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
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