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    • 9. 发明公开
    • AUFSCHLAGZÜNDER
    • EP1504235A1
    • 2005-02-09
    • EP02721949.2
    • 2002-05-13
    • RUAG Munition
    • KUTZLI, JörgGUENOT, Pascal
    • F42C15/295
    • F42C15/295
    • Percussion fuses of missiles must meet numerous safety requirements and must trigger ignition with minimal delay. According to the inventive method, after the launch of a missile (M), a turbine/firing pin unit (1) is unlocked behind a cap (2) comprising a central inlet (3), and the rotor disk (1a) of said unit is subjected to the dynamic pressure (S). Said dynamic pressure (S) pushes the turbine/firing pin unit (1) into a front position (II), in such a way that it can act as an impact detector. According to the inventive device, the turbine/firing pin unit (1) comprises a screw thread (1c) on its shaft and is screwed into a threaded bush ( 32), in such a way that the dynamic pressure (S) pushes the unit (1) into the front position (II), against the direction of flow. During the impact, the rear end of the unit (1) acts as a percussion needle and initiates an ignition chain.
    • 导弹的撞击保险丝必须符合多项安全要求,并且必须以最小的延迟触发点火。 根据本发明的方法,在发射导弹(M)之后,涡轮/击发销单元(1)在包括中央入口(3)的帽(2)后被解锁,并且所述转子盘 单元受到动态压力(S)。 所述动压力(S)将涡轮/撞针单元(1)推入前部位置(II),使得它可以用作冲击检测器。 根据本发明的装置,涡轮机/撞针单元(1)在其轴上包括螺纹(1c)并且以这样的方式拧入螺纹衬套(32)中,使得动压力(S)将单元 (1)逆着流动方向进入前部位置(II)。 在冲击过程中,单元(1)的后端用作冲击针并启动点火链。