发明名称 Method for joining sandwich truss core panels and composite structures produced therefrom
摘要 Fluted core sandwich panels are joined together to form a composite structure. Variations in panel ends are accommodated by a core stiffener insert installed in a joint between ends of the panels.
申请公布号 US8834667(B2) 申请公布日期 2014.09.16
申请号 US201012907329 申请日期 2010.10.19
申请人 The Boeing Company 发明人 McCarville Douglas A.;Guzman Juan C.;Hand Michael Leslie
分类号 B29C65/48;B32B3/20;B29C65/00;B29C65/50;B29L31/30;B29L31/00;B64C1/00;B64C1/06 主分类号 B29C65/48
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method of fabricating a composite structure, comprising: forming first and second panels each having a fluted core and an end, the first and second panels each having a core sandwiched between first and second facesheets, the core comprising a support between the first and second facesheets, the fluted cores being mismatched at the first and second panel ends, creating mismatched cores, the first and the second panels each comprising a truss panel having a fluted core, the fluted core being a series of hollow isosceles trapezoidal flutes with inclined side walls extending traverse to a plane of the first and second face sheets; altering the first and second panel ends to match-up the mismatched cores, so as to form altered panel ends, the altering including removing at least a portion of the flutes between the first and second facesheets; installing a composite core stiffener insert between the altered panel ends, the composite core stiffener comprising a plurality of fibers that form a web and a set of flanges, the set of flanges adhered to the first panel and the second panel, the web comprising a substantially straight portion extending between the first panel and the second panel such that the set of flanges contact an inner surface of the first panel and an inner surface of the second panel; and joining the altered panel ends together at a joint.
地址 Chicago IL US