2011
DOI: 10.1109/tps.2010.2053722
|View full text |Cite
|
Sign up to set email alerts
|

Analysis and Design of Moving-Magnet-Type Linear Synchronous Motor for Electromagnetic Launch System

Abstract: The replacement of steam catapults with electromagnetic ones is becoming an overwhelming trend in aircraft launch systems. Recently, the double-sided linear launcher has attracted more and more attention from researchers. This paper presents the design and analysis of the moving-magnet-type permanentmagnet linear synchronous motor (PMLSM). The thrust density is the most important indicator for a powerful motor, so an analytical expression of the thrust-density coefficient is derived from basic electromagnetic … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
13
0

Year Published

2012
2012
2022
2022

Publication Types

Select...
9
1

Relationship

0
10

Authors

Journals

citations
Cited by 52 publications
(13 citation statements)
references
References 8 publications
0
13
0
Order By: Relevance
“…It must be recalculated when other parameters have been changed. The influences of gap length, thickness of magnet, pole arc coefficient, number of pole pairs to the average thrust have been already discussed for a double-sided linear synchronous motor used for electromagnetic catapults in [3], and some results are consistent with the computed results in [4]. However, it was found in [5] that the optimization of structural parameter can promote the velocity and thrust properties, in which the essence problem is the elimination of higher harmonics in the Fig.…”
Section: Introductionmentioning
confidence: 61%
“…It must be recalculated when other parameters have been changed. The influences of gap length, thickness of magnet, pole arc coefficient, number of pole pairs to the average thrust have been already discussed for a double-sided linear synchronous motor used for electromagnetic catapults in [3], and some results are consistent with the computed results in [4]. However, it was found in [5] that the optimization of structural parameter can promote the velocity and thrust properties, in which the essence problem is the elimination of higher harmonics in the Fig.…”
Section: Introductionmentioning
confidence: 61%
“…A small air gap between the PM and the EM is effective for achieving a large thrust and high thrust density [31]. However, this makes it difficult to assemble the motor and increases the risk of contact between the PM and the EM.…”
Section: Effect Of Em and Pm Dimensions On Thrust And Thrust Denmentioning
confidence: 99%
“…[1]- [3]. Particular examples include transportation and electromagnetic launch (EML) [4], [5]. In comparison to their rotary-to-linear counterparts, the PMLM offer significant advantages, notably the absence of mechanical gears and transmission systems, which results in a higher efficiency, better dynamic performance, and improved reliability.…”
Section: Introductionmentioning
confidence: 99%