基于有限元-边界元法的电磁轨道炮增强构型仿真

IF 1.8 Q3 ENGINEERING, ELECTRICAL & ELECTRONIC
S. R. Naga Praneeth;Bhim Singh
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引用次数: 0

摘要

在处理机电系统建模时,数值挑战是不可避免的。特别是在处理移动导体问题时,如旋转或线性电机,需要特别注意气隙区域。Railguns空中区域是这个建模问题的又一个补充。空气区域需要重新网格化或自定义网格拓扑。此外,为形状复杂的导体生产空气网也有其自身的困难。可以通过使用有限元边界元(FE-be)技术来减少空气网格需求。空气网格的边界元和导体的有限元允许创建具有移动导体的模型,并使模型制作更容易、更快。本文通过有限元边界元模拟方法,研究了当轨道炮中增加轨道的几何形状发生变化时,轨道炮的电气和机械参数的变化。锥形和圆角是在电磁轨道炮的增强轨道上实现的两种几何变化。使用LS Dyna软件对设计的轨道炮变体进行了研究。为了计算炮管效率,推导了一种新的增程式电磁轨道炮后膛电压公式。分析了增广电磁轨道炮的四种配置,重点是力分布、电感梯度和运动电动势($iL^{\prime}v$)。其中一种新的配置使发射初期的力分布提高了8.8%,电枢的最终初速提高了7%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Finite Element-Boundary Element Method Based Simulations of Electromagnetic Railgun in Augmented Configurations
When dealing with electromechanical system modelling, numerical challenges are inevitable. Especially when working with moving conductor problems, such as rotational or linear motors, special care needs to be taken for the air-gap region. Railguns air region is one more addition to this modelling problem. The air region necessitates either remeshing or a custom mesh topology. In addition, the production of air mesh for conductors with complicated shapes has its own difficulties. The air mesh requirement may be reduced by using the finite element-boundary element (FE-BE) technique. Boundary elements for air mesh and finite elements for conductors allow for the creation of models with moving conductors and makes model production easier and quicker. This paper investigates the changes observed in the railgun's electrical and mechanical parameters through the finite element-boundary element simulation approach when the geometry of the augmentation rails in a railgun is changed. Tapering and filleting are two geometry changes implemented on the augmenting rails of an electromagnetic railgun. Designed railgun variants are investigated using LS-Dyna software. A new formulation for breech voltage in augmented electromagnetic railguns is derived to calculate barrel efficiency. Four configurations of augmented electromagnetic railguns are analyzed, emphasizing force profile, inductance gradient, and motional-emf ( $iL^{\prime }v$ ). One of the new configurations has resulted in an improvement in the force profile during the initial stages of the launch by 8.8%, and the armature's final muzzle velocity has improved by 7%.
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来源期刊
CiteScore
4.30
自引率
0.00%
发文量
27
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