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Reduced-calibre missile - has piston actuated by propellant gases and freeing driving disc spring locking catches

机译:小口径导弹-活塞由推进气体驱动并释放驱动盘式弹簧锁扣

摘要

The reduced-calibre missile has the central part enclosed by a segmented guide ring, while a driving disc is fixed to its rear end by detachable locking devices. The devices (6) are released by the effect of the propellant gases, there being inside the disc (9) a piston (11) on which these act. The missile (1) has, behind a stop ring (16), spring-loaded locking catches (6) engaging in the disc, and which are freed by the piston.
机译:减径导弹的中央部分被分段的导向环包围,而驱动盘则通过可拆卸的锁定装置固定在其后端。装置(6)在推进剂气体的作用下被释放,在盘(9)内部有活塞(11),它们作用在该活塞上。导弹(1)在止动环(16)的后面装有弹簧加载的锁止钩(6),该锁止钩(6)啮合在圆盘中,并由活塞释放。

著录项

  • 公开/公告号DE2407220A1

    专利类型

  • 公开/公告日1980-09-04

    原文格式PDF

  • 申请/专利权人 RHEINMETALL GMBH;

    申请/专利号DE19742407220

  • 发明设计人 HELLWIGROLF;KARIUSDIETMARING.;

    申请日1974-02-15

  • 分类号F42B13/16;

  • 国家 DE

  • 入库时间 2022-08-22 17:41:40

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