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PROTECTIVE COVER OF MISSILE, MISSILE HAVING THE SAME AND IMPACT RELIEF METHOD OF MISSILE

机译:导弹的保护罩,具有相同的导弹和减轻撞击的方法

摘要

PURPOSE: A protection cover of a guided missile and a shock relieving method of the guided missile are provided to protect machines or electric devices of a guided missile with added reliability because a protection cover fractures to buffer an impact when the guided missile flies into water. CONSTITUTION: A protection cover of a guided missile(100) comprises a shell assembly(130), a shock absorbing ball(150), and a closing plate(120). The shell assembly comprises a plurality of supporters. One end of the shell assembly forms a closed plane and the other end of the shell assembly is formed into a shape of an opened hollow cylinder. The shock absorbing ball is housed inside the shell assembly. The closing plate is joined to the closed plane of the shell assembly and blocks the inflow of fluid.
机译:目的:提供一种制导导弹的保护罩和一种制导导弹的减震方法,以增加可靠性,保护制导导弹的机器或电气设备,因为当制导导弹飞入水中时,该保护罩会破裂以缓冲冲击。组成:制导导弹(100)的保护罩,包括一个外壳组件(130),一个减震球(150)和一个封闭板(120)。壳体组件包括多个支撑件。壳体组件的一端形成封闭平面,壳体组件的另一端形成为敞开的空心圆柱体的形状。减震球容纳在壳体组件内部。封闭板连接至壳体组件的封闭平面,并阻止流体流入。

著录项

  • 公开/公告号KR20120056123A

    专利类型

  • 公开/公告日2012-06-01

    原文格式PDF

  • 申请/专利权人 AGENCY FOR DEFENSE DEVELOPMENT;

    申请/专利号KR20100117683

  • 发明设计人 KIM IN HACK;KIM HYUNG RYUL;DOK KO WOOK;

    申请日2010-11-24

  • 分类号F42B15/20;F42B12/02;F42B17;F42B12/76;

  • 国家 KR

  • 入库时间 2022-08-21 17:09:57

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