Efficiency and Practical Implementation of the Double Armature Linear Pulse Electromechanical Accelerator

V. Bolyukh, A. Kocherga
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Abstract

A mathematical model of a linear pulsed electromechanical accelerator with coil and massive electrically conductive armatures in the presence of a ferromagnetic shield has been developed and implemented in the Somsol Multiphysics software package. The electrical and mechanical characteristics of the accelerator are obtained when the inductor winding is excited from capacitive energy storage of vibration-damped, aperiodic and aperiodic with feeding by current forms. Using a complex efficiency criterion, which takes into account the amplitude of the current in the inductor winding, the maximum speed of the electrically conductive armature, the magnitude of the impulse of the total electrodynamic forces, the average level of the stray field and electrically conductive armature. On the basis of a two-armature accelerator with a ferromagnetic shield, a model of an electromagnetic catapult for a unmanned aerial vehicle was manufactured and tested. In the process of experimental research, the electrical, magnetic, mechanical and thermal parameters of the catapult were measured simultaneously. It was found that the maximum speed of a unmanned aerial vehicle based on an accelerator with a parallel connection of active elements is 60% higher than with their serial connection.
双电枢线性脉冲机电加速器的效率与实用实现
在Somsol Multiphysics软件包中建立了具有线圈和大质量导电电枢的线性脉冲机电加速器在铁磁屏蔽下的数学模型。得到了电感绕组由阻尼式、非周期式和非周期式三种电流馈电形式的电容式储能系统励磁时加速器的电学和机械特性。采用一种复杂的效率准则,该准则考虑了电感绕组中电流的幅值、导电电枢的最大速度、总电动力脉冲的大小、杂散场和导电电枢的平均水平。在铁磁屏蔽双电枢加速器的基础上,研制了一种无人机电磁弹射器模型并进行了试验。在实验研究过程中,对弹射器的电、磁、力学和热参数进行了同步测量。研究发现,基于加速器的无人机,主动元件并联时的最大速度比主动元件串联时高60%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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