冲击起爆单元中飞片参数的数值模拟

Simulate and Calculate of Flyer Parameters in Impact Detonation Unit

  • 摘要: 为了研究飞片参数对飞片冲击起爆的影响规律,采用Lee-Tarver点火增长模型对不同材料飞片的厚度、直径冲击起爆HNS-Ⅳ炸药进行数值模拟研究,分析不同飞片参数对起爆阈值的影响.结果表明,对于直径为Φ1.57 mm×25 μm的飞片,聚酰亚胺的冲击起爆动能低于玻璃和陶瓷材料,是目前冲击起爆装置低能化设计较为理想的材料.飞片参数研究表明,在25~145 μm厚度范围内,冲击起爆炸药的飞片阈值速度随着飞片厚度的不断增大而降低,当飞片的厚度大于145 μm,飞片冲击起爆HNS-Ⅳ炸药的阈值速度无明显变化.当飞片直径为1.02~1.57 mm,飞片阈值速度随着飞片直径的增加逐渐降低,当飞片直径超过1.57 mm时,飞片冲击起爆HNS-Ⅳ炸药的阈值速度趋于一个定值.

     

    Abstract: To study the influence of flyer parameters on shock and detonation, Lee-Tarver ignition and growth model was adopted to simulate the process that flyers shock and detonate HNS-IV explosive, where the flyer was made by different materials,thickness and diameter. The influence of different flyer parameters on detonation threshold was analyzed. The results show that the shock initiation kinetic energy of polyimide was lower than those of glass and ceramic, which makes it an ideal material for lower-energy of shock initiation devices. The detonation threshold velocity decreases as the flyer thickness increases in a range from 25 to 145 μm, but when the flyer thickness exceeds 145 μm, the threshold velocity has no obvious change. In a diameter range from 1.02 to 1.57 mm, the threshold velocity gradually decreases with the increase of flyer diameter, the threshold velocity tends to be a constant value when the flyer diameter exceeds 1.57 mm.

     

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