A Novel Secondary for Reducing Thrust Ripple of Long Primary Double Sided Linear Induction Machine Used in Microgravity Experimental Chamber Launch System
Pages 1 - 6
Abstract
Based on the electromagnetic field theory, the distribution of thrust density along the longitudinal direction of long primary double-sided linear induction machine (DLIM) with plates secondary is studied. Then a novel wedge type secondary for long primary DLIM is proposed to reduce the ripple of thrust and acceleration. The influence of new secondary parameters on DLIM performance is researched, and the characteristics of thrust and its ripple of plate secondary and new wedge secondary are calculated. The effects of these two kinds secondary on thrust force ripple and system acceleration are compared. The research suggests that the new secondary structure can reduce thrust ripple and improve the stability of system acceleration.
References
[1]
C. Lotz, T. Frobose, A. Wanner, L. Overmeyer and W. Ertmer, “Einstein-Elevator: A New Facility for Research from µg to 5 g,” Gravitational and Space Research, Vol. 5, No.2, pp.11-27, 2017.
[2]
X. Long, “Theory and method of electromagnetic design for linear induction motors,” Beijing: Science Press, 2006.
[3]
X. Sun, L. Shi, Z. Zhang, H. Zhu, “The thrust fluctuation suppression of segmented double sided linear induction motor,” Annual Conference of the IEEE Industrial Electronics Society, pp.3693-3697, 2017.
[4]
T. Yang, L. Zhou, “Longitudinal dynamic end effect in long primary double-sided linear induction motor Part 1: air gap magnetic field,” Electric Machines & Control, 2014, 18(4):52–59.
[5]
T. Yang, L. Zhou, and L. Li, “Influence of Design Parameters on End Effect in Long Primary Double-Sided Linear Induction Motor,” IEEE Transactions on Plasma Science, Vol.39, No.1, pp 192–197, 2011.
[6]
C. Lotz, Y. Wessarges, J. Hermsdorf, W. Ertmer, and L. Overmeyer, “Novel active driven drop tower facility for microgravity experiments investigating production technologies on the example of substrate-free additive manufacturing,” Advances in Space Research, Vol.61, No.8, pp.1967-1974, 2018.
[7]
T. Yang, L. Zhou, L. Li, “Performance Calculation for Double-Sided Linear Induction Motor with Short Secondary”, [C]// International Conference on Electrical Machines & Systems. IEEE, pp.3478-3483, 2008.
[8]
S. Nie, W. Ma, W. Li, and J. Xu, “Research on thrust ripple of long primary linear induction motors with symmetrical current excited,” Proceedings of the CSEE, Vol.35, No.21, pp.5585-5591, 2015.
[9]
I. Boldea, “Linear electric machine, drives, and MAGLEVs handbook,” CRC Press, London, UK, 2013.
[10]
J. F. Gieras, “Linear Induction Drives,” Oxford, U.K.: Clarendon, 1994.
Index Terms
- A Novel Secondary for Reducing Thrust Ripple of Long Primary Double Sided Linear Induction Machine Used in Microgravity Experimental Chamber Launch System
Index terms have been assigned to the content through auto-classification.
Recommendations
Comments
Information & Contributors
Information
Published In
August 2019
5842 pages
Copyright © 2019.
Publisher
IEEE Press
Publication History
Published: 01 August 2019
Qualifiers
- Research-article
Contributors
Other Metrics
Bibliometrics & Citations
Bibliometrics
Article Metrics
- 0Total Citations
- 0Total Downloads
- Downloads (Last 12 months)0
- Downloads (Last 6 weeks)0
Reflects downloads up to 13 Jan 2025