- 专利标题: PANEL STRUCTURE FOR AN AIRCRAFT AND MANUFACTURING METHOD THEREOF
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申请号: US15803559申请日: 2017-11-03
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公开(公告)号: US20180127081A1公开(公告)日: 2018-05-10
- 发明人: Javier TORAL VÁZQUEZ , Esteban MARTINO GONZALEZ , Diego FOLCH CORTES , Pablo GOYA ABAURREA , Vasillis VOTSIOS , Michel FOUINNETAU , Sylvain ROUMEGAS
- 申请人: Airbus Operations, S.L. , Airbus Operations (S.A.S.)
- 优先权: EP16382507.8 20161104
- 主分类号: B64C1/12
- IPC分类号: B64C1/12 ; B32B5/02 ; B32B5/18 ; B64C5/02 ; B64F5/10
摘要:
A panel structure for an aircraft with at least one composite layer, and at least one net-shaped layer attached to the composite layer, wherein the net-shaped layer has a material suitable to improve the impact resistance of the panel structure. The net-shaped layer can be used to attach two composite layers. Alternatively, the net-shaped layer can be attached to a surface of one composite layer. In this last case, the net-shaped layer may be joined to a laminate sheet material and filled with a foam material. An impact reinforced panel structure is disclosed capable of withstanding any impact, such as a blade release, or a bird strike, without substantially modifying the manufacturing process.
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