首页> 外国专利> Aircraft hinge, particularly aircraft seat hinge for use in aircraft seat, has amplifying unit, enclosure unit and hinge unit, which are provided in common to aircraft component that is connected to base element in hinged state

Aircraft hinge, particularly aircraft seat hinge for use in aircraft seat, has amplifying unit, enclosure unit and hinge unit, which are provided in common to aircraft component that is connected to base element in hinged state

机译:飞机铰链,特别是用于飞机座椅的飞机座椅铰链,具有放大单元,封闭单元和铰链单元,所述放大单元,封闭单元和铰链单元共同提供给以铰链状态连接到基础元件的飞机部件

摘要

The aircraft hinge (10) comprises an amplifying unit (12) for amplification of an aircraft component (14). An enclosure unit (16) enclosures the amplifying unit. A hinge unit (18) that is arranged in a fastened state is directly in contact with a base element (20). The amplifying unit, the enclosure unit and the hinge unit are provided in common to the aircraft component that is connected to the base element in a hinged state. The hinge unit is designed to be pushed in a mounting on the base element. The amplifying unit engages partially through the enclosure unit in an attached state. An independent claim is included for a method for mounting an aircraft hinge.
机译:飞机铰链(10)包括用于放大飞机部件(14)的放大单元(12)。封闭单元(16)封闭放大单元。以紧固状态布置的铰链单元(18)直接与基础元件(20)接触。放大单元,封闭单元和铰链单元被共同设置为以铰链状态连接到基础元件的飞行器部件。铰链单元设计为可推入底座上的安装座中。放大单元在附接状态下部分地通过外壳单元接合。包括用于安装飞机铰链的方法的独立权利要求。

著录项

  • 公开/公告号DE102013102060A1

    专利类型

  • 公开/公告日2014-09-04

    原文格式PDF

  • 申请/专利权人 RECARO AIRCRAFT SEATING GMBH & CO. KG;

    申请/专利号DE201310102060

  • 发明设计人 KIESER OLAF;

    申请日2013-03-01

  • 分类号B64D11/06;E05D9;

  • 国家 DE

  • 入库时间 2022-08-21 15:37:21

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