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

机译:基于双面管状直线感应电动机的EMALS优化设计

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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.
机译:基于双面管状线性感应电动机,一种新颖的进化算法用于优化电磁飞机发射系统各阶段的推力。半分析模型可以快速准确地预测设备中的所有电磁量,包括推力,反电动势,感应电流密度的分布以及牙齿中的平均磁通密度。使用半分析公式,可以大大简化机器的特性,从而可以快速评估成本函数和设计约束。

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