发明名称 Method and Apparatus for Reducing Ply Wrinkling of Composite Laminates During Forming
摘要 Ply wrinkling during hot drape forming of a composite laminate is reduced at outside corner radii of a forming tool. First and second tensioning materials placed between a composite laminate charge and the forming tool maintain the laminate charge in tension at the radius corners as the charge is formed down over corner radii.
申请公布号 US2015183171(A1) 申请公布日期 2015.07.02
申请号 US201514660668 申请日期 2015.03.17
申请人 The Boeing Company 发明人 Kline William Thomas;Harris Christopher Gary;Hopkins Andrew M.;Sutkus, JR. Donald John
分类号 B29C70/34 主分类号 B29C70/34
代理机构 代理人
主权项 1. A method of hot drape forming a composite laminate charge on a forming tool that reduces ply wrinkling, comprising: placing a first tensioning material on the forming tool; placing the first tensioning material in tension; placing a second tensioning material on the first tensioning material; placing a composite laminate charge on the forming tool overlying the first tensioning material and the second tensioning material; and hot drape forming the laminate charge over the forming tool, including transferring the tension in the first tensioning material through the second tensioning material to the laminate charge.
地址 Chicago IL US