| 小型霍普金森杆多级电磁发射系统的优化 |
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| 引用本文： | 刘战伟,陈喜民,董杰,刘爽,谢惠民.小型霍普金森杆多级电磁发射系统的优化[J].实验力学,2015,30(1):9-16. |
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| 作者姓名： | 刘战伟 陈喜民 董杰 刘爽 谢惠民 |
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| 作者单位： | 北京理工大学 宇航学院, 北京 100081;北京理工大学 宇航学院, 北京 100081;北京理工大学 宇航学院, 北京 100081;北京理工大学 宇航学院, 北京 100081;清华大学 航空航天学院, 北京 100084 |
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| 基金项目： | 国家自然科学基金资助(NOS.11072033, 11232008, 11372037)、北京市自然基金资助(NO.3122027) |
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| 摘 要： | 根据小型霍普金森杆(Mini-SHB)对发射效率高、体积小、噪声污染小的要求及动态性能测试对高应变率的要求,本文对磁阻式小型霍普金森杆电磁发射系统进行了优化。利用电磁发射原理、电磁仿真计算和控制变量方法,对影响子弹发射速度的五个因素:电容组电容量、电路初始电压、电磁线圈匝数、线圈用漆包线直径、子弹初始位置分别进行了仿真优化。根据仿真得到的各个最优参数研制的电磁发射系统获得了单级16.16m/s、二级21m/s的最高子弹出口速度,达到了微小型试件动态性能测试对高应变率的要求。
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| 关 键 词： | 电磁发射技术 小型霍普金森杆 动态力学性能 高应变率 |
| 修稿时间： | 8/5/2014 12:00:00 AM |
The Optimization of Multistage Electromagnetic Launching System of Mini-SHB |
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| LIU Zhan-wei,CHEN Xi-min,DONG Jie,LIU Shuang and XIE Hui-min.The Optimization of Multistage Electromagnetic Launching System of Mini-SHB[J].Journal of Experimental Mechanics,2015,30(1):9-16. |
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| Authors: | LIU Zhan-wei CHEN Xi-min DONG Jie LIU Shuang and XIE Hui-min |
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| Institution: | Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;FML, Department of Engineering Mechanics, Tsinghua University, Beijing 100084, China |
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| Abstract: | According to the requirements for Mini-split Hopkinson bar (SHB), such as high launching efficiency, small size, low noise pollution and high strain rate in dynamic performance tests, the optimization of electromagnetic launching system of Mini-SHB, is presented in this paper. By using electromagnetic emission principle, electromagnetic simulation and variable control method, the simulation optimization of fives factors influencing the bullet launching velocity was carried out respectively, including capacitor bank capacity, circuit initial voltage, electromagnetic coil turns, coil wire diameter, initial position of bullet. The electromagnetic launching system developed based on each simulation optimized parameters enables the highest bullet exit velocity to reach 16.16m/s for single stage and 21m/s for two stages, respectively, which meets the requirements of high strain rate for dynamic performance test of miniature specimens. |
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| Keywords: | electromagnetic launching technique mini-split Hopkinson bar(SHB) dynamic mechanical properties high strain rate |
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