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Study on Suppressing Effect of Deposited Layer on Armature Melting at Sliding Electrical Contact Interfaces |
Yao Jinming1, Sun Jiandong2, Bao Jianbo2, Zhang Tengfei1 |
1. College of Automation & College of Artificial Intelligence Nanjing University of Posts and Telecommunications Nanjing 210023 China; 2. Nari Group Corporation State Grid Electric Power Research Institute Nanjing 210023 China |
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Abstract Maintaining good sliding electrical contact performance is crucial for achieving high-frequency and high-efficiency operation in electromagnetic rail launch systems. In the environment of high current and high-speed sliding electrical contacts, an aluminum deposited layer appears on the rail surface during the first launch after rail surface cleaning. During repetitive launches, the armature slides on the deposited rail, causing the deposited layer to melt due to heating. Melting state of the deposited layer affects the melting wear process on the armature's surface, thereby altering the contact state and influencing the sliding electrical contact performance. Therefore, studying armature's melting characteristics influenced by deposited layer is of great significance for a deeper understanding of interface melting wear mechanisms and for improving sliding electrical contact performance. Firstly, by analyzing the heating process of the deposited layer, equations for calculating its melting moment and melting thickness were established. Within contact time (tc) between armature and deposited layer, the deposited layer is heated by the interface heat source and undergoes melting. A criterion for determining the melting of the deposited layer was proposed by comparing the contact time with the melting moment. If the heating time (tc) of the deposited layer is greater than melting moment (tm), then melting occurs within the contact time. Analysis of the melting characteristics of the deposited layer under different current conditions reveals that the larger the current load, the larger the melting range of the deposited layer. In addition, the deposited layer is more likely to melt during the low-speed stage and less likely to melt during the high-speed stage. Assuming that the deposited layer completely melts at time tr after the start of contact, the armature and the rail directly engage in heat transfer from time tr onwards. Based on the analysis of the heat balance equation under the condition of complete melting of the deposited layer, a calculation model for the melting wear of the armature under the influence of the deposited layer was established, yielding the melting wear rate of the armature. Finally, repetitive launch experiments were conducted with a 20 mm square caliber inner bore. Keeping current waveform and launch mass unchanged, each launch had a velocity of approximately 140 m/s, with a total of 7 launches conducted in the experiments. After each experiment, the armature and rail samples were recovered, and a profile gauge was used to measure the maximum melting depth on the armature's surface and the thickness of the deposited layer on the rail's surface. The experimental results show that the thickness of the deposited layer gradually increases with the number of launches, while the maximum melting depth on the armature's surface decreases with the increasing number of launches. By analyzing the thickness distribution curve of the deposited layer in conjunction with the criterion for deposited layer melting, it was found that the deposited layer was in a state of complete remelting under the current launch conditions. Using the armature melting calculation model under the condition of complete deposited layer remelting, the average maximum melting depth was further calculated. The calculated results from the model show the same trend as the experimental measurements, indicating that deposited layer melting has an inhibitory effect on armature melting.
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Received: 28 August 2023
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[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.Electro-magnetic launch hypervelocity integrated projectile[J]. Journal of National University of Defense Technology, 2019, 41(4): 1-10. [2] 马伟明, 鲁军勇. 电磁发射技术的研究现状与挑战[J]. 电工技术学报, 2023, 38(15): 3943-3959. Ma Weiming, Lu Junyong.Research progress and challenges of electromagnetic launch technology[J]. Transactions of China Electrotechnical Society, 2023, 38(15): 3943-3959. [3] 胡鑫凯, 鲁军勇, 李白, 等. 瞬态条件下电磁轨道发射装置绝缘体热损伤分析[J]. 电工技术学报, 2023, 38(21): 5673-5681. Hu Xinkai, Lu Junyong, Li Bai, et al.Thermal damage analysis of insulator in electromagnetic rail launcher under transient conditions[J]. Transactions of China Electrotechnical Society, 2023, 38(21): 5673-5681. [4] 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. [5] 张嘉炜, 鲁军勇, 谭赛, 等. 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, et al.A magnetic diffusion model of electromagnetic launcher con-sidering initial contact pressure[J]. Transactions of China Electrotechnical Society, 2022, 37(2): 488-495. [6] Chen Lixue, Xu Xuan, Wang Zengji, et al.Melting distribution of armature in electromagnetic rail launcher[J]. IEEE Transactions on Plasma Science, 2023, 51(1): 234-242. [7] Cooper K P, Jones H N, Meger R A.Analysis of railgun barrel material[J]. IEEE Transactions on Magnetics, 2007, 43(1): 120-125. [8] Watt T, Stefani F.The effect of current and speed on perimeter erosion in recovered armatures[J]. IEEE Transactions on Magnetics, 2005, 41(1): 448-452. [9] 李白, 鲁军勇, 谭赛, 等. 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, et al.Research on dynamic wear process of armature surface in high-speed sliding electric contact[J]. Transactions of China Electrotechnical Society, 2023, 38(1): 131-139. [10] 徐伟东, 袁伟群, 陈允, 等. 电磁轨道发射器连续发射的滑动电接触[J]. 强激光与粒子束, 2012, 24(3): 668-672. Xu Weidong, Yuan Weiqun, Chen Yun, et al.Sliding electrical contact performance of electromagnetic launcher system in rapid fire mode[J]. High Power Laser and Particle Beams, 2012, 24(3): 668-672. [11] 刘传谱, 袁伟群, 严萍, 等. 重复推进滑动电接触的试验研究[J]. 强激光与粒子束, 2010, 22(4): 923-926. Liu Chuanpu, Yuan Weiqun, Yan Ping, et al.Experimental study of sliding electrical contacts in a multi-shot railgun[J]. High Power Laser and Particle Beams, 2010, 22(4): 923-926. [12] 姚金明, 傅强. 大电流高速滑动电接触界面热量分配过程[J]. 电工技术学报, 2023: 39(17): 5497-5507. Yao Jinming, Fu Qiang.Heat Partition process at sliding electrical contact interfaces with high-speed and large current[J]. Transactions of China Electro-technical Society, 2023, 39(17): 5497-5507. [13] Paek-Spidell G Y. Analysis of heat partitioning during sliding contact at high speed and pressure[D]. Wright-Patterson Air Force Base: Air Force Institute of Technology, 2014. [14] 汤亮亮. 电磁发射中枢轨接触界面金属液化层特性的实验与理论研究[D]. 武汉: 华中科技大学, 2015. Tang Liangliang.Experimental and theoretical study on liquid metal film characteristic of armature/rail contact interface in an electromagnetic launching[D]. Wuhan: Huazhong University of Science and Technology, 2015. [15] Chen Lixue, He Junjia, Xia Shengguo, et al.Some key parameters of different caliber solid-armature railgun related to linear current density[J]. IEEE Transactions on Plasma Science, 2017, 45(7): 1134-1138. [16] Yao Jinming, Yu Kun, Fu Qiang, et al.Computational method for heat partition at the rail-armature interface based on least squares regression[J]. IEEE Transactions on Plasma Science, 2021, 49(6): 2008-2014. [17] 温诗铸, 黄平. 摩擦学原理[M]. 4版. 北京: 清华大学出版社, 2013. [18] Tian Xuefeng, Kennedy F E Jr. Contact surface temperature models for finite bodies in dry and boundary lubricated sliding[J]. Journal of Tribology, 1993, 115(3): 411-418. [19] 肖铮. 电枢—轨道载流滑动接触面摩擦磨损研究[D]. 武汉: 华中科技大学, 2012. Xiao Zheng.Friction and wear behavior of armature-rail sliding electrical contact surface[D]. Wuhan: Huazhong University of Science and Technology, 2012. [20] Yao Jinming, Xia Shengguo, Chen Lixue, et al.Analysis of the melt erosion patterns at rail-armature contact of rail launcher in current range of 10- 20 kA/mm[J]. IEEE Transactions on Plasma Science, 2019, 47(3): 1674-1680. |
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