Design of a Compact Stator Winding in an Axial-Flux Permanent Magnet Machine for Aerospace Applications

C. Goldstein, Ehab Sayed, Mohamed Abdalmagid, A. Callegaro, Mikhail Goykhman, A. Emadi
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引用次数: 1

Abstract

The weight and volume of electric drive systems are of primary concern in aerospace applications. Here, a high power density axial-flux permanent magnet machine is developed. A compact stator winding with rectangular wire is proposed. The stator coils are connected along the machine inner diameter (ID). The ID connections help to reduce the machine weight and volume and meet the application targets. A detailed winding design procedure is presented considering manufacturing constraints. An electrostatic analysis is also performed to define the wire insulation thickness and the minimum spacing between conductors to assure the insulation system is free of partial discharges. Additional half turns are added to three coils of the winding to place the three-phase terminals at the machine outer diameter (OD). The resultant electromagnetic impact of these three coils is assessed.
航空航天轴向磁通永磁电机定子绕组的紧凑设计
在航空航天应用中,电力驱动系统的重量和体积是主要关注的问题。研制了大功率密度轴向磁通永磁电机。提出了一种采用矩形导线的紧凑定子绕组。定子线圈沿机器内径(ID)连接。ID连接有助于减少机器重量和体积,满足应用目标。考虑到制造条件的限制,给出了详细的绕组设计过程。还进行了静电分析,以确定电线绝缘厚度和导体之间的最小间距,以确保绝缘系统没有局部放电。在绕组的三个线圈上增加额外的半圈,将三相端子置于机器外径(OD)处。对这三个线圈产生的电磁影响进行了评估。
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