发明名称 RESISTANCE WELDING OF THERMOPLASTICS IN AEROSPACE STRUCTURE
摘要 We form joints between the rib (104) and spar (102) webs in a composite wingbox by welding the webs using heat along the bondline produced by connecting tabs on a susceptor (1) to a current source. Rib-spar web joints are difficult to create inductively because they fall in a plane where it is difficult to use fixed or moving induction coils to produce the current and resulting heating.
申请公布号 EP0830283(A1) 申请公布日期 1998.03.25
申请号 EP19960909794 申请日期 1996.03.19
申请人 THE BOEING COMPANY 发明人 MATSEN, MARC, R.;MCCARVILLE, DOUGLAS, A.;STEPAN, MICHAEL, M.
分类号 B29C65/00;B29C65/34;B29C65/36;B64C1/00;B64C3/18 主分类号 B29C65/00
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