降低涡流层器件涡流能量损失的方法

E. Danilina, V. Astakhov
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引用次数: 1

摘要

本文讨论了降低涡流层器件工作区域涡流能量损失的几种方法。利用已知的数学模型进行了数值实验,以评估有效性,识别和分析每种方法的所有优点和缺点。计算结果用图形表示了能量损失与工作区域壳体厚度和磁场电感频率的关系;随场频变化,涡流沿工区壳长分布曲线图;在对称轴上为原磁场和壳层反应场的分布图。结果表明,对于三电感涡流层器件,在工作区域壳体中加入两个等间距的正交切口可以减少43%的能量损失,而根据连接方法的不同,电感的交替配置可以减少20%至29%的能量损失。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Methods for Eddy Current Energy Losses Reduction in Vortex-Layer Devices
This paper discusses several methods to reduce the eddy current energy losses in a working area of the vortex-layer devices. Using a known mathematical model numerical experiments were carried out to evaluate effectiveness, to identify and analyze all the advantages and disadvantages for each of the proposed methods. The calculation results are presented as graphs of the dependences of the energy losses on the working area shell thickness and on the frequency of the field inductors; as graphs of the distribution eddy current flow function along the working area shell length with the varying field frequency; as graphs of the distribution primary magnetic field and shell reaction field on the symmetry axis. It was established that for the three-inductor vortex-layer device addition of two equally spaced orthogonal cuts in the working area shell leads to a 43% energy losses reduction, and an alternating configuration of the inductors gives a reduction from 20% to 29% depending on the connection method.
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