Method, system and apparatus for assembling a composite wing skin with stiffeners
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United States of America Patent
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Mar 13, 2018
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app pub date -
Feb 23, 2015
filing date -
Feb 23, 2015
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Abstract
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.
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