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For a fuze of a tube that is with a twist of the tubular end projectile

机译:用于引爆管形末端弹丸的引信

摘要

The igniter comprises a disk-shaped element ( 15 ) with a central portion ( 16 ) and a boundary portion ( 17 ) surrounding it for interrupting and/or releasing an ignition chain ( 13 a , 13 b) of the igniter. Only the central portion interrupts the chain of ignition and is supported by a holding device ( 19 ). A collecting space is provided around the holding device which, seen in the direction of flight of the projectile, is located below the boundary portion ( 17 ). The central portion ( 16 ) and the boundary portion ( 17 ) are connected with each other by means of a rated breaking point ( 18 ). Upon the initial acceleration of the projectile the boundary portion ( 17 ) is sheared off from the central portion ( 16 ) and received in the collecting space ( 21 ), whereupon the central portion ( 16 ) is also subsequently removed from the ignition chain ( 13 a , 13 b) by the twist of the projectile.
机译:点火器包括具有中心部分(16)和围绕它的边界部分(17)的盘形元件(15),用于中断和/或释放点火器的点火链(13a,13b)。仅中央部分中断点火链并且由保持装置(19)支撑。在保持装置周围设置有收集空间,从弹丸的飞行方向看,收集空间位于边界部分(17)的下方。中心部分(16)和边界部分(17)通过额定断裂点(18)彼此连接。当弹丸开始加速时,边界部分(17)从中心部​​分(16)上切下并被容纳在收集空间(21)中,随后中心部分(16)也随后从点火链(13)上移开。 a,13 b)通过弹丸的扭曲。

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