发明名称 Method of forming a Laminar composite structure
摘要 A stack of composite layers 1-9 is assembled on a layup tool 10, each composite layer comprising a fibre-reinforced matrix material. The composite layers include an inner composite layer 1 and an outer composite layer 9. During assembly of the stack, a series of spacers 20, 22, 23 are placed in a selected part of the stack, each spacer comprising a spacer matrix material. Each spacer is sandwiched between a respective adjacent pair of the composite layers. The selected part of the stack forms a bulge, and the outer composite layer has a greater path length at the bulge than the inner composite layer. After assembly of the stack, a bend is formed in the stack with the outer composite layer towards an outside of the bend and the inner composite layer towards an inside of the bend, the bend in the stack coinciding with the bulge. During or after formation of the bend in the stack, excess matrix material in liquid form flows out of the bulge.
申请公布号 GB2533369(A) 申请公布日期 2016.06.22
申请号 GB20140022583 申请日期 2014.12.18
申请人 Airbus Operations Limited 发明人 Vimal Jaiswal
分类号 B29C70/30;B29C53/02;B29C53/04;B29C70/02 主分类号 B29C70/30
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