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SEPARATED FRAGMENTATION-DEMOLITION HEAD PART OF PROJECTILE

机译:分离的碎片-弹药头部

摘要

FIELD: rocket equipment.;SUBSTANCE: invention relates to the field of rocket equipment and can be used in development of jet projectiles with separated head parts of fragmentation-demolition action. Proposed device comprises case with fairing, combat compartment with explosive charge and ready fragments, as well as separation, stabilization and detonation systems, gas-dynamically interconnected by means of central gas duct equipped with head chamber to accommodate command initiation device. Combat compartment has block of ready fragmentation sleeves as means of destruction. They are arranged on cylindrical part of housing. At the same time the combat compartment is equipped with the anticipatory device made in the form of a hollow conical skirt, which thrusts interacting with the bottom of the compartment and with the head chamber made in the form of a cup. Bottom part of the cup is rigidly attached to the central gas line. Front part of the cartridge is attached to the fairing. Detonation system is made in the form of two cascades. They include the main and duplicating detonating circuits closing in detonators of the front and rear belts of the detonation, equipped with receiving detonator blocks located in front disk of the gas line. Main detonating chains thermodynamically connected to each other by means of detonation cords laid in longitudinal slots on the outer diameter of the gas duct are additionally equipped with transverse and reverse detonation cords. They are arranged on outer diameter of gas duct and have on each detonation section total length equal to half of length of main detonation cord, providing possibility of transfer of initiating pulse from receiving detonator grain to bottom detonator. In the longitudinal groove at the place of passage of the main detonation cord through the area of the front detonator arrangement, there is a radial recess filled with an inert compound. In the front part of the hollow skirt a strong crosswise bridge is installed, covering a zone of effective power action on the front belt of detonation at operation of receiving detonation blocks.;EFFECT: high reliability of the device owing to high reliability of outputting the igniting and detonation pulse and protecting the device units from abnormal operation.;1 cl, 2 dwg
机译:技术领域本发明涉及火箭设备领域,可用于具有破碎-拆卸作用的分离头部的喷气弹的开发。所提出的装置包括带有整流罩的箱子,带有炸药和现成碎片的战斗舱以及分离,稳定和引爆系统,它们通过配备有头部腔室的中央气体导管进行气动力互连,以容纳命令启动装置。战斗隔间有块准备好的碎片套筒,可作为破坏手段。它们布置在外壳的圆柱部分上。同时,作战舱装备有以中空圆锥形裙部形式制成的预期装置,该预期装置与舱室的底部以及以杯状形式制成的顶舱相互作用。杯子的底部牢固地连接到中央气体管线。滤芯的前部连接到整流罩。爆炸系统以两个级联的形式制成。它们包括在起爆前后皮带的起爆器中闭合的主起爆电路和重复起爆电路,并在气体管线的前盘上装有接收起爆器块。借助于放置在燃气管道外径上的纵向槽中的导爆索在热力学上相互连接的主导爆索还配备了横向和反导爆破索。它们布置在导气管的外径上,并且在每个爆震段上的总长度等于主引爆绳长度的一半,从而提供了将引发脉冲从接收雷管晶粒传递到底部雷管的可能性。在主导爆索通过前部雷管装置区域的位置的纵向凹槽中,有一个径向凹槽,里面充满了惰性化合物。在空心裙的前部安装了坚固的横向桥,覆盖了在接收爆轰块操作时爆轰前带上有效动力作用的区域。;效果:由于输出高可靠性而使设备具有很高的可靠性点火和爆震脉冲并保护设备单元免受异常操作的影响; 1 cl,2 dwg

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