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二维慢烤模型点火位置及其温度的理论推演

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为理论分析凝聚炸药慢速烤燃过程,并为慢速烤燃点火点位置研究奠定理论基础。根据炸药的热传导理论方程,利用叠加原理和分离变量法,将炸药非反应性热传导项与自热反应热传导项拆分,推导得到凝聚炸药二维慢速烤燃模型的温度分布解析解。计算并分析了自热反应温度场随时间和炸药尺寸的变化规律。根据慢烤试验结果,对理论计算得出的点火点位置、点火温度及时间进行了验证。研究结果表明:理论确定的点火时间、点火点位置与试验测量的点火时间、点火点位置相符。炸药自热反应最高温度所在位置随其尺寸的增加,由中心移动至边缘角落。随着试验时间的增加,自热反应温度分布趋于稳定。就尺寸为φ76×190 mm的RDX炸药而言,发生点火时自热反应温度分布与点火前80000 s时的自热反应温度分布一致。
Theoretical Deduction of Ignition Position and Temperature of Two-dimensional Slow Cook-off Model
According to the theoretical equation of heat conduction of explosives, the non-reactive heat conduction term of explosives is separated from the self-heating reaction heat conduction term by using the superposition principle and the separation variable method, which lays a theoretical foundation for the theoretical analysis of slow cook-off process of condensed explosives and the study on the ignition point of slow cook-off. Therefore the analytical solution of temperature distribution for two-dimensional slow cook-off model of condensed explosives is derived. The variation of the temperature field of self-heating reaction with time and explosive size is calculated and analyzed. The ignition position, ignition temperature and ignition time calculated theoretically are verified by the results of slow cook-off test. The results show that the ignition time and ignition position determined by theory are consistent with those measured by experiment. With the increase of the size, the position of the highest temperature of self-heating reaction of explosive moves from the center to the edge corner. With the increase of test time, the temperature distribution of self-heating reaction tends to be stable. For the RDX explosive with size of φ76 mm × 190 mm, the self-heating reaction temperature distribution at the ignition time is consistent with the self-heating reaction temperature distribution at 80000 s before ignition.

ammunitionslow cook-offignition positionheat conductionanalytical solution

张坤、智小琦、肖游、王帅、罗锐恒、张姚瑶、黄云伟

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中北大学 机电工程学院, 山西 太原030051

中国兵器装备集团自动化研究所有限公司 智能制造事业部,四川 绵阳621000

湖北航天化学技术研究所 航天化学动力技术重点实验室, 湖北 襄阳441003

弹药 慢速烤燃 点火点位置 热传导 解析解

山西省基础研究计划

20210302124340

2024

兵工学报
中国兵工学会

兵工学报

CSTPCD北大核心
影响因子:0.735
ISSN:1000-1093
年,卷(期):2024.45(5)
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