Reduction of losses in dual‐permanent‐magnet‐excited Vernier machine by segmented stator for electric aircraft

Jinghua Ji, Chen Jia, Wenxiang Zhao, Z. Ling, Yu Zeng, Zongwang Li
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Abstract

The authors present a low‐loss dual‐permanent‐magnet‐excited vernier (DPMEV) machine with segmented stator design to meet the requirements of low iron loss of electric aircraft based on the field modulation theory. The stator topology features and losses of both the original and segmented DPMEV machines are comparatively investigated. Then, the armature air‐gap flux density is deduced by the magnetic motive force‐permeance model, and the influence of each harmonic on the losses are analysed. It is found that the harmonic which produces losses in the original machine reduced greatly after introducing the segmented structure. Furthermore, the electromagnetic performances of two DPMEV machines are comparatively analysed by finite element analysis. Finally, two prototypes of the original and segmented DPMEV machines are built and tested to verify the theoretical analysis.
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通过分段定子降低电动飞机双永磁励磁维尔纳机的损耗
作者基于场调制理论,提出了一种采用分段式定子设计的低损耗双永磁励磁游标(DPMEV)机,以满足电动飞机对低铁损的要求。比较研究了原始和分段式 DPMEV 机器的定子拓扑特征和损耗。然后,通过磁动力-磁导率模型推导出电枢气隙磁通密度,并分析了各次谐波对损耗的影响。结果发现,引入分段结构后,原机产生损耗的谐波大大减少。此外,还通过有限元分析比较分析了两台 DPMEV 机器的电磁性能。最后,制造并测试了原始和分段式 DPMEV 机器的两个原型,以验证理论分析。
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Reduction of losses in dual‐permanent‐magnet‐excited Vernier machine by segmented stator for electric aircraft A compensation method for PMSM sensorless control with parameter identification considering SMO observation error Research on efficient design method of high torque motor with dual airgap hybrid rotor for aircraft engines
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