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带空穴柱形装药壳体破片爆炸驱动特性

王辰旭1,张甲浩1,蔡轶强1,周晟1,龚杰2,陈鹏万3,余庆波1*()   

  1. (1. 北京理工大学 机电学院,北京 100081;2. 湖南云箭集团有限公司,湖南 长沙 410137;3. 北京理工大学 材料学院,北京 100081)
  • 收稿日期:2024-12-04 修回日期:2025-07-16
  • 通讯作者: *邮箱:yuqb@bit.edu.cn
  • 基金资助:
    国家自然科学基金项目(12132003)

Explosive Driving Characteristics of Shell Fragments Driven by Cylindrical Charge with Cavity

WANG Chenxu1, ZHANG Jiahao1, CAI Yiqiang1, ZHOU Sheng1, GONG Jie2, CHEN Pengwan3, YU Qingbo1*()   

  1. (1. School of Mechatronics Engineering, Beijing Institute of Technology, Beijing 100081, China; 2. Hunan Vanguard Group Company Limited, Changsha 410137, Hunan, China; 3. School of Materials Science & Engineering, Beijing Institute of Technology, Beijing 100081, China)
  • Received:2024-12-04 Revised:2025-07-16

摘要: 为研究带空穴柱形装药壳体破片爆炸驱动特性,揭示空穴装药结构对壳体破片初速的影响机理,利用数值仿真研究不同空穴锥角下壳体破片爆炸驱动过程和初速分布规律。通过分析稀疏波传播路径、速度损失系数和破片加速过程,拟合了壳体破片初速沿轴向分布函数,计算结果与数值仿真结果之间的相对误差不超过15 %。研究结果表明:稀疏波的提前产生和横截面装填比的降低是破片初速下降的主要因素;非起爆端破片初速随空穴锥角的减小和空穴锥顶高度的增大而减小;非起爆端反射稀疏波为近似平面波且与空穴表面呈一定角度,稀疏波到达壳体的时间与壳体的轴向位置呈线性正相关关系;横截面装填比与k呈二次函数关系,k为该横截面距非起爆端的长度和锥顶高度之间的比值,速度损失系数随比值k的减小呈指数形式衰减;研究成果可对破甲杀伤复合战斗部和带空穴结构的可变形破片战斗部的总体结构设计、材料选型及结构优化提供有益参考。

关键词: 破片战斗部, 空穴装药, 数值分析, 初速分布

Abstract: In order to study the explosion driving characteristics of cylindrical charge shell fragments with cavities and reveal the influence mechanism of cavity charge structure on the initial velocity of shell fragments, numerical simulation was carried out on the explosion driving process and initial velocity distribution of shell fragments under different cavity cone angles. By analyzing the sparse wave propagation path, velocity loss coefficient and fragment acceleration process, the initial velocity distribution function of the shell fragment along the axial direction is fitted. The error between the calculation results and the numerical simulation results is less than 15 %. The results show that the earlier generation of rarefaction wave and the decrease of cross-section ratio of mass of charge to shell are the main factors for the decrease of initial velocity of fragments. The initial velocity of the fragments near the non-detonation end decreases with the decrease of the cavity cone angle and the increase of the cavity cone top height. The reflected rarefaction wave from the non-detonation end is an plane wave approximately and has a certain angle with the cavity surface. The instant when rarefaction wave reaches shell is linearly positively correlated with the axial position of the shell. The cross-section ratio of mass of charge to shell has a quadratic function relationship with the ratio k between the distance between the cross section and the non-initiating end and the height of the cavity cone top. The velocity loss coefficient decays exponentially with the ratio k decreasing. The research can provide a useful reference for the overall structural design, material selection and structural optimization of the anti-armour and anti-personnel composite warhead and the deformable fragment warhead with cavity charge structure.

Key words: fragment warhead, shaped charge, numerical analysis, velocity distribution

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