发明名称 SYSTEMS AND METHODS FOR FORMING COMPOSITE MATERIALS
摘要 A composite membrane assembly may include a plurality of stacked composite plies. Each composite ply may include a main body of reinforced fibers connected together with a resin. The main body may include a base connected to an opposed boundary surface through opposed ends and opposed sides. At least one non-orthogonal cut is formed through a thickness of the main body from the base to the boundary surface. The non-orthogonal cut(s) is staggered with respect to at least one other non-orthogonal cut of an adjacent composite ply so that the non-orthogonal cut(s) does not form a contiguous linear cut with the other non-orthogonal cut(s) of the adjacent composite ply.
申请公布号 CA2926631(A1) 申请公布日期 2016.11.14
申请号 CA20162926631 申请日期 2016.04.07
申请人 THE BOEING COMPANY 发明人 KISMARTON, MAX
分类号 B32B3/14;B32B5/26;B32B5/28;B32B27/04;B32B38/00 主分类号 B32B3/14
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