发明名称 Method of manufacturing a composite element
摘要 A method of manufacturing a composite element. A stack of plies is assembled on a lay-up table, each ply comprising a plurality of reinforcement elements such as dry-fibers. A first part of the stack of plies is bound to form a partially bound stack of plies, a second part of the stack of plies remaining unbound. The partially bound stack of plies is press-formed in a mold cavity between a pair of mold tools to form a shaped pre-form, plies in the second part of the stack sliding against each other during the press-forming. A liquid matrix material is injected into the shaped pre-form in the mold cavity and subsequently cured.
申请公布号 US8911650(B2) 申请公布日期 2014.12.16
申请号 US200913054185 申请日期 2009.07.27
申请人 Airbus Operations Limited 发明人 Topping Simon W;Edwards Martin;Kallinen Risto;Haack Nils
分类号 B29C70/48;B29C70/54;B29L31/00;B29B11/16 主分类号 B29C70/48
代理机构 Lowe Hauptman & Ham, LLP 代理人 Lowe Hauptman & Ham, LLP
主权项 1. A method of manufacturing a composite element, the method comprising: a. assembling a stack of plies on a lay-up table, each ply comprising a plurality of reinforcement elements; b. binding together a first part of the stack of plies to form a partially bound stack of plies, a second part of the stack of plies remaining unbound, wherein the binding comprises applying pressure to the first part of the stack of plies; and thereafter c. press-forming the partially bound stack of plies in a mould cavity between a pair of mould tools to form a shaped pre-form, plies in the second part of the stack sliding against each other during the press-forming; d. injecting a liquid matrix material into the shaped pre-form in the mould cavity; and e. curing the liquid matrix material.
地址 Bristol GB