seal assembly includes a seal member and a layer of sealant between the seal member and the interface between the flange and the surface of the component. Also a method for sealing a bush, a kit of parts for forming a bush assembly, and a clamping tool for forming a bush assembly.
摘要翻译：一种衬套组件，包括具有孔的部件，安装在所述孔中的衬套，并且具有在围绕所述孔的部件的表面上径向向外延伸的凸缘，以及密封组件，用于密封所述凸缘和所述表面之间的界面组件，其中所述密封组件包括密封构件和所述密封构件与所述凸缘与所述构件表面之间的界面之间的密封剂层。还有一种用于密封衬套的方法，用于形成衬套组件的部件套件和用于形成衬套组件的夹紧工具。

5. 发明授权

US10228005B2 Fastener receptacle strip 有权
公开(公告)号：US10228005B2
公开(公告)日：2019-03-12
申请号：US14373108
申请日：2013-01-11
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Paul Hadley , John Gleave
IPC分类号： F16B5/02 , B64C1/12 , B64C3/14 , F16B11/00
摘要： A structural assembly comprising a first component having a ramped surface, and a fastener assembly for fastening the first component to a second component, the fastener assembly including a receptacle strip of resiliently deformable material attached to the ramped surface of the first component so as to assume the contour of the ramped surface, and a plurality of fastener receptacles attached to the receptacle strip for receiving respective fasteners. Also, a method of fastening a first component to a second component using the fastener assembly.

6. 发明授权

US09102393B2 Seal assembly for an aircraft wing 有权
标题翻译：飞机机翼的密封组件
公开(公告)号：US09102393B2
公开(公告)日：2015-08-11
申请号：US13845620
申请日：2013-03-18
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Paul Hadley , Alan Quayle
IPC分类号： B64C3/18 , B64C3/26
CPC分类号： B64C3/185 , B64C3/187 , B64C3/26 , B64C3/28
摘要： A wing assembly for an aircraft is disclosed having a spar, a wing cover, and a rib. The spar has a web portion and a flange portion joined by a radius corner, wherein a gap is formed at an interface between the spar, the wing cover and the rib. The assembly further includes a seal member which substantially covers the gap, and sealant provided between the seal member and the rib and/or the wing cover and/or the spar so as to seal the gap.
摘要翻译：公开了一种用于飞机的翼组件，其具有翼梁，翼盖和肋。翼梁具有腹板部分和由半径角连接的凸缘部分，其中在翼梁，翼罩和肋之间的界面处形成间隙。组件还包括基本上覆盖间隙的密封构件和设置在密封构件与肋和/或翼盖和/或翼梁之间以便密封间隙的密封剂。

7. 发明授权

US09061755B2 Aircraft wing assembly 有权
标题翻译：飞机机翼总成
公开(公告)号：US09061755B2
公开(公告)日：2015-06-23
申请号：US13714666
申请日：2012-12-14
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Paul Hadley , John Gleave
IPC分类号： B64C9/24 , B64C9/22 , B64F5/00
CPC分类号： B64C9/24 , B64C9/22 , Y02T50/32 , Y10T29/49815
摘要： An aircraft wing assembly, comprising a wing having a fixed leading edge, a slat mounted upon a slat deployment mechanism for moving the slat between a retracted position and an extended position with respect to the fixed leading edge, the fixed leading edge having an aperture to accommodate the slat deployment mechanism, and a closing plate mounted off the slat deployment mechanism for closing a gap between a lower trailing edge of the slat and a lower edge of the aperture when the slat is retracted. The closing plate can include a first portion and a second portion, and a hinge connecting the first and the second portions. The closing plate can include a plurality of integrally formed spacer elements for positioning the closing plate with respect to the slat deployment mechanism. Also, a method of removing an access panel in an aircraft wing assembly.
摘要翻译：一种飞机机翼组件，包括具有固定前缘的机翼，安装在用于在缩回位置和相对于固定前缘的延伸位置之间移动所述板条的板条展开机构的板条，所述固定前缘具有孔，适应板条展开机构，以及安装在板条展开机构上的封闭板，用于当板条缩回时封闭板条的下后缘与孔的下边缘之间的间隙。封闭板可以包括第一部分和第二部分，以及连接第一和第二部分的铰链。封闭板可以包括多个整体形成的间隔件元件，用于相对于板条展开机构定位封闭板。另外，一种去除飞机机翼组件中的检修面板的方法。

8. 发明授权

US09027890B2 Translating cable device sealing 有权
标题翻译：翻译电缆设备密封
公开(公告)号：US09027890B2
公开(公告)日：2015-05-12
申请号：US13714701
申请日：2012-12-14
申请人： Airbus Operations Limited
发明人： James Wilson , Paul Hadley , Alexandru Teodoru
IPC分类号： B64C13/30 , B64C9/22 , B64D15/12
CPC分类号： B64C13/30 , B64C9/22 , B64D15/12 , Y02T50/32 , Y02T50/44
摘要： An aircraft wing assembly, comprising a wing having a fixed leading edge, a slat mounted for movement between a retracted position and an extended position with respect to the fixed leading edge, and a translating cable device for electrically connecting the slat to the wing and having a strut coupled at one end to the slat, the fixed leading edge having an aperture to accommodate the strut, and a seal assembly for sealing between the strut and the aperture.
摘要翻译：一种飞机机翼组件，包括具有固定前缘的机翼，安装成相对于固定前缘在缩回位置和延伸位置之间运动的板条;以及平移电缆装置，用于将板条电连接到机翼并具有在一端连接到板条的支柱，固定的前缘具有用于容纳支柱的孔，以及用于密封支柱和孔之间的密封组件。

9. 发明申请

US20150030380A1 FASTENER RECEPTACLE STRIP 审中-公开
标题翻译：紧固件接头条
公开(公告)号：US20150030380A1
公开(公告)日：2015-01-29
申请号：US14373108
申请日：2013-01-11
申请人： AIRBUS OPERATIONS LIMITED
发明人： James Wilson , Paul Hadley , John Gleave
IPC分类号： F16B11/00 , B64C3/14 , B64C1/12
CPC分类号： F16B11/00 , B64C1/12 , B64C3/14 , F16B5/02 , F16B11/006 , Y10T29/49947 , Y10T403/472
摘要： A structural assembly comprising a first component having a ramped surface, and a fastener assembly for fastening the first component to a second component, the fastener assembly including a receptacle strip of resiliently deformable material attached to the ramped surface of the first component so as to assume the contour of the ramped surface, and a plurality of fastener receptacles attached to the receptacle strip for receiving respective fasteners. Also, a method of fastening a first component to a second component using the fastener assembly.
摘要翻译：一种包括具有斜坡表面的第一部件和用于将第一部件紧固到第二部件的紧固件组件的结构组件，所述紧固件组件包括附接到第一部件的倾斜表面的弹性可变形材料的容置条，以便呈现倾斜表面的轮廓，以及附接到接收器条的多个紧固件插座，用于接收相应的紧固件。而且，使用紧固件组件将第一部件紧固到第二部件的方法。

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