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电爆驱动高速飞片冲击下HNS小尺寸装药的起爆与爆轰特性

杨坤1,刘丹阳1,2*,蹇雨桐1,王菁1,刘昌华2,何亚新2,顾玲芝2,陈朗1   

  1. 1. 北京理工大学 爆炸科学与安全防护全国重点试验室,北京 100081;2. 四川华川工业股份有限公司,四川 成都 610105
  • 收稿日期:2025-02-06 修回日期:2025-04-18
  • 基金资助:
    国家自然科学基金项目(12302432);中国博士后科学基金资助项目(2024M754097)

Initiation and Detonation Characteristics of HNS Micro Explosive Charges under the Impact of High-speed Flyers Driven by Electric Explosion

YANG Kun1,LIU Danyang1,2*, JIAN Yutong1, WANG Jing1, LIU Changhua2, HE Yaxin2, GU Lingzhi2, CHEN Lang1   

  1. 1. State Key Laboratory of Explosion Science and Safety Protection, Beijing Institute of Technology, Beijing 100081, China; 2. Sichuan Huachuan Industrial Co., Ltd., Chengdu 610105, Sichuan, China
  • Received:2025-02-06 Revised:2025-04-18

摘要: 爆炸箔起爆技术具有高安全性和高可靠性,且便于微型化、集成化,契合精密微起爆系统需求。为深入认识爆炸箔起爆系统小尺寸装药引发与爆轰输出特性,搭建了电爆炸驱动飞片特性同步观测系统,以及飞片冲击起爆小尺寸装药爆轰的炸药与窗口界面粒子速度测试系统,研究了飞片速度、形态特性及其冲击作用下HNS-IV小尺寸装药的起爆与爆轰反应行为。研究表明:起爆电压与飞片出膛速度呈正相关,起爆电压900 V~1500 V时,飞片出膛速度为2000 m/s ~4200 m/s。高强度冲击下HNS-IV基炸药爆轰成长距离短,在3455 m/s飞片作用下,2.14 mm内可成长为稳定爆轰,爆轰波结构分析表明其反应速率快,爆轰反应时间小于27 ns,反应区宽度仅0.13 mm。3 mm直径小尺寸装药条件并未显著影响HNS-IV炸药的主要爆轰反应,但反应后期出现能量快速衰减现象。基于试验标定炸药爆轰反应速率方程,进一步仿真研究了装药尺寸对能量输出的影响,结果显示与增加装药直径相比,增大药柱厚度更能有效提升装药端面的能量输出。

关键词: 电爆炸驱动飞片, HNS炸药, 爆轰反应区, 冲击起爆, 爆轰反应速率方程

Abstract: Exploding foil initiator (EFI) represents a promising initiation technology for meeting the high requirements of miniaturized and intelligent weapon systems for initiation capability. To gain an in-depth understanding of the initiation and detonation output characteristics of an exploding foil initiator system, a synchronized observation system for the electrical explosion-driven flyer characteristics of metal bridge foils was established, along with a particle velocity measurement system at the explosive-window interface for flyer-impact-initiated small-scale explosive detonation. The study investigated the flyer velocity, morphological characteristics, and the initiation and detonation reaction behavior of small-scale HNS-IV explosive under flyer impact. The results show that the flyer velocity is positively correlated with the initiation voltage. When the initiation voltage ranged from 900 to 1500 V, flyer velocity exiting the acceleration chamber was measured at 2000 to 4200 m/s. HNS-IV-based explosives demonstrated a short detonation growth distance; for instance, stable detonation was achieved within just 2.14 mm when impacted by a 3455 m/s flyer. Further analysis of the detonation wave structure indicated that HNS-IV has a fast detonation reaction rate, with a reaction time of less than 27 ns and a reaction zone width of only 0.13 mm. Under the condition of a 3 mm diameter micro-charge, the main detonation reaction of HNS-IV explosives remained largely unaffected, but a rapid energy decay was observed in the late stage of the reaction. The detonation reaction rate model was first calibrated by experimental results and then simulations were conducted to study the effect of charge size on the energy output. The results showed that increasing the charge thickness is more effective in enhancing energy output at the end of charge than increasing the charge diameter.

Key words: electric explosion-driven flyer, HNS, detonation reaction zone, shock initiation, detonation reaction rate equation

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