直升机尾桨的电动动力系统

L. Castellini, M. D'Andrea, M. Villani
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引用次数: 1

摘要

介绍了电动直升机尾桨用多相永磁无刷电机的设计。所提出的电机允许替代实际机构在尾桨系统匹配包络,重量和性能。为了在电机外形尺寸小的情况下获得大的转矩,选择了一种带有内部pm的辐条式解决方案。采用了一种优化程序,将热学和电磁要求结合起来,以改进整体设计。通过有限元分析对电机性能进行了评估,以验证最终设计并开始样机生产。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Electric powertrain for helicopter tail rotor
The design of multi-phase permanent magnet brushless motor for an electrical helicopter tail rotor is introduced and described. The presented electric machine allows a substitution of the actual mechanisms in tail rotor system matching envelope, weights and performances. In order to obtain high torque with small overall dimensions of the motor, a spoke-type solution with interior PMs has been chosen. An optimization procedure has been used to combine thermal and electromagnetic requirements with the aim to improve the overall design. The motor performance has been evaluated by the FE analysis to validate the final design and start the prototype production.
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