发明名称 Method of locally reinforcing a composite element and reinforced aircraft wing structure central box section
摘要 A method of locally reinforcing an element made of composite material having a longest dimension, such as a composite beam, which is intended to bear multidirectional forces. To do that, at least one metal reinforcing piece is secured to the composite element, at a point on the composite element that is intended to bear vertical forces. The same may be done at each of those points on the composite element that is intended to bear vertical forces.
申请公布号 US2009121082(A1) 申请公布日期 2009.05.14
申请号 US20080244847 申请日期 2008.10.03
申请人 AIRBUS FRANCE 发明人 GODENZI CHRISTIAN;TANGHE FREDERIC;GAY STEPHANE;PRIOUL NICOLAS
分类号 B64C3/18;B21D53/92 主分类号 B64C3/18
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