发明名称 Composite part forming system
摘要 A system and method for forming a composite part. The method comprises positioning a prepreg material relative to a composite forming tool 302. The composite forming tool comprises a frame (308, fig 4) associated with a shaping system (310, fig 3), a base 312 comprising at least one mould, and the shaping system associated with the frame and configured to move relative to the frame, the base, and the prepreg material. The method also lowers the shaping system of the composite forming tool towards the prepreg material. The method applies pressure to the prepreg material with a centerline presser 326 of the shaping system. The method also applies a force to the prepreg material using a number of compliant elongate members 334, 337 of the shaping system to uniformly apply the prepreg material to the at least one mold of the base of the composite forming tool. Forming surfaces 402, 404 may be moved along the surface 602 of the mould.
申请公布号 GB2531644(A) 申请公布日期 2016.04.27
申请号 GB20150015641 申请日期 2015.09.03
申请人 The Boeing Company 发明人 Silas Lawton Studley;Matthew Ray DesJardien;James N. Buttrick
分类号 B29C70/38;B29C70/30;B29C70/54 主分类号 B29C70/38
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