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    Hybrid joining method for lap joints
    7.
    发明授权
    Hybrid joining method for lap joints 有权
    搭接接头的混合接合方法

    公开(公告)号：US08932418B2

    公开(公告)日：2015-01-13

    申请号：US12316473

    申请日：2008-12-12

    申请人： Joerg Jendrny

    发明人： Joerg Jendrny

    IPC分类号： B32B7/08 ,  B29C65/00 ,  B32B37/00 ,  B32B38/04 ,  B32B38/14 ,  B29C65/48 ,  B32B3/00 ,  B21J15/02 ,  B21J15/14 ,  F16B5/04 ,  F16B11/00

    CPC分类号： B32B3/00 ,  B21J15/02 ,  B21J15/14 ,  B21J15/147 ,  F16B5/04 ,  F16B11/006 ,  Y10T156/1057 ,  Y10T428/12389 ,  Y10T428/24479 ,  Y10T428/24612

    摘要： The invention relates to a method of producing an overlapping hybrid connection between two or more components. A hybrid connection in the meaning of the invention is characterized by adhesively bonding and producing mechanical spot joint connections between two joining parts, the adhesive layer being arranged in the region of the mechanical joint connections. The method according to the invention is carried out in the following method steps: purposefully removing material from one or more of the components or purposefully applying material to one or more of the components in the region of the lap joint to be produced to form one or more projections, applying adhesive to one or more of the components in the region of the lap joint to be produced, overlapping the components, pressing the components together in the region of the lap joint to press the projections against the overlapping component(s) and producing one or more mechanical spot joint connections on the projections in the overlap region. The method according to the invention enables a desired uniform adhesive material thickness to be obtained reliably by using the projection as spacers and also enables a mechanical spot joint connection to be produced without curing the adhesive. The invention further relates to a component comprising projections for obtaining a defined adhesive layer thickness and the use of the method and the component in an aircraft.

    摘要翻译： 本发明涉及一种在两个或多个组件之间产生重叠混合连接的方法。 本发明意义上的混合连接的特征在于在两个连接部分之间粘合并产生机械点接头连接，所述粘合剂层布置在机械接头连接的区域中。 根据本发明的方法通过以下方法步骤进行：有目的地从一个或多个部件移除材料或有目的地将材料施加到待生产的搭接接头区域中的一个或多个部件以形成一个或多个 更多的突起，将粘合剂施加到要生产的搭接接头区域中的一个或多个部件，与部件重叠，在搭接部分的区域中将部件压在一起以将突起压靠在重叠部件上， 在重叠区域上的突起上产生一个或多个机械点接头连接。 根据本发明的方法能够通过使用突起作为间隔物可靠地获得所需的均匀粘合剂材料厚度，并且还能够在不固化粘合剂的情况下制造机械点接头连接。 本发明还涉及一种包括用于获得限定的粘合剂层厚度的凸起的部件以及该飞机中该方法和部件的使用。

    Method for assembling composite hardware, and riveting member enabling implementation thereof
    9.
    发明授权
    Method for assembling composite hardware, and riveting member enabling implementation thereof 有权
    用于组装复合硬件的方法，以及能够实现其的铆接构件

    公开(公告)号：US08668420B2

    公开(公告)日：2014-03-11

    申请号：US12935310

    申请日：2009-03-19

    申请人： Pierre Auriol

    发明人： Pierre Auriol

    IPC分类号： F16B13/06

    CPC分类号： F16B19/1081 ,  B21J15/147 ,  F16B5/04

    摘要： The invention relates to a method for assembling parts (P1 and P2) in composite hardware by means of a riveting member (R), and is notable in that it comprises: using a bushing (200), the hollow core (230) of which has two different sections (231 and 232); using an insert (100) having no functional axial bearing surface for the radial swelling of the bushing (200) in the through-hole (T), but the diameter (D3) of which is capable of enabling the housing thereof, with no change in shape, in the first section (231) of the hollow core (230), and is also capable of enabling the forcible housing thereof in the second section (232); axially feeding the insert (100) into the bushing (200) such that the latter radially swells inside the through-hole (T) up to the small section (232) thereof and such that the recess well-defined by said small section is occupied by said insert (100); and ensuring, by means of a rivet set (400), the pressure on the first section (231) of the bushing (200) by the end that changes shape to ensure the bending thereof by radial centrifugal extension.

    摘要翻译： 本发明涉及一种通过铆接构件（R）在复合材料硬件中组装零件（P1和P2）的方法，其特征在于它包括：使用衬套（200），其中空芯（230） 有两个不同的部分（231和232）; 使用不具有用于衬套（200）在通孔（T）中的径向膨胀的功能性轴向表面的插入件（100），但是其直径（D3）能够使其壳体不变化 在中空芯（230）的第一部分（231）中，并且还能够使其在第二部分（232）中的强制外壳; 将插入件（100）轴向地馈送到衬套（200）中，使得后者在通孔（T）的内部径向膨胀直到其小部分（232），并且使得由所述小部分明确限定的凹部被占据 通过所述插入件（100）; 以及通过铆钉组（400）确保衬套（200）的第一部分（231）上的压力通过改变形状的端部，以通过径向离心延伸来确保其弯曲。