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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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