发明名称 FABRICATION PROCESS FOR THERMOPLASTIC COMPOSITE PARTS
摘要 A fabrication method of forming a thermoplastic composite laminate material with tailored and varying thickness in a continuous process. This process utilizes automated equipment or hand lay-up 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. The 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 these multiple ply stacks.
申请公布号 HK1116136(A1) 申请公布日期 2011.07.08
申请号 HK20080111471 申请日期 2008.10.16
申请人 THE BOEING COMPANY 发明人 RUBIN, ALEXANDER, M.;FOX, JAMES, R.;WILKERSON, RANDALL, D.
分类号 B29D99/00;B29C;B29D 主分类号 B29D99/00
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