Optimization of Rotor Tooth Shape of Aerospace Homopolar Alternators

R. E. Hopkins, E. Erdelyi
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引用次数: 11

Abstract

In the first part of the optimization process, the width and depth of the rotor tooth are incrementally varied for two airgap radial lengths and two field excitations. In the second part the tooth shape that would yield a sinusoidal voltage is investigated. The numerical results are represented by curves for the no-load radial flux density in a 95 KVA, 120/208 v 3,400 cps alternator. The results show that the fundamental airgap flux density depends on the length of the airgap and on the rotor tooth width. It depends only slightly on the rotor tooth depth and excitation. A more sinusoidal output voltage can be obtained by flaring the tips of the rotor tooth and widening the rotor tooth.
航空同极交流发电机转子齿形优化研究
在第一部分优化过程中,在两种气隙径向长度和两种场激励下,转子齿的宽度和深度是增量变化的。在第二部分的齿形,将产生一个正弦电压的研究。数值结果用95 KVA、120/208 v、3400 cps交流发电机空载径向磁通密度曲线表示。结果表明,基态气隙磁通密度与气隙长度和转子齿宽有关。它只稍微取决于转子齿深和激励。通过扩宽转子齿尖和扩宽转子齿尖可以获得更正弦的输出电压。
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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