发明名称 A method for the manufacture of a component by composite fibre construction
摘要 One or more layers of fiber material (5) are braided or wound around a two part tool core. One part (3) of the core is then removed and the wound fiber structure(6) remaining on the other half is compressed to create a preform (7). The preform is placed in a resin transfer molding tool, impregnated with resin and cured. The core half remaining in the molded fiber reinforced plastic (FRP) component is then removed.
申请公布号 AU2003200918(B2) 申请公布日期 2007.09.13
申请号 AU20030200918 申请日期 2003.03.07
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 TIM LEERAAR;JURGEN FILSINGER;MARTIN STAUB;ANDREAS GESSLER
分类号 B64C1/00;B29C39/10;B29C70/34;B29C70/48;B29D99/00;B29K105/08;B29L31/30;B64C9/02 主分类号 B64C1/00
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