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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.

3. 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

4. 发明专利

GB2417228A Aircraft wing 未知
公开(公告)号：GB2417228A
公开(公告)日：2006-02-22
申请号：GB0418487
申请日：2004-08-18
申请人： AIRBUS UK LTD
发明人： NEALE LEE ROBERT , QUAYLE ALAN , WOOD ERIC STEPHEN
IPC分类号： B64C3/26 , B64C1/00 , B64C3/00 , B64C3/18 , B64C3/38 , B64C7/00 , B64C11/24 , B64C27/46
摘要： An aircraft wing (1) that may be used in large transport aircraft comprises: (i) a first wing portion (2) that, in use, forms an inner portion of an aircraft wing, and is attached to (ii) a readily replaceable second wing portion (3) comprising a wingtip. The second wing portion (3) may be readily replaceable by a third wing portion comprising a wingtip, the third wing portion having a different functionality from the second wing portion (3).

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