首页> 外国专利> Reinforcement element for shell component of aircraft or spacecraft, has shape stiffener part, which has light metal material, and base part, which has high-corrosion resistant material

Reinforcement element for shell component of aircraft or spacecraft, has shape stiffener part, which has light metal material, and base part, which has high-corrosion resistant material

机译:用于飞机或航天器的壳体部件的增强元件,具有由轻金属材料制成的形状加强件和具有高耐腐蚀材料的底座部分。

摘要

The reinforcement element (100) has a shape stiffener part, which has a light metal material, and a base part, which has a high-corrosion resistant material. The base part is formed as a profile part, particularly as a L or a T-section part. The high corrosion-resistant material is formed as a metal material, particularly titanium or a titanium alloy. The light metal material is formed as aluminum or an aluminum alloy. An independent claim is also included for a method for the production of a reinforcement element.
机译:加强元件(100)具有形状加强件和基础部分,该形状加强件具有轻金属材料,该基础部分具有高耐腐蚀材料。基础部分形成为轮廓部分,特别是L形或T形部分。高耐腐蚀材料形成为金属材料,特别是钛或钛合金。轻金属材料形成为铝或铝合金。还包括一种用于制造增强元件的方法的独立权利要求。

著录项

  • 公开/公告号DE102006051462A1

    专利类型

  • 公开/公告日2008-05-15

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20061051462

  • 发明设计人 SCHROEER THORSTEN;ROMING THORSTEN;

    申请日2006-10-31

  • 分类号B64C1/00;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:40

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