航天主推进用600kW环形直驱磁通开关永磁电机的设计

C. Sanabria-Walter
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引用次数: 6

摘要

电动飞行是未来航空航天工业的主要目标之一。对于航空航天应用,提供高扭矩密度的电机对于飞机直接驱动电力推进的可行性至关重要。除了低重量和高扭矩能力外,候选解决方案还应具有固有的容错能力,以便在航空航天中使用。由于这些原因,基于磁通开关永磁(FSPM)电机的第一个解决方案用于直升机主旋翼驱动的示例应用进行了研究,因为这些机器在过去十年的研究中显示出高扭矩重量比和高效率。尽管如此,设计适合这种应用的机器的任务超越了电磁设计,进入了比传统设计更深的机械设计领域:这种铁基机器的轻量化使得支撑结构和气隙控制的设计具有挑战性,需要非常规的方法。本文介绍了该机器的主要设计步骤和初步实验结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of a 600kW ring-type direct-drive Flux-Switching Permanent Magnet machine for aerospace main propulsion
More-Electric flight is one of the main objectives of the aerospace industry for the future. For aerospace applications, electrical machines providing high torque density are paramount for the viability of direct-drive electrical propulsion of aircraft. Besides low-weight and high torque capability, a candidate solution should also be inherently fault tolerant for it to be used in aerospace. For these reasons a first solution based on Flux-Switching Permanent Magnet (FSPM) machines for an exemplary application of a helicopter main rotor drive was investigated, since these machines have shown high torque-to-weight ratios and high efficiency during research in the last decade. Despite this, the task of designing a machine appropriate for this application goes beyond the electromagnetic design and into the area of mechanical design much deeper than for traditional designs: The lightweight nature of such an iron-based machine makes the design of support structures and airgap control challenging and requires unconventional approaches. This paper presents the main design steps and first experimental results for such a machine.
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