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1. 发明申请

WO2009118548A3 COMPOSITE AIRCRAFT JOINT 审中-公开
标题翻译：复合飞机接头
公开(公告)号：WO2009118548A3
公开(公告)日：2009-12-03
申请号：PCT/GB2009050242
申请日：2009-03-12
申请人： AIRBUS UK LTD , FLOOD JOHN , HADLEY PAUL , QUAYLE ALAN
发明人： FLOOD JOHN , HADLEY PAUL , QUAYLE ALAN
IPC分类号： B64C3/26
CPC分类号： B64C1/12 , B29C65/564 , B29C65/76 , B29C66/43441 , B29C66/721 , B29L2031/3076 , Y10T156/10
摘要： The present invention relates to a joint between a laminar composite cover (12) and a second cover (15) (which may or may not be also formed from a composite material). The invention also relates to a method of manufacturing such a joint and a method of manufacturing a composite cover suitable for use in such a joint. The laminar composite cover (12) comprises a stack of layers, substantially all of the layers being shaped to form a joggle, each joggle comprising a first portion, a second portion where the layer extends substantially parallel with the first portion, and a ramp (33) between the first and second portions where the layer extends at an angle to the first and second portions, the number of layers being substantially the same on both sides of the ramp. The second cover (15) partially overlaps with the composite cover, and a clamp or fastener (31) holds the covers together where they overlap. The covers have external sides which are substantially aligned with each other so as to form a smooth aerodynamic surface.
摘要翻译：本发明涉及层状复合盖（12）和第二盖（15）之间的接头（其可以或可以不由复合材料形成）。本发明还涉及这种接头的制造方法和制造适用于这种接头的复合罩的方法。层状复合材料盖（12）包括一叠层，基本上所有的层都被成形为形成一个弯曲部，每个弯曲部包括第一部分，第二部分，其中该层基本上平行于第一部分延伸，以及斜面在第一和第二部分之间，其中层与第一和第二部分成一定角度延伸，层数在斜坡两侧基本相同。第二盖（15）部分地与复合盖重叠，并且夹具或紧固件（31）将盖保持在重叠的位置。盖具有彼此基本对准的外侧，以便形成平滑的空气动力学表面。

2. 发明申请

WO2010116168A2 COUPLING ASSEMBLY 审中-公开
标题翻译：联轴器总成
公开(公告)号：WO2010116168A2
公开(公告)日：2010-10-14
申请号：PCT/GB2010050552
申请日：2010-03-31
申请人： AIRBUS OPERATIONS LTD , COULTER STEVEN , HADLEY PAUL , HOPKINS GERAINT
发明人： COULTER STEVEN , HADLEY PAUL , HOPKINS GERAINT
IPC分类号： B64C1/12
CPC分类号： B64C3/28 , F16B5/025 , Y10T29/49947 , Y10T403/19
摘要： A coupling assembly for joining a first component to a second component, the assembly comprising a shaft for connecting to a first component, and a bracket including a mounting plate for connecting to a second component. The bracket has a bracket arm extending from the mounting plate, and a head having a through-bore on the bracket arm. The shaft is received in the through-bore. A setting device acts between the head and the shaft for setting of the position of the shaft with respect to the head in the axial direction of the shaft. The assembly further includes one or more spherical bearing surfaces, which permit self-alignment of the setting device to accommodate tilting of the shaft with respect to the head about a central point in two orthogonal directions. Also, a joint comprising a first component joined to a second component by one or more of the coupling assemblies. Also, a method of forming a joint using one or more of the coupling assemblies.
摘要翻译：一种用于将第一部件连接到第二部件的联接组件，所述组件包括用于连接到第一部件的轴和包括用于连接到第二部件的安装板的支架。支架具有从安装板延伸的支架臂和在支架臂上具有通孔的头部。轴被容纳在通孔中。设置装置作用在头部和轴之间，用于在轴的轴向方向上相对于头部设置轴的位置。组件还包括一个或多个球面轴承表面，其允许定位装置的自对准以适应轴在两个正交方向上围绕中心点相对于头部的倾斜。而且，包括由一个或多个联接组件接合到第二部件的第一部件的接头。此外，使用一个或多个联接组件形成接头的方法。

3. 发明申请

WO2011003844A3 STRINGER 审中-公开
公开(公告)号：WO2011003844A3
公开(公告)日：2011-06-30
申请号：PCT/EP2010059521
申请日：2010-07-05
申请人： AIRBUS OPERATIONS LTD , AIRBUS OPERATIONS GMBH , BORGHINI-LILLI MATTEO , HADLEY PAUL , PHILLIPS NATHAN
发明人： BORGHINI-LILLI MATTEO , HADLEY PAUL , PHILLIPS NATHAN
IPC分类号： B64C1/06
CPC分类号： B64C1/064 , B29C70/30 , B29D99/0014 , Y02T50/433 , Y10T156/1062 , Y10T428/24479
摘要： A laminated composite stringer having a termination at one end in its longitudinal direction, and including a laminated stack of composite structural plies, wherein internal plies in the stack are terminated consecutively towards the stringer termination to provide a taper of reducing stack thickness. Also, a composite structure comprising a panel and the stringer; and a method of manufacturing the stringer. The composite structure may be used in aircraft.
摘要翻译：一层压复合纵梁，其长度方向的一端具有终端，并且包括复合结构层的层压叠层，其中堆叠中的内层连续地朝向纵梁终端端接，以提供减小堆叠厚度的锥度。而且，一种复合结构，包括一个面板和该纵梁; 以及制造桁条的方法。复合结构可用于飞机。

4. 发明专利

CA2719174A1 COMPOSITE AIRCRAFT JOINT 未知
公开(公告)号：CA2719174A1
公开(公告)日：2009-10-01
申请号：CA2719174
申请日：2009-03-12
申请人： AIRBUS UK LTD
发明人： FLOOD JOHN , HADLEY PAUL , QUAYLE ALAN
IPC分类号： B64C3/26
摘要： The present invention relates to a joint between a laminar composite cover (12) and a second cover (15) (which may or may not be also formed from a composite material). The invention also relates to a method of manufacturing such a joint and a method of manufacturing a composite cover suitable for use in such a joint. The laminar composite cover (12) comprises a stack of layers, substantially all of the layers being shaped to form a joggle, each joggle comprising a first portion, a second portion where the layer extends substantially parallel with the first portion, and a ramp (33) between the first and second portions where the layer extends at an angle to the first and second portions, the number of layers being substantially the same on both sides of the ramp. The second cover (15) partially overlaps with the composite cover, and a clamp or fastener (31) holds the covers together where they overlap. The covers have external sides which are substantially aligned with each other so as to form a smooth aerodynamic surface.

5. 发明专利

BRPI0909003A2 junta compósita para aeronave 未知
公开(公告)号：BRPI0909003A2
公开(公告)日：2016-05-03
申请号：BRPI0909003
申请日：2009-03-12
申请人： AIRBUS UK LTD
发明人： QUAYLE ALAN , FLOOD JOHN , HADLEY PAUL
IPC分类号： B64C3/26

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