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.