Recent Developments of the Arrayed Controlled Turn-less Structures (ACTS) Motor

O. Zucker, Carl Demolder, T. Le
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Abstract

The paper discusses the application of the Array Controlled Turn-less Structures (ACTS) motor for VTOL application. The motor enhances the three main competing characteristics of electric motors; namely specific power, efficiency and reliability. The motor arrays an ensemble of elemental turn-less motors which include turn-less elements each with their dedicated inverters which are operated in synchronism. The resulting small pole size enhances the power density, the enhanced conductor packing enhances the efficiency, and the massive parallelism enhance the reliability. Vertical takeoff requires much higher thrust compared to wing assisted takeoff. With limited on-board power, this higher thrust is presently provided by in ordinary larger propulsion disk area which reduces the craft aerodynamics, and the cruising Lift-to-Drag (L/D) ratio and accordingly the flight efficiency and range. The high specific power of the ACTS motor allows for a different scenario and thus craft architecture. By substantially increasing the takeoff power which is now possible with the higher specific power of the ACTS motor, the propulsion disk area can be substantially reduced, with the resulting greater streamlined, high L/D craft, and thus longer range. The paper discusses key aspect of the motor and inverter architecture and technology. Furthermore, it discusses its application to a high L/D VTOL and prospective performance.
阵列控制无匝结构(ACTS)电机的最新进展
本文讨论了阵列控制无匝结构(ACTS)电机在垂直起降中的应用。该电机增强了电动机的三个主要竞争特性;即比功率、效率和可靠性。电动机阵列是一组基本无转电动机,其中包括每个无转电动机及其同步运行的专用逆变器。由此产生的小极尺寸提高了功率密度,增强的导体封装提高了效率,大量并行性提高了可靠性。与机翼辅助起飞相比,垂直起飞需要更高的推力。在机载动力有限的情况下,这种更高的推力目前由普通的更大的推进盘面积提供,这降低了飞行器的空气动力学和巡航升阻比(L/D),从而降低了飞行效率和航程。ACTS电机的高比功率允许不同的场景,因此工艺架构。通过大幅增加起飞功率(现在ACTS发动机的比功率更高),推进盘面积可以大幅减少,从而产生更大的流线型,更高的L/D,从而更远的航程。本文讨论了电机和逆变器的结构和技术的关键方面。此外,还讨论了该方法在高L/D垂直起降中的应用及未来性能。
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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