发明名称 Methodfor reducing ply wrinkling of composite laminates during forming
摘要 Ply wrinkling during hot drape forming of a composite laminate is reduced at corner radii. A tensioning material placed over an uncured composite laminate charge maintains a compressive force on the laminate charge as the charge is formed over a tool.
申请公布号 US9573301(B2) 申请公布日期 2017.02.21
申请号 US201313847046 申请日期 2013.03.19
申请人 The BOEING COMPANY 发明人 Kline William Thomas;Harris Christopher Gary
分类号 B29C43/32;B29C70/34;B29C70/54;B29C70/56 主分类号 B29C43/32
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method of reducing ply wrinkling during hot drape forming of a composite laminate, comprising: placing a tensioning material over an uncured composite laminate charge; hot drape forming the laminate charge over a forming tool; using the tensioning material to compress the laminate charge as the laminate charge is being formed over the forming tool; and removing the tensioning material after the laminate charge has been formed.
地址 Chicago IL US