High-Temperature Starter-Generator with Fractional-Slot Concentrated Windings for More Electric Aircraft: Design and Testing of the Scaled-Size Prototype

F. Ismagilov, V. Vavilov, N. Tarasov, V. Ayguzina
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引用次数: 1

Abstract

This paper presents the design and experimental research of a scaled-size prototype of the high-temperature starter-generator for more electric aircrafts. A computer model of the prototype with a high accuracy and good convergence with the experimental results was designed. In addition, the cooling efficiency evaluation was carried out; the losses in starter-generator active parts were estimated. Based on the results of experimental research and computer simulation, the full-size starter-generator was designed. It is important to notice that the full-size starter-generator was less loaded in terms of electromagnetic and thermal loads. This shows the proposed method efficiency. The obtained mass properties of the full-sized starter-generator is less than the 10 kg Thales’ starter-generator. This proves the efficiency of the researched variant.
多电飞机用分数槽集中绕组高温起动发电机:按比例样机的设计与试验
本文介绍了多电飞机用高温起动发电机按比例样机的设计与实验研究。设计了精度高、与实验结果收敛性好的样机计算机模型。此外,还进行了冷却效率评价;估计了起动器-发电机有功部分的损耗。在实验研究和计算机仿真的基础上,设计了全尺寸起动发电机。值得注意的是,全尺寸起动发电机在电磁和热负荷方面的负荷较小。验证了该方法的有效性。得到的全尺寸起动发电机的质量特性小于泰雷兹公司的10公斤起动发电机。这证明了所研究的变体的有效性。
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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