发明名称 Aircraft`s lockbolt for joining layers of e.g. airfoil, has elastic clamping element adapted for clamping lockbolt inserted into through-hole so that lockbolt is fastened in through-hole due to effect achieved with element
摘要 <p>The lockbolt has a bolt shaft (5) protruding from a bolt head (4), and a tear-off shaft (6) extending from the bolt head in the form of an extension of the bolt shaft and connected to the bolt shaft at a preset breaking point. The tear-off shaft includes an elastic clamping element (8) that is adapted for clamping the lockbolt that is inserted into a through-hole so that the lockbolt is fastened in the through-hole due to clamping effect achieved with the element. The clamping element is shaped in the form of a ring that surrounds the tear-off shaft circumferentially. An independent claim is also included for a method of producing a lockbolt connection.</p>
申请公布号 DE102005044824(A1) 申请公布日期 2007.03.29
申请号 DE20051044824 申请日期 2005.09.20
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 OTTEN, JUERGEN;OTTEN, MATTHIAS
分类号 F16B19/06 主分类号 F16B19/06
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