Multi-physical-field characteristics modeling and structure optimization for kW-level ultra-high- speed PM motors with integrated support system

被引:3
|
作者
Gao, Qixing [1 ]
Wang, Xiaolin [1 ]
Zhang, Yan [2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China
[2] Jinling Inst Technol, Sch Intelligence Sci & Control Engn, Nanjing 211169, Peoples R China
基金
中国国家自然科学基金;
关键词
Flywheel energy storage; Integrated support system; Multi-physical-field charac-teristics; Mechanical strength; Rotor dynamics; Ultra-high-speed motor; DESIGN;
D O I
10.1016/j.cja.2022.12.013
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the aerospace industry, the low-mass ultra-high-speed flywheel system play a critical role. In this paper, a kW-level Ultra-High Speed Permanent Magnet Synchronous Motor (UHSPMSM) as the core component of flywheel system is proposed and analyzed with considera-tion of multiple physical fields, including electromagnetic characteristics, mechanical strength and rotor dynamics. The integrated support structure is put forward to improve rotation accuracy and operation stability of the UHSPMSM. Further, influence of the integrated support structure on critical speed is explored, and the key parameters such as support position and support stiffness are designed. Moreover, the rotor strength is analyzed by analytical model developed of rotor stress that can deal with multiple boundary types. Material and thickness of the sleeve are optimized, and range of interference value is accurately limited based on four extreme operating conditions. The 3-D Finite Element Model (FEM) is used to validate the strength characteristics and stress distribu-tion of rotor. A 1.5 kW-150000 r/min UHSPMSM with integrated support system is manufactured and tested. The feasibility of UHSPMSM proposed and the accuracy of analysis method are verified through electromagnetic, temperature rise and vibration characteristics test. The machine prototype realizes the load operation at rated speed and the multi-physical-field characteristics achieve the design specification.(c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
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页码:455 / 467
页数:13
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