边界层吸入风扇推进用高频电机

Andy Yoon, K. Haran
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引用次数: 13

摘要

高比功率电动机是飞机电力/混合动力推进的关键使能技术。高频、“空芯”机器拓扑结构显示出当机器在高速下(例如15,000 rpm)集成到喷气发动机中时,具有高比功率的潜力。在本文中,我们探讨了这些机器如何在一定速度范围内扩展到电力推进系统,并在新提出的带有尾部边界层(STARC-ABL)推进器的单通道涡轮电动飞机中包括“边界层摄取”风扇。通过实验验证了详细的分析模型,并利用进化遗传算法研究了速度对拓扑权值的影响。结果表明,该拓扑结构在低速下仍能保持较高的比功率,特别是选择适当的支撑结构设计。此外,实例研究表明,边缘驱动的风扇拓扑结构有利于边界层吸入风扇。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High Frequency Electric Machines for Boundary Layer Ingestion Fan Propulsor
High specific power electric motor is a key enabling technology for electric/hybrid-electric propulsion for aircraft. High-frequency, ‘air-core’ machine topologies show potential for high specific power when the machines are integrated within jet engines at high speed, e.g. 15,000 rpm. In this paper, we explore how these machines scale to electric propulsion systems at a range of speeds, to also include ‘boundary layer ingestion’ fan in newly proposed Single-aisle Turboelectric Aircraft with an Aft Boundary-Layer (STARC-ABL) propulsors. Detailed analytical models that have been experimentally verified, and an evolutionary genetic algorithm are utilized to study the effect of speed on weight of the topology. The results show that the topology, especially with proper selection of support structure design, maintains high specific power even at lower speeds. Furthermore, a case study shows that rim-driven fan topology is favorable for the boundary layer ingestion fan.
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