Optimal Design of EMALS Based on a Double-Sided Tubular Linear Induction Motor

被引：24

作者：

Musolino, Antonino ^{[1
]}

Raugi, Marco ^{[1
]}

Rizzo, Rocco ^{[1
]}

Tucci, Mauro ^{[1
]}

机构：

[1] Univ Pisa, Dept Energy Syst Terr & Construct Engn, I-56126 Pisa, Italy

来源：

IEEE TRANSACTIONS ON PLASMA SCIENCE | 2015年 / 43卷 / 05期

关键词：

Electromagnetic analysis; induction accelerators; induction motors; linear motors; optimization methods; AIRCRAFT LAUNCH SYSTEM; ELECTROMAGNETIC LAUNCHER; MODEL;

D O I：

10.1109/TPS.2015.2413675

中图分类号：

O35 [流体力学]; O53 [等离子体物理学];

学科分类号：

070204 ; 080103 ; 080704 ;

摘要：

A novel evolutionary algorithm is used for the optimization of the thrust force of the stages of an electromagnetic aircraft launch system, based on a double-sided tubular linear induction motor. A semianalytical model allows for a fast and accurate prediction of all the electromagnetic quantities in the device, including the thrust force, the back electromotive force, the distribution of the induced current density, and the average magnetic flux density in the teeth. Using the semianalytical formulation, the characterization of the machine is greatly facilitated, so allowing a fast evaluation of the cost function and of the design constraints.

引用

页码：1326 / 1331

页数：6

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