Design and simulation of a permanent-magnet electromagnetic aircraft launcher

被引：51

作者：

Patterson, D ^{[1
]}

Monti, A

Brice, CW

Dougal, RA

Pettus, RO

Dhulipala, S

Kovuri, DC

Bertoncelli, T

机构：

[1] Univ Nebraska, Dept Elect Engn, Lincoln, NE 68588 USA

[2] Univ S Carolina, Dept Elect Engn, Columbia, SC 29208 USA

[3] Politecn Milan, Dipartimento Elettrotecn, I-20133 Milan, Italy

来源：

IEEE TRANSACTIONS ON INDUSTRY APPLICATIONS | 2005年 / 41卷 / 02期

关键词：

aircraft launcher; linear machine; linear permanent-magnet (PM) synchronous machine; PM machine; power electronic drive; system simulation; track sectioning;

D O I：

10.1109/TIA.2005.844404

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

This paper describes the basic design, refinement, and verification using finite-element analysis, and operational simulation using the Virtual Test Bed, of a linear machine for an electromagnetic aircraft launcher, for the aircraft carrier of the future. Choices of basic machine format and procedures for determining basic dimensions are presented. A detailed design for a permanent-magnet version is presented, and wound-field coil and induction machine versions are briefly discussed. The long armature-short field geometry is justified, and in particular the impact of this geometry on the scale of the power electronic drive system is examined.

引用

页码：566 / 575

页数：10

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