发明名称 Composite structural member
摘要 A method of manufacturing a composite structural member including laying up a stack of fiber reinforced laminate plies, wherein at least one of the plies is laid up as discrete first and second ply portions, and the fibers of the second portion have a different characteristic from those of the first portion. Also, a composite structural member manufactured according to the method.
申请公布号 GB201005308(D0) 申请公布日期 2010.05.12
申请号 GB20100005308 申请日期 2010.03.30
申请人 AIRBUS OPERATIONS LTD 发明人
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