发明名称 BENDS IN COMPOSITE PANELS
摘要 PROBLEM TO BE SOLVED: To provide a method and apparatus for forming a bend in a composite panel.SOLUTION: A method for forming a bend in a composite panel 300 comprises forming a slot 400 having a curved flange 408 in the composite panel, inserting a sheet 602 into the curved flange, and bending the composite panel 300 with the slot 400 and the sheet 602 within the curved flange 408 about a longitudinal axis 508 of the slot 400 to form the bend. The curved flange 408 has a bend allowance width larger than a bend slot width.
申请公布号 JP2015074229(A) 申请公布日期 2015.04.20
申请号 JP20140200909 申请日期 2014.09.30
申请人 BOEING CO 发明人 STEPHEN M YOUNG;CARL AARON DAVISON;WILL GEORGE PFEFFER
分类号 B29C53/02;B29C70/06;B64C1/00;B64D11/00 主分类号 B29C53/02
代理机构 代理人
主权项
地址