Effect of Encapsulation Shell on Launching Performance of Asynchronous Coil Launcher

被引:1
|
作者
Cong, Yuantao [1 ,2 ]
Cheng, Junsheng [2 ,3 ,4 ]
Wang, Qiuliang [1 ,2 ]
Xiong, Ling [2 ]
Sun, Jian [1 ,2 ]
Wang, Yichen [1 ,2 ]
机构
[1] Univ Chinese Acad Sci, Sch Elect Elect & Commun Engn, Beijing 100049, Peoples R China
[2] Chinese Acad Sci, Inst Elect Engn, Beijing 100190, Peoples R China
[3] Chinese Acad Sci, Ganjiang Innovat Acad, Ganzhou 341000, Peoples R China
[4] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
关键词
Permeability; Conductivity; Mathematical models; Encapsulation; Velocity measurement; Performance evaluation; Analytical models; Electromagnetic launch; encapsulation shell; induced current; induction coil launcher;
D O I
10.1109/TPS.2021.3125682
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
In order to obtain the impact of the shell on the transmission performance of the asynchronous induction coil launcher (AICL), two kinds of finite element models with and without shell are established to study the influence of which on the launch performance. The displacement and exit velocity of the armature are obtained by simulation. Then, we simulated the shells with different conductivities or different permeabilities and summarized the law of the influence of conductivity and permeability on the armature exit speed. In addition, a 3-D model that is relatively closer to the actual situation is established, and the influence of the shell on the armature speed is simulated and analyzed. Finally, the armature exit velocity was measured experimentally, the launch performances of the shelled and unshelled devices were compared, and the reliability of the simulation results was verified, indicating that the impact of the shell on the launch performance should be considered during the design of the launcher. The results show that the shell affects the distribution of the magnetic field. This article summarizes the influence of the shell material characteristics, including conductivity and permeability on the launch performance, and the impact on the launch performance is ultimately manifested as the drop of the armature exit velocity.
引用
收藏
页码:4002 / 4008
页数:7
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