Design and Testing of a Modular High-Speed Permanent-Magnet Machine for Aerospace Propulsion

James Swanke, Hao Zeng, Dheeraj Bobba, T. Jahns, B. Sarlioglu
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引用次数: 3

Abstract

High-power-density megawatt-scale surface permanent magnet (SPM) machines are strong candidates for future aircraft electric propulsion applications. Additional power density and fault tolerance benefits can be gained by designing the machine as an Integrated Modular Motor Drive (IMMD) that breaks the machine into multiple three-phase modules, each with its own dedicated power electronics. This paper discusses development of a 1 MW SPM machine for an IMMD configuration with a rated speed of 20,000 rev/min. A lower-power demonstrator version of this machine (200 kW) has been built to retire key technical risks and to validate machine models for the final design. The materials, components, and performance of this demonstrator machine are reviewed. The machine test configuration is described, and initial test results are presented that exhibit promising agreement with performance predictions provided by simulations and analytical models. Finally, fault tolerance benefits of the modular stator design are experimentally demonstrated.
航天推进用模块化高速永磁电机的设计与试验
高功率密度的兆瓦级表面永磁(SPM)电机是未来飞机电力推进应用的有力候选者。通过将机器设计为集成模块化电机驱动器(IMMD),可以将机器分成多个三相模块,每个模块都有自己的专用电力电子设备,从而获得额外的功率密度和容错性优势。本文讨论了额定转速为20,000转/分钟的imd配置的1mw SPM机的开发。该机器的低功率演示版本(200千瓦)已经建成,以消除关键技术风险并验证最终设计的机器模型。对该样机的材料、部件和性能进行了综述。描述了机器测试配置,并提出了初步测试结果,显示出与仿真和分析模型提供的性能预测有希望的一致。最后,通过实验验证了模块化定子设计的容错效果。
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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