|
|
Analyzing Influence of Barrel Shell on Launching Performance of Electromagnetic Rail Launcher |
Zhai Xiaofei1, Zou Kun1,2, Li Peifei1, Peng Zhiran1, LiuHua1 |
1. National Key Laboratory of Science and Technology on Vessel Integrated Power System Naval University of Engineering Wuhan 430033 China; 2. School of Electrical Engineering Southeast University Nanjing 210096 China |
|
|
Abstract As part of the electromagnetic launcher (EML), the barrel shell mainly provides preloading force for the rails to constrain the expansion and deformation of the EML, and at the same time provides support stiffness for the rail to ensure the straightness of the EML. During the launch process of the armature, the instantaneous change of rail current will induce a huge eddy current on the metal barrel shell of the EML, and the eddy current magnetic field of the shell has a certain weakening effect on the magnetic field inside the device, and will also affect the current distribution of the rails, thereby affecting the electrical features and mechanical properties of the EML, affecting the launching performance such as the exit speed of the armature. Since the shell structure and material will affect the shell eddy current, it is necessary to analyze the influence of the shell material and structure on the electromagnetic parameters of the EML and the force of the armature and rails, so as to obtain the influence law of the shell on the launching performance. Firstly, the magnetic field control equation considering the eddy current of the shell is established, and the finite element model (FEM) of three shell structures is established: the integral structure shell, the upper-lower separated structure shell and the laminated structure shell. After the speed frequency is introduced, the frequency changed current excitation is used to simulate the velocity skin effect caused by the launching of the armature in the bore, so as to obtain the inductance gradient and shell loss with frequency change curve, as well as the electric density distribution of the rails and the eddy current distribution cloud in the shell. Secondly, the simulation of electromagnetic-structural is carried out, and the stress distribution of each component of the EML is obtained. The system electrical simulation is established, and the launching simulation results of the three shell structures are compared. The results of the electromagnetic-structural simulation and system launching simulation show that the laminated structure shell has the smallest eddy current, the largest inductance gradient, the largest stress of the device components, and the highest armature exit speed, while the integral structure shell has the largest eddy current, the largest shell loss, the smallest inductance gradient, the smallest stress of the device components, and the lowest armature exit speed. Finally, the simulation and test results of the laminated structure shell EML are compared, and the error of both the armature exit speed and the current peak is less than 1%. Under the condition of satisfying the support strength of the EML, the selection of materials with high permeability and low conductivity and the design of the shell structure that suppresses eddy currents are conducive to improving the exit speed and system efficiency of the EML. In addition, reducing the eddy current of the shell is conducive to increasing the electromagnetic thrust of the armature, but it will also increase the external expansion force of the rails, which requires increasing the structural strength of the shell to provide higher preloading force, therefore, the structural design and material selection of the shell should take into account both electromagnetic properties and mechanical properties to obtain excellent launching performance.
|
|
|
|
|
|
[1] 马伟明,鲁军勇,李湘平.电磁发射超高速一体化弹丸[J].国防科技大学学报,2019,41(4):1-10. Ma Weiming,Lu Junyong,Li Xiangping.Electromagnetic launch hypervelocity integrated projectile[J].Journal of National University of Defense Technology,2019,41(4):1-10(in Chinese). [2] 王莹, 肖峰. 电炮原理[M]. 北京: 国防工业出版社, 1995 [3] 马伟明. 关于电工学科前沿技术发展的若干思考[J]. 电工技术学报, 2021, 36(22): 4627-4636. Ma Weiming.Thoughts on the Development of Frontier Technology in Electrical Engineering. Transactions of China Electrotechnical Society, 2021, 36(22): 4627-4636. [4] Weiming Ma,Junyong Lu.Tingking and study of Electromagnetic Lunch Technology[J]. IEEE Transactions on Plasma Science,2017,45(7):1071-1077.DOI:10.1109/TPS.2017.2705979. [5] 彭之然, 刘华, 汪光森, 翟小飞, 张晓. 基于多模块分时放电半解析模型的脉冲电源触发策略[J]. 电工技术学报, 2021, 36(zk1): 54-61. Peng Zhiran, Liu Hua, Wang Guangsen, Zhai Xiaofei, Zhang Xiao.Trigger Strategy of Pulsed Power Supply Based on the Semi-Analytical Model of Sequentially-Triggered Power Units. Transactions of China Electrotechnical Society, 2021, 36(zk1): 54-61. [6] Landen D, Satapathy S.Eddy current effects in the laminated containment structure of railguns[J]. IEEE Transactions on Magnetics,2007, 43(1): 150-156. [7] 林庆华,栗保明. 有限元/边界元耦合法计算电磁轨道炮三维瞬态涡流场[J]. 兵工学报,2010,34(2):217-221. LIN Qinghua, LI Baoming.Finite-element/boundary-element coupling method for 3D transient eddy current field calculation in electromagnetic railgun[J]. Acta Armamentarii, 2010, 34(2): 217-221. [8] 刘守豹, 阮江军, 黄道春,等.封装对轨道炮电感梯度的影响[J].电工电能新技术,2009,28(4):42-45+75. WAN Lei, HAO Rui-xiang,YOU Xiao-jie et.al,.Design of new plasma ignition power supply[J].Advanced Technology of Electrical Engineering and Energy,2009,28(4):42-45+75. [9] 楼宇涛,栗保明. 管身对中口径电磁轨道炮的影响分析[J].强激光与粒子束,2015,27(9):093201-1~093201-6. Lou Yutao,Li Baoming. Influence of containment for medium caliber electromagnetic railgun[J]. High Power laser and particle beams, 2015,27(9):093201-1~093201-6. [10] 楼宇涛,栗保明.电磁轨道炮封装中涡流损耗的抑制方法[J].高电压技术,2016,42(6):1935-1941. LOU Yutao, LI Baoming.Methods for Reducing the Loss Caused by the Eddy Current in Electromagnetic Railgun Shielding[J].High Voltage Engineering,2016,42(6):1935-1941. [11] 彭之然,汪光森,翟小飞,等.电磁轨道发射装置时变电感梯度建模与分析[J].电工技术学报, 2020,35(23):4843-4851. Peng Zhiran,Wang Guangsen,Zhai Xiaofei, et al.Modeling and Analysis of Time-varying Inductance Gradient for Electromagnetic Rail Launcher[J].Transactions of China Electrotechnical Society, 2020,35(23):4843-4851. [12] 李湘平, 鲁军勇, 张晓, 冯军红, 蔡喜元. 电磁发射弹丸膛口磁场分布特性分析[J]. 电工技术学报, 2021, 36(3): 525-531. Li Xiangping, Lu Junyong, Zhang Xiao, Feng Junhong, Cai Xiyuan.Analysis of Distribution Characteristics of Electromagnetic Launcher Projectile Muzzle Magnetic Field. Transactions of China Electrotechnical Society, 2021, 36(3): 525-531. [13] 林庆华,栗保明. 基于瞬态多物理场求解器的电磁轨道炮发射过程建模与仿真[J]. 兵工学报, 2020, 41(9):1697-1707. LIN Qinghua, LI Baoming.Modeling and Simulation of Electromagnetic Railgun Launching Process Based on a Transient Multi-physical Field Solver[J]. Acta Armamentarii, 2020, 41(9):1697-1707. (in Chinese) [14] Peng Z, Zhang X, Zhai X, et al.Field‐circuit coupled analysis of an electromagnetic launcher sliding contact[J]. IEEJ Transactions on Electrical and Electronic Engineering, 2022,17(8):1198-1208. [15] 李白, 鲁军勇, 谭赛, 张永胜, 蔡喜元. 高速滑动电接触电枢表面动态磨损过程研究[J]. 电工技术学报, 2023, 38(1): 131-139. Li Bai, Lu Junyong, Tan Sai, Zhang Yongsheng, Cai Xiyuan.Research on Dynamic Wear Process of Armature Surface in High-Speed Sliding Electric Contact. Transactions of China Electrotechnical Society, 2023, 38(1): 131-139. [16] 翟小飞,李鑫航,刘华,彭之然.电磁轨道发射装置动态电感梯度分析[J].国防科技大学学报,2022,44(03):156-163. ZHAI Xiaofei LI Xinhang LIU Hua.Analysis of the Dynamic Inductance Gradient of Electromagnetic Rail Launcher[J].Journal of National University of Defense Technology, 2022,44(03):156-163. [17] Lv Q A, Xiang H J, Lei B, et al.Physical principle and relevant restraining methods about velocity skin effect[J]. IEEE Transactions on Plasma Science, 2015, 43(5):1523-1530. [18] Nail Tosun, Doˇga Ceylan, Hakan Polat,et.al. A Comparison of Velocity Skin Effect Modeling With 2-D Transient and 3-D Quasi-Transient Finite Element Methods[J].Plasma,2021,49(4):1500-1507. [19] 张嘉炜, 鲁军勇, 谭赛, 张永胜, 李白. 考虑初始接触压力的滑动电接触界面磁扩散模型[J]. 电工技术学报, 2022, 37(2): 488-495. Zhang Jiawei, Lu Junyong, Tan Sai, Zhang Yongsheng, Li Bai.A Magnetic Diffusion Model of Electromagnetic Launcher Considering Initial Contact Pressure. Transactions of China Electrotechnical Society, 2022, 37(2): 488-495. [20] Zhai X, Liu H, Peng Z.Research on Armature Thrust Inductance Gradient of the Electromagnetic Rail Launcher[J]. IEEE Transactions on Plasma Science, 2022, 50(3): 754-760. |
|
|
|