Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners

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. 本发明公开了种用于形成复合机翼蒙皮的夹具装置以及相关系统和方法，其包括提供具有工作表面的框架。多个引导块耦接于框架的工作表面。所述多个引导块中的每个引导块均具有垂直于框架的工作表面定向的第引导表面以及大致平行于框架的工作表面定向的第二引导表面。多个夹持块中的每个夹持块均能移动地耦接于所述多个引导块中的个引导块。所述多个夹持块中的每个夹持块均具有夹持表面，夹持表面垂直于框架的工作表面定向，并且处于面向相邻的引导块的第引导