发明名称 Method, system and appartus for assembling a composite wing skin with stiffeners
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.
申请公布号 GB201602830(D0) 申请公布日期 2016.04.06
申请号 GB20160002830 申请日期 2016.02.18
申请人 BOEING COMPANY, THE 发明人
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