发明名称 METHOD FOR FABRICATING CURVED THERMOPLASTIC COMPOSITE PARTS
摘要 A fabrication method of forming curved thermoplastic composite laminate parts with tailored and varying thickness in a continuous process. Automated equipment or hand lay-up are used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
申请公布号 WO2008073164(A2) 申请公布日期 2008.06.19
申请号 WO2007US18611 申请日期 2007.08.22
申请人 THE BOEING COMPANY;RUBIN, ALEXANDER M.;FOX, JAMES R.;WILKERSON, RANDALL D. 发明人 RUBIN, ALEXANDER M.;FOX, JAMES R.;WILKERSON, RANDALL D.
分类号 B29D99/00 主分类号 B29D99/00
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