发明名称 Joining curved composite sandwich panels
摘要 A curved composite structure, comprises at least two curved composite panel segments joined together. Each of the panel segments includes a fluted core sandwiched between first and second facesheets. A layer of adhesive is used to rigidly bond the panel segments together.
申请公布号 US8815038(B2) 申请公布日期 2014.08.26
申请号 US200912398138 申请日期 2009.03.04
申请人 The Boeing Company 发明人 McCarville Douglas A.;Guzman Juan C.
分类号 B29C53/36 主分类号 B29C53/36
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method comprising: providing a first curved composite panel, wherein the first curved composite panel comprises a first fluted core having a first plurality of flutes covered by a first face sheet and a second face sheet opposite the first face sheet, wherein a first edge of a first flute of the first plurality of flutes extends outwardly from the first face sheet and the second face sheet, and wherein the first edge is relative to a first axis of the first flute; providing a second curved composite panel, wherein the second curved composite panel comprises a second fluted core having a second plurality of flutes covered by a third face sheet and a fourth face sheet opposite the third face sheet, wherein the third face sheet and the fourth face sheet extend outwardly past a second edge of a second flute of the second plurality of flutes, wherein the second edge is relative to a second axis of the second flute, and wherein a space is defined between the third face sheet and the fourth face sheet where the third face sheet and the fourth face sheet extend outwardly past the second edge; forming an overlapping joint between the first curved composite panel and the second curved composite panel by inserting the first flute into the space; inserting a mandrel into the first flute; and curing the overlapping joint.
地址 Chicago IL US