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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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