Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners
    3.
    发明申请
    Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners 有权
    用于加固复合翼型皮肤的方法,系统和装置

    公开(公告)号:US20160244185A1

    公开(公告)日:2016-08-25

    申请号:US14629131

    申请日:2015-02-23

    IPC分类号: B64F5/00

    摘要: A jig apparatus and associated systems and methods for forming a composite wing skin is presented, including providing a frame with a working surface. A plurality of indexing blocks are coupled to the working surface of the frame. Each of the plurality of indexing blocks has a first indexing surface oriented perpendicular to the working surface of the frame and a second indexing surface oriented approximately parallel to the working surface of the frame. A plurality of clamping blocks are also each moveably coupled to one of the plurality of indexing blocks. Each of the plurality of clamping blocks has a clamping surface oriented perpendicular to the working surface of the frame and in facing relation to the first indexing surface of an adjacent indexing block thereby defining a plurality of channels.

    摘要翻译: 提出了一种用于形成复合翼面的夹具装置和相关系统和方法,包括为框架提供工作表面。 多个分度块联接到框架的工作表面。 多个分度块中的每一个具有垂直于框架的工作表面定向的第一分度表面和与框架的工作表面大致平行取向的第二分度表面。 多个夹紧块也可移动地联接到多个分度块之一。 多个夹紧块中的每一个具有夹紧表面,该夹紧表面垂直于框架的工作表面定向,并且与相邻的分度块的第一分度表面相对,从而限定多个通道。