发明名称 Systems and methods for forming composite materials
摘要 SYSTEMS AND METHODS FOR FORMING COMPOSITE MATERIALS A composite membrane assembly (900) may include a plurality of stacked composite plies (500). Each composite ply (500) may include a main body (501) of reinforced fibres (502) connected together with a resin. The main body (501) may include a base (504) connected to an opposed boundary surface (506) through opposed ends (508 and 510) and opposed sides (511). At least one non-orthogonal cut (514) is formed through a thickness of the main body (501) from the base (504) to the boundary surface (506). The non-orthogonal cut(s) (514) is staggered with respect to at least one other non-orthogonal cut (514) of an adjacent composite ply (500) so that the non-orthogonal cut(s) (514) does not form a contiguous linear cut (514) with the other non orthogonal cut(s) (514) of the adjacent composite ply (500). 908 914 900 1012 1008 1008 1008 1006 1006 1006 1006 1010 1100--, 1102 FIr. 11A
申请公布号 AU2016202221(A1) 申请公布日期 2016.12.01
申请号 AU20160202221 申请日期 2016.04.11
申请人 The Boeing Company 发明人 Kismarton, Max
分类号 B64C1/12;B32B3/10;B32B17/04;B32B27/04;B32B38/04;B64C1/06 主分类号 B64C1/12
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