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Design Optimization of Reluctance-Synchronous Linear Machines for Electromagnetic Aircraft Launch System

This paper describes the design optimization and analysis of reluctance-synchronous linear motor with a solid or laminated moving part (secondary). The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the remova...

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Published in:IEEE transactions on magnetics 2009-01, Vol.45 (1), p.389-395
Main Authors: Mirzaei, M., Abdollahi, S.E.
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Language:English
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description This paper describes the design optimization and analysis of reluctance-synchronous linear motor with a solid or laminated moving part (secondary). The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the removal of permanent-magnet secondary and replacing it with a reluctance-type secondary. The first purpose of this paper is designing a reluctance-synchronous linear motor with the maximum-output thrust force and optimum power factor. In this model, a long primary (armature) and a short secondary are evaluated. Distributed winding is considered for design and analysis. Finally, air-gap winding configuration is evaluated.
doi_str_mv 10.1109/TMAG.2008.2008977
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subjects Aircraft components
Aircraft propulsion
Cross-disciplinary physics: materials science
rheology
Design and analysis
Design engineering
Design optimization
Electromagnetic analysis
Electromagnetic forces
electromagnetic launcher
Electromagnetic launching
Exact sciences and technology
Finite element methods
finite-element method
Magnetic flux
Magnetism
Materials science
Mathematical analysis
Mathematical models
Motors
Optimization
Other topics in materials science
Physics
Reactive power
reluctance-synchronous linear motor
Saturation magnetization
Synchronous motors
Winding
title Design Optimization of Reluctance-Synchronous Linear Machines for Electromagnetic Aircraft Launch System
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