Cogging force mitigation techniques in a modular linear permanent magnet motor

被引:17
|
作者
Tootoonchian, Farid [1 ]
Nasiri-Gheidari, Zahra [2 ]
机构
[1] Iran Univ Sci & Technol, Dept Elect Engn, High Precis & High Speed Machines Lab, Tehran, Iran
[2] Sharif Univ Technol, Sch Elect Engn, Tehran, Iran
关键词
linear motors; permanent magnet motors; machine control; force control; permanent magnets; magnetic leakage; magnetic flux; air gaps; propulsion; cogging force mitigation techniques; modular linear doubly salient permanent magnet motors; linear propulsion systems; power density; reduced maintenance cost; reduced initial cost; permanent magnet leakage flux; fault tolerance capability; cogging thrust; air-gap reluctance variation minimisation; PM volume; average air-gap length; thrust ripples; cogging reduction techniques; FLUX-REVERSAL MACHINE; SYNCHRONOUS MOTOR; EXPERIMENTAL-VERIFICATION; TORQUE; REDUCTION; DESIGN; ROTOR; SIMULATION;
D O I
10.1049/iet-epa.2015.0575
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
Modular linear doubly salient permanent magnet motors are well adapted to linear propulsion systems because of their distinct characteristics, such as high efficiency and power density, reduced maintenance and initial cost, low noise and permanent magnet (PM) leakage flux, and fault tolerance capability. However, such motors suffer from high cogging thrust. In this study, various techniques based on previously proposed methods for PM machines are applied on the studied motor and evaluated by using non-linear three-dimensional time-stepping finite element analysis; three novel, optimised techniques are then presented. The techniques presented are based on the minimisation of the variation in air-gap reluctance relative to the displacement. The PM volume and average air-gap length are kept constant in all optimisations. Since the average thrust and thrust ripples under load condition may be affected by cogging reduction techniques, these values are presented for all given techniques. The results show that the proposed techniques not only maintained the average thrust under various loads but also significantly suppressed the thrust ripples for different average thrusts and cogging forces.
引用
收藏
页码:667 / 674
页数:8
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