公开(公告)号：EP1010615A3

公开(公告)日：2002-05-22

申请号：EP99500147.6

申请日：1999-08-17

申请人： CONSTRUCCIONES AERONAUTICAS, S.A.

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

IPC分类号： B64C1/00 ,  F16B1/00

CPC分类号： B64C1/06 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10S29/003 ,  Y10T29/49904 ,  Y10T29/49906 ,  Y10T29/49947 ,  Y10T29/49948

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° 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.

公开(公告)号：EP1010615A2

公开(公告)日：2000-06-21

申请号：EP99500147.6

申请日：1999-08-17

申请人： CONSTRUCCIONES AERONAUTICAS, S.A.

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

IPC分类号： B64C1/00 ,  F16B1/00

CPC分类号： B64C1/06 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10S29/003 ,  Y10T29/49904 ,  Y10T29/49906 ,  Y10T29/49947 ,  Y10T29/49948

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° 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.

摘要翻译： 一种用于制作可拆卸和/或固定牵引 - 压缩耦合过程被施加到复合材料，其中复合材料的基本层叠体（1）被折叠至少一次，以获得至少一个裙部（2）在角度形成紧密 与层叠体的其余90°; 通过使用裙部和所述层叠体的其余部分，一组分配板之间的过渡半径（5,6）施加在基本层压以稳定裙和产生一个均匀的负荷分布，各组分配裙部形成孔 - 板和引入的牵引螺栓（4），其具有在所述孔中的初始预张力，因此获得的部件之间的连接将被接合。 本发明适用于飞机的空气动力结构。