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Thermal Stresses Analysis of the Rails and the Armature of an Electromagnetic Launcher

机译:导轨的热应力分析和电磁发射器的电枢

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In an electromagnetic launcher, the magnetic field creates a dynamic force that moves the armature forward. During the launch, electrical current creates high body forces and temperature distribution in the rails and the armature. As a result the rails and armature experience high amplitude stress and strain which damage the rails and the armature and reduces their life span. The purpose of this paper is to investigate the effect of body force as well as the temperature distribution on the displacement of the rails in an electromagnetic launcher. In this study the physical and geometrical properties of the rails are constant in location. In our formulation of governing non-linear differential equations, Maxwell, Energy equation and Navier equation are applied to the rails under dynamic loading. To solve the non-linear governing differential equations a finite difference base code is developed and utilized. It is shown that the Maximum volumetric forces take place where the highest magnetic field gradient occurs. In addition, the maximum magnetic force is accumulated at the trailing edge of the armature and portions of the rail interior. The thermal stresses distribution follows the same trend as displacement due to temperature behavior of the rails.
机译:在电磁发射器中,磁场产生动态力,其向前移动电枢。在发射期间,电流在轨道和电枢中产生高体力和温度分布。结果,轨道和电枢经历了高幅度应力和压力,损坏了轨道和电枢,并降低了它们的寿命。本文的目的是研究体力的影响以及电磁发射器中轨道位移的温度分布。在该研究中,轨道的物理和几何特性在位置恒定。在我们控制非线性微分方程的配方中,MaxWell,能量方程和Navier方程被应用于动态负载下的轨道。为了解决非线性控制微分方程,开发和利用有限差分基码。结果表明,最大容量力发生在发生最高磁场梯度的地方。另外,最大磁力累积在轨道内部的衔铁的后缘和部分。由于轨道的温度行为,热应力分布遵循与位移相同的趋势。

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