场反构型电磁推进器轴向稳态磁场的数值仿真研究

Numerical Simulation Study of Axial Steady State Magnetic Field of Field-reversed Configuration Electromagnetic Thruster

  • 摘要: 轴向稳态磁场作为场反构型电磁推进器的核心部分,其性能直接影响推进器的整体工作效率和性能。针对其在工程实验中工作效率较低和性能较差的情况,开展轴向稳态磁场分布优化研究。采用多物理场仿真软件自适应函数细化轴向稳态磁场区域网格法提高仿真精度,并开展了数值模拟,探究了轴向稳态磁场线圈不同结构对磁场分布的影响,并利用实验结果进行对比验证,为场反构型电磁推进器轴向稳态磁场的优化设计提供了理论依据。

     

    Abstract: The axial steady-state magnetic field is an indispensable component of electromagnetic thrusters in field reversal configuration. The characteristics and strength of the magnetic field distribution are directly correlated with the overall efficiency and performance of the thruster. In light of the shortcomings in efficiency and performance observed in current engineering experiments, an in-depth study has been undertaken with the objective of optimizing the distribution of the axial steady-state magnetic field, thereby enhancing the operational efficacy of the thruster. During the course of the in-depth study, it was established that the distribution and strength of the magnetic field must be rigorously controlled. Accordingly, a comprehensive optimisation study of the axial steady-state magnetic field was conducted. This study was not merely a theoretical endeavour, it was also intended to facilitate practical improvements. The research programme initially deployed the adaptive capabilities of multi-physics field simulation software. By optimizing the method of mesh division in the region of the axial steady-state magnetic field, the accuracy of the simulation calculation was markedly enhanced. Furthermore, the impact of varying coil configurations on the magnetic field distribution within the axial steady-state magnetic field was subjected to comprehensive analysis. Furthermore, a comprehensive analysis of the coil structure was conducted with the objective of optimizing the coil design. Through a process of repeated testing and adjustments, the objectives of optimizing the magnetic field distribution and maximising the thruster efficiency were successfully achieved. This study makes a significant contribution to the advancement of direct performance, while also providing a foundation for future developments in electromagnetic propulsion technology. It ensures that the thruster can operate with optimal efficiency and reliability. The comparison of experimental results with numerical simulations provides strong validation and a scientific theory.

     

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