First Step to Optimum Rotor Design for E-Motors with High Power Density for Aircraft Propulsion

被引:1
作者
Keuter, Ralf Johannes [1 ]
Ponick, Bernd [1 ]
机构
[1] Leibniz Univ Hannover, Inst Drive Syst & Power Elect, Hannover, Germany
来源
2022 25TH INTERNATIONAL CONFERENCE ON ELECTRICAL MACHINES AND SYSTEMS (ICEMS 2022) | 2022年
关键词
Aicraft propulsion; rotor design; permanent-magnet synchronous machine (PMSM); multiobjectiv genetic algorithm; all-electric aircraft;
D O I
10.1109/ICEMS56177.2022.9982946
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
To meet the challenge of all-electric flight, e-motors with particularly high power density are necessary, PM synchronous machines being a preferable motor type. The rotor of an e-motor is a key factor determining its characteristics and thus also its power density. There is a wide range of rotor topologies with an even wider range of parameters to choose from. Since flux density directly affects torque generation, the idea is to determine which rotor topology achieves the best main spatial harmonic flux density to rotor weight ratio. For this purpose, a multiobjective genetic algorithm was used, which finds the best solutions in sufficient time despite the large parameter range. The evaluation of about 25000 results shows that surface mounted configurations such as traditional surface magnets or a Halbach-Array configuration provide good solutions. However, for a high torque, high current density approach, spoke-type magnets are the best, since they have advantages in terms of demagnetization. For a high-speed, low pole pair approach, V-shaped buried magnets seem to lead to the best solution. The presented approach provides a possibility to perform a pre-selection of rotor topologies, but requires more detailed application-specific investigations.
引用
收藏
页数:6
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