发明名称 |
Method for making a laminated structure and aeroplane provided with such a structure |
摘要 |
<p>The process involves presenting a panel and a plate (3) in stack, and piercing the stack to form a fixation hole. A fixing rod (8) is inserted into the fixation hole. A negative clearance between diameters of the fixation hole and the rod is created during the piercing process. The rod is inserted over the panel and drawn in a direction of a reacting plate while assembling the rod onto the hole. An independent claim is also included for an aircraft including a laminated structure.</p> |
申请公布号 |
EP1537993(A2) |
申请公布日期 |
2005.06.08 |
申请号 |
EP20040300814 |
申请日期 |
2004.11.25 |
申请人 |
AIRBUS FRANCE |
发明人 |
GUITTARD, DOMINIQUE;CABANAC, JEAN-PIERRE;ROGER, JANY |
分类号 |
F16B5/04;B32B37/00;B64C1/00;B64C1/26;F16B4/00;F16B5/02;(IPC1-7):B32B31/00 |
主分类号 |
F16B5/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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