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Optimization of Shield Thickness of Finite-Length Solid Rotors for Eddy-Current Loss Minimization

机译:为减小涡流损耗而优化的有限长实心转子的屏蔽层厚度

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摘要

A high-conductivity shield is often used for coating the rotor of solid-rotor synchronous machines for reducing the surface eddy-current losses due to armature-reaction space/time harmonics and/or tooth ripple. Since the design process for determining the optimal shield thickness can be complicated and time consuming, a simple analytical model based on Maxwell''s equations was developed and presented in a previous paper to simplify the process. It has been shown that such an analytical tool can be used as a quick and effective “screening tool” for determining the range of the optimal shield thickness for minimizing rotor surface losses; however, the influence of finite rotor axial length including the end-face losses was not taken into account. In this paper, an additional step is introduced in the shield design process where a special finite-element (FE) method that accounts for the impact of finite rotor axial length is employed for refining the design obtained from the analytical solution. Comparisons are made for a number of shield thicknesses and rotor lengths for significant space and time harmonic combinations to verify the validity of the proposed two-step design process (analytical and FE) and to evaluate the impact of the finite length of solid rotors.
机译:高电导率屏蔽层通常用于涂覆实心转子同步电机的转子,以减少由于电枢反应空间/时间谐波和/或齿纹引起的表面涡流损耗。由于确定最佳屏蔽层厚度的设计过程可能很复杂且耗时,因此开发了基于Maxwell方程的简单分析模型,并在先前的论文中提出以简化此过程。已经表明,这种分析工具可以用作快速有效的“筛选工具”,用于确定最佳屏蔽层厚度的范围,以最大程度地减少转子表面损失;但是,未考虑转子有限轴向长度(包括端面损失)的影响。在本文中,在屏蔽设计过程中引入了额外的步骤,其中采用了一种特殊的有限元(FE)方法,该方法考虑了有限的转子轴向长度的影响,用于完善从解析解决方案获得的设计。比较了多种屏蔽层的厚度和转子长度,以得出有效的空间和时间谐波组合,从而验证了建议的两步设计过程(分析和有限元分析)的有效性,并评估了实心转子有限长度的影响。

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