Design Study of a Coupled Inner-Stator Magnetically Geared Motor for Electric Aircraft Applications

Thomas F. Tallerico, J. Scheidler
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Abstract

Electric aircraft require high performance and high reliability electric motor drivetrains. A geared electric motor drivetrain will outperform a direct drive motor drivetrain in most applications. Traditional mechanical gearing, however, has mechanical contact-based wear and failure modes that result in added maintenance costs and require an oil lubrication system. Magnetically geared motor drives are a potential technology for electric aircraft applications capable of enabling the benefits of a geared drive without the maintenance, reliability, and lubrication system cost of mechanical gears. In this paper, a topology of magnetically geared motor, an inner-stator magnetically geared motor, is explored to estimate its achievable performance for electric aircraft applications. Optimization results on the topology show that it can achieve greater than 15 Nm/kg specific torque and 96% efficiency at 100 kW of power.
电动飞机用内定子耦合磁力减速电机的设计研究
电动飞机需要高性能、高可靠性的电动机传动系统。在大多数应用中,齿轮传动电机传动系统将优于直接驱动电机传动系统。然而,传统的机械传动装置具有机械接触磨损和失效模式,导致维护成本增加,并且需要油润滑系统。磁性减速电机驱动是电动飞机应用的潜在技术,能够实现齿轮传动的优点,而无需机械齿轮的维护,可靠性和润滑系统成本。本文研究了一种内定子磁力减速电机的拓扑结构,以估计其在电动飞机上可实现的性能。拓扑优化结果表明,在功率为100 kW时,比转矩可大于15 Nm/kg,效率可达96%。
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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