首页> 外国专利> Arrangement for connecting of a conductive state and an externally guided tube of a protection tube envelope, which is a component of a lightning protection system for, with an aircraft structure

Arrangement for connecting of a conductive state and an externally guided tube of a protection tube envelope, which is a component of a lightning protection system for, with an aircraft structure

机译:用于将导电状态与保护管外壳的外部引导管连接的装置,该保护管外壳是用于飞机结构的防雷系统的部件

摘要

The arrangement is as far as possible to connect a flexible, metallic protective tubes on, the insulated electrical conductors or cables wrapping and in particular in aircraft as a protection against electromagnetic influences or electrical dangers, such as overvoltages and to lightning strikes, are used, with a suitable structure. An efficient they contribute to the prevention of electrical dangers by lightning, in electrical systems. Dollars a the arrangement has mainly a first electrically conductive tube piece, which is designed conically, in the interior of bundled insulated electrical lines run, and a second electrically conducting pipe portion, which is designed to be conical on the inside, whereby the externally guided tube encased the first pipe section and in the second pipe section, and wherein between the conical ends of the pipe pieces the end of the externally guided tube is clamped. The two pipe sections have in each case on one side a flange, which together with a metal by means of screws are connected to the partition wall of the aircraft. If the end face of the inner side of these flanges are removed, touches the flangeless end of the second pipe section the end face of the inner side of a first flange of the first pipe section and, via the second pipe section is a metal the form of clamp is fastened, wherein the two flanges, wherein the shape of a clamp is equipped with a protective conductor connection. Otherwise, the ..
机译:该装置应尽可能将柔性金属保护管连接在绝缘的导体或电缆上,尤其是在飞机上,以防止电磁干扰或电气危险(例如过电压和雷击),具有合适的结构。它们有效地有助于防止电气系统中的雷电电气危险。美元的装置主要具有在成束的绝缘电线的内部呈圆锥形设计的第一导电管件,以及在内部呈圆锥形设计的第二导电管件,从而从外部引导在第一管段中和在第二管段中都包裹有管,并且其中,在管件的圆锥形端部之间夹紧了外部引导管的端部。两个管段分别在一侧具有凸缘,该凸缘与金属一起通过螺钉与飞机的分隔壁连接。如果这些法兰内侧的端面被去除,则接触第二管段的无法兰端,即第一管段的第一法兰内侧的端面,并且通过第二管段是金属固定夹的形式,其中两个凸缘,其中夹的形状配备有保护性导体连接。否则,..

著录项

  • 公开/公告号DE4322232C2

    专利类型

  • 公开/公告日2002-04-11

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH 21129 HAMBURG DE;

    申请/专利号DE19934322232

  • 发明设计人 KIRMA SAFA 22880 WEDEL DE;

    申请日1993-07-03

  • 分类号B64D45/02;H02G3/06;H05K9/00;H02G13/00;

  • 国家 DE

  • 入库时间 2022-08-22 00:26:03

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