发明名称 COMPOSITE AIRCRAFT JOINT
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.
申请公布号 CA2719174(A1) 申请公布日期 2009.10.01
申请号 CA20092719174 申请日期 2009.03.12
申请人 AIRBUS UK LIMITED 发明人 FLOOD, JOHN;HADLEY, PAUL;QUAYLE, ALAN
分类号 B64C3/26 主分类号 B64C3/26
代理机构 代理人
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