发明授权
EP1010615B1 A process for making a dismountable and/or fixed traction-compression joint to be applied to composite materials
有权
一种用于可拆卸的和/或固定Zugkompressionsverbindung过程中复合材料使用
- 专利标题： A process for making a dismountable and/or fixed traction-compression joint to be applied to composite materials
- 专利标题（中）： 一种用于可拆卸的和/或固定Zugkompressionsverbindung过程中复合材料使用
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申请号： EP99500147.6申请日： 1999-08-17
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公开(公告)号： EP1010615B1公开(公告)日： 2005-10-26
- 发明人: Dominguez Casado, Rafael , Perez Perez, Antonio , Huertas Garcia, Manuel , De Castro Nodal, Manuel , Cerezo Pancorbo, Carlos , Robledo Sacristan, Bonifacio , Grueso Diez, César , Redondo Vara, Enrique
- 申请人： Airbus Espana, S.L.
- 申请人地址： Avda. John Lennon, s/n 28906 Getafe (Madrid) ES
- 专利权人： Airbus Espana, S.L.
- 当前专利权人： Airbus Espana, S.L.
- 当前专利权人地址： Avda. John Lennon, s/n 28906 Getafe (Madrid) ES
- 代理机构： Elzaburu Marquez, Alberto
- 优先权： ES9802635 19981218
- 主分类号： B64C1/00
- IPC分类号： B64C1/00 ; F16B1/00
摘要：
A process for making a dismountable and/or fixed traction-compression coupling to be applied to composite materials, in which a basic laminate (1) of composite material is folded at least once to obtain at least one skirt (2) forming an angle close to 90 DEG with the rest of the laminate; by using a transition radius between the skirt and the rest of the laminate, a set of distribution plates (5, 6) is applied over the basic laminate to stabilize the skirt and produce a uniform load distribution, making holes in each set of distribution skirt-plates and introducing traction bolts (4) with an initial pretension in said holes, hence obtaining the connection between the components to be joined. The invention is applicable to the aerodynamic structures of aircraft.
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