[外文翻譯]電磁飛機(jī)彈射系統(tǒng)的設(shè)計(jì)與仿真/Design and Simulation of an Electromagnetic Aircraft Launch System
內(nèi)包含中文翻譯和英文原文，內(nèi)容完善，建議下載閱覽。

①中文頁數(shù)7

中文字?jǐn)?shù)3227

②英文頁數(shù)6

英文字?jǐn)?shù)2176

③ 摘要
本文利用有限元分析（FEA）介紹了電磁飛機(jī)彈射系統(tǒng)的設(shè)計(jì)、優(yōu)化和驗(yàn)證，并且利用虛擬仿真試驗(yàn)臺（VTB）實(shí)現(xiàn)實(shí)時(shí)仿真。該試驗(yàn)臺為未來航空母艦的電磁飛機(jī)彈射系統(tǒng)（EMALS）提供一系列備選線性電機(jī)。提出了基本機(jī)器類型的選擇和基本尺寸的確定步驟。提出了一種永磁體結(jié)構(gòu)的詳細(xì)設(shè)計(jì)，介紹了一種勵(lì)磁線圈和感應(yīng)電機(jī)類型。討論了長定子-短動(dòng)子的幾何尺寸，特別是提出這個(gè)幾何尺寸對電力電子驅(qū)動(dòng)系統(tǒng)的相關(guān)影響。

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

④關(guān)鍵字 Electromagnetic