首页> 外国专利> Composite panel for e.g. fixed-wing aircraft for ballistic protection against surface-to-air missiles, has splinter protective layer integrated in panel, arranged between core layer and cover layer and firmly connected with cover layer

Composite panel for e.g. fixed-wing aircraft for ballistic protection against surface-to-air missiles, has splinter protective layer integrated in panel, arranged between core layer and cover layer and firmly connected with cover layer

机译:复合面板例如固定翼飞机,用于防空对地导弹的弹道保护,在面板上集成了碎片保护层,布置在核心层和覆盖层之间,并与覆盖层牢固连接

摘要

The panel (10) has a core layer (11) made of a honeycomb structure that is arranged between cover layers (12a, 12b) and directly connected with one of the cover layers. A splinter protective layer (13) is integrated in the panel, arranged between the core layer and the other cover layer and firmly connected with the latter cover layer. The protective layer is formed from aramide or ultra high molecular weight polyethylene material. The cover layers have a glass fiber laminate, a carbon fiber laminate, an aramide layer, a ceramic layer or a sheet metal. An independent claim is also included for a method for manufacturing a composite panel.
机译:面板(10)具有由蜂窝结构制成的芯层(11),该芯层布置在覆盖层(12a,12b)之间并且直接与覆盖层之一连接。碎片保护层(13)集成在面板中,布置在芯层和另一个覆盖层之间并与后者覆盖层牢固连接。保护层由芳族聚酰胺或超高分子量聚乙烯材料形成。覆盖层具有玻璃纤维层压板,碳纤维层压板,芳族聚酰胺层,陶瓷层或金属板。还包括用于制造复合板的方法的独立权利要求。

著录项

  • 公开/公告号DE102011008574A1

    专利类型

  • 公开/公告日2012-04-12

    原文格式PDF

  • 申请/专利权人 EC TECHNIK GMBH;

    申请/专利号DE20111008574

  • 发明设计人 ALTER ROLF MATTHIAS;WALTER JUERGEN DR.;

    申请日2011-01-14

  • 分类号B64C1/12;B32B3/12;B32B7/02;

  • 国家 DE

  • 入库时间 2022-08-21 17:05:02

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