发明名称 Dual skinned structures
摘要 A dual skinned structure comprises a first skin 12, a second skin 14 and an intermediate structure 16. The intermediate structure comprises a plurality of first contact portions 18 connected to an interior surface of the first skin, a plurality of second portions 20 connected to an interior surface of the second skin and a plurality of interconnecting portions 22 integral to the first and second contact portions and extending between ones of the first and second contact portions to form an internal structure alternating between the interior surfaces of the first and second skins. The first and second skins and the intermediate structure may comprise fibre reinforced composite material. In forming the structure use may be made of releasable mandrels and deltoid fillers. The dual skinned structure may have an aerofoil section such as winglets.
申请公布号 GB2475523(A) 申请公布日期 2011.05.25
申请号 GB20090020391 申请日期 2009.11.20
申请人 GKN AEROSPACE SERVICES LIMITED 发明人 CHRIS GEAR;EDDIE JONES;JUSTIN ELLIOTT;DALE EDMUNDS;GIOVANNI MARENGO
分类号 B32B3/28;B32B37/10;B64C3/20 主分类号 B32B3/28
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