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Triggering arrangement for pyrotechnical warning rocket - has stumbling string actuating hinged flap with triggering string of rocket

机译:烟火预警火箭的触发装置-具有绊脚致动铰链襟翼和火箭触发弦

摘要

The triggering mechanism is used for pyrotechnical warning devices, for smoke, signalling or illuminating flare rockets. It is also used for flare burning at stationary positions. The triggering arrangement socket is connected with a housing accommodating the pyrotechnical device. The rear end has triggering strings. The triggering arrangement is used in a warning rocket system staggered when the enemy bypasses the warning rocket arrangement in the ground. The socket has spring loaded hinge flap and the triggering string is fixed on it. The flap is moved from one position into another. The flap is fixed by a bracket into a first position and this bracket carries a wire which actuates the system when an enemy stumbles on the string.
机译:触发机构用于烟火警报装置,烟雾,信号或照明弹火箭。它也用于固定位置的火炬燃烧。触发装置插座与容纳烟火装置的壳体连接。后端具有触发弦。当敌人绕过地面的警告火箭装置时,触发装置交错布置在警告火箭系统中。插座具有弹簧加载的铰链翻板,触发绳固定在其上。襟翼从一个位置移动到另一位置。襟翼通过托架固定在第一位置,并且该托架上装有一根钢丝,当敌人跌倒在弦上时,该钢丝可启动系统。

著录项

  • 公开/公告号CH592863A5

    专利类型

  • 公开/公告日1977-11-15

    原文格式PDF

  • 申请/专利权人 BUEHRLE AG (WERKZEUGMASCHINENFABRIK OERLIKON);

    申请/专利号CH19750007233

  • 发明设计人

    申请日1975-06-05

  • 分类号F41H11/06;F41H13/00;

  • 国家 CH

  • 入库时间 2022-08-22 22:11:08

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