Modeling and Optimization of Detent Force for Flexible Permanent Magnet Synchronous Linear Motor Considering Spacing Between Primaries
ID:176 Submission ID:176 View Protection:PRIVATE Updated Time:2021-07-01 09:43:02 Hits:895 Oral Presentation

Start Time:2021-07-02 08:30 (Asia/Shanghai)

Duration:20min

Session:[S1] Concurrent Session 1 » [S1-3] Oral Session 11 & 14

Presentation File

Tips: The file permissions under this presentation are private. You have not logged in yet and cannot view it temporarily.

Abstract
A kind of flexible permanent magnet linear synchronous motor (PMLSM) with multiple primaries and secondaries is adopted in this paper. Considering the flexible adjustment of the assembly spacing distance between primaries, the magnetic coupling effect between the two adjacent primaries and the end effect are analyzed. Also, how magnetic coupling effect influences the characteristics of the detent force is compared and analyzed in detail. The model of the detent force which has taken both end effect and magnetic coupling effect at different spacing distances into consideration is derived to reveal the fluctuation rule. To minimize the detent force, the rectangular and ladder end teeth are employed with the orthogonal optimization method, which effectively suppress the detent force when the mover runs across the sectional primary cores. Finally, a prototype of segmented multi-mover permanent magnet synchronous linear motor (SMM-PMSLM) with continuous arrangement as well as its test platform are developed to test the detent force.
Keywords
Linear motor, flexible assembly, detent force, end effect, magnetic coupling effect.
Speaker
Qian Huang
Nanjing University of Aeronautics and Astronautics

Qian Huang  is currently working towards the M.E. degree in electrical engineering in Nanjing University of Aeronautics and Astronautics, Nanjing, China. Her current research interests include the design and drive control of permanent magnet linear synchronous motors.
 

Submission Author
Xuzhen Huang Nanjing University of Aeronautics and Astronautics
Comment submit
Verification code Change another
All comments