Sympathetic detonation of booster pipe with JO-9C charge
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摘要: 为了研究冲击波作用下引信传爆装置的响应规律，进行了以主发炸药为RDX-8701、被发装置为聚奥-9C（JO-9C）装药的传爆管（含导爆药柱）的殉爆实验。通过观测残留传爆药、壳体和见证块变形，判断传爆管的爆炸程度，分析了殉爆过程中JO-9C爆轰波的成长历程及传播规律。采用AUTODYN软件建立了殉爆实验有限元模型，计算模型中主要考虑了主发炸药产生的爆炸冲击波对传爆管的冲击响应。基于流固耦合方法，通过调整距离模拟计算得到了传爆管的临界殉爆距离和殉爆安全距离。结果表明，传爆管上端的侧角受到爆炸冲击后产生的爆轰波沿斜下方传播，使传爆药柱完全爆轰，并引起导爆药柱发生殉爆；数值模拟结果显示，JO-9C装药的传爆管临界殉爆距离为5.7 mm，殉爆安全距离为8.8 mm。Abstract: In the present study we carried out sympathetic detonation experiments, using RDX-8701 as donor and booster pipe and using JO-9C charge as acceptor explosive, to study the response of the fuse explosion device under shock wave. By observing the remainder of the JO-9C explosive, the deformation of the witness and the steel shell, and judging the explosive reaction state, we analyzed the histories in the sympathetic detonation reaction of the acceptor, and established the calculation model of the sympathetic detonation using AUTODYN. The calculated results of the model included the effects of the shock waves produced by the donor that acted on the booster pipe. Based on the fluid-solid coupling method, we also obtained the critical and safety distance of the sympathetic detonation through numerical simulation by adjusting experimental distance. The results show that the detonation wave propagated down firstly along the slope direction of the booster charge, thereby leading to the detonation of the booster charge, and then detonated the detonator explosive. According to the numerical simulation results, the critical and the safety distances of the sympathetic detonation were 5.7 mm and 8.8 mm respectively.
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Key words:
- JO-9C charge /
- booster pipe /
- sympathetic detonation /
- ignition and growth model
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图 8 距离5 mm时传爆管殉爆压力云图
Figure 8. Pressure contours of sympathetic detonation for booster pipe at 5 mm
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[1] LU J P, LOCHERT I J, KENNEDY D L, et al. Simulation of sympathetic reaction tests for PBXN-109[C]//Proceedings of 13th International Symposium on Detonation. New York, USA, 2006: 1338-1349. [2] FISHER S, BAKER E L, WELLS L, et al. XM982 excalibur sympathetic detonation modeling and experimentation[C]//Insensitive Munitions and Energetic Materials Technology Symposium. New York, USA, 2006: 937-951. [3] MOSTAFA H E, MEKKY W F, El-DAKHAKHNI W W. Sympathetic detonation wave attenuation using polyurethane foam[J]. Journal of Materials in Civil Engineering, 2013, 26(8):04014046. doi: 10.1061/%28ASCE%29MT.1943-5533.0000934 [4] 周保顺, 王少龙, 徐明利, 等.非均质炸药殉爆试验数值模拟[J].弹箭与制导学报, 2009, 29(5):145-148. http://d.old.wanfangdata.com.cn/Periodical/djyzdxb200905039ZHOU Baoshun, WANG Shaolong, XU Mingli, et al. Numerical simulation of sympathetic detonation of heterogeneous condensed explosives[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2009, 29(5):145-148. http://d.old.wanfangdata.com.cn/Periodical/djyzdxb200905039 [5] 陈朗, 王晨, 鲁建英, 等.炸药殉爆实验和数值模拟[J].北京理工大学学报, 2009, 29(6):497-501. http://d.old.wanfangdata.com.cn/Periodical/bzycj201002007CHEN Lang, WANG Chen, LU Jianying, et al. Experiment simulation of sympathetic detonation tests[J]. Transactions of Beijing Institute of Technology, 2009, 29(6):497-501. http://d.old.wanfangdata.com.cn/Periodical/bzycj201002007 [6] 姜颖资, 王伟力, 黄雪峰, 等.带壳炸药在高速运动炸药作用下殉爆效应研究[J].工程爆破, 2014, 20(3):1-4. http://www.cqvip.com/QK/98385X/201403/661615887.htmlJIANG Yingzi, WANG Weili, HUANG Xuefeng, et al. Research on the sympathetic detonation effect of shelled explosive by high-speed movement explosive[J]. Engineering Blasting, 2014, 20(3):1-4. http://www.cqvip.com/QK/98385X/201403/661615887.html [7] 王晨, 伍俊英, 陈朗, 等.壳装炸药殉爆实验和数值模拟[J].爆炸与冲击, 2010, 30(2):152-158. doi: 10.11883/1001-1455(2010)02-0152-07WANG Chen, WU Junying, CHEN Lang, et al. Experiments and numerical simulations of sympathetic detonation of explosives in shell[J]. Explosion and Shock Waves, 2010, 30(2):152-158. doi: 10.11883/1001-1455(2010)02-0152-07 [8] 路胜卓, 罗卫华, 陈卫东, 等.壳装高能固体推进剂的殉爆实验与数值模拟[J].哈尔滨工程大学学报, 2014, 35(12):1507-1512. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgcdxxb201412010LU Shengzhuo, LUO Weihua, CHEN Weidong, et al. Experiments and numerical simulations of sympathetic detonation of high-energy solid propellant in shell[J]. Journal of Harbin Engineering University, 2014, 35(12):1507-1512. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgcdxxb201412010 [9] 陶为俊, 浣石. RDX-8701炸药二维冲击起爆状态的研究[C]//第八届全国爆炸力学学术会议. 江西吉安, 2007: 58-63. [10] VANDERSALL K S, TARVER C M, GARCIA F, et al. On the low pressure shock initiation of octahydro-1, 3, 5, 7-tetranitro-1, 3, 5, 7-tetrazocine based plastic bonded explosives[J]. Journal of Applied Physics, 2010, 107(9):094906. doi: 10.1063/1.3407570 [11] 李晓杰, 姜力, 赵铮, 等.高速旋转弹头侵彻运动金属薄板的数值模拟[J].爆炸与冲击, 2008, 28(1):57-61. doi: 10.11883/1001-1455(2008)01-0057-05LI Xiaojie, JIANG Li, ZHAO Zheng, et al. Numerical study on penetration of a high-speed-rotating bullet into the moving sheet-metal plate[J]. Explosion and Shock Waves, 2008, 28(1):57-61. doi: 10.11883/1001-1455(2008)01-0057-05 -
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