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. The composite forming tool comprises a frame associated with a shaping system, a base comprising at least one mold, 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 of the shaping system. The method also applies a force to the prepreg material using a number of compliant elongate members of the shaping system to uniformly apply the prepreg material to the at least one mold of the base of the composite forming tool.
申请公布号 US2016089841(A1) 申请公布日期 2016.03.31
申请号 US201414500667 申请日期 2014.09.29
申请人 The Boeing Company 发明人 Studley Silas Lawton;DesJardien Matthew Ray;Buttrick James N.
分类号 B29C70/38 主分类号 B29C70/38
代理机构 代理人
主权项 1. A method for forming a composite part comprising: positioning a prepreg material relative to a composite forming tool, the composite forming tool comprising a frame associated with a shaping system; a base comprising at least one mold; and the shaping system associated with the frame and configured to move relative to the frame, the base, and the prepreg material; lowering the shaping system of the composite forming tool towards the prepreg material; applying pressure to the prepreg material with a centerline presser of the shaping system; and applying a force to the prepreg material using a number of compliant elongate members of the shaping system to uniformly apply the prepreg material to the at least one mold of the base of the composite forming tool.
地址 Chicago IL US