导弹与制导技术

地空导弹多极矩电磁发射器设计

  • 薛新鹏 ,
  • 舒涛 ,
  • 杨志勇 ,
  • 冯刚
展开
  • 空军工程大学防空反导学院,西安 710051

薛新鹏(1992-),男,黑龙江双鸭山人,硕士研究生,研究方向:电磁发射技术。

收稿日期: 2016-04-04

  网络出版日期: 2025-05-23

Design of Multipole Electromagnetic Emitter for Surface-to-air Missile

  • XUE Xinpeng ,
  • SHU Tao ,
  • YANG Zhiyong ,
  • FENG Gang
Expand
  • Air and Missile Defense College, Air Force Engineering University, Xi'an 710051, China

Received date: 2016-04-04

  Online published: 2025-05-23

摘要

针对如何提高地空导弹初始发射速度和战场隐蔽性的问题,设计了一种新型地空导弹多极矩电磁发射器。多极矩电磁发射器的结构装置为弹射线圈产生电磁弹射力,多极矩线圈来产生持续轴向加速力,以单级六极矩线圈为例,采用电磁场有限元方法进行发射过程仿真并提出了该发射器的设计流程。以某型地空导弹的发射性能为指标,根据建立的发射器原理和仿真模型计算得出了该发射器的线圈和电路参数,实现了地空导弹多极矩电磁发射器的设计。

本文引用格式

薛新鹏 , 舒涛 , 杨志勇 , 冯刚 . 地空导弹多极矩电磁发射器设计[J]. 弹箭与制导学报, 2017 , 37(2) : 27 -31 . DOI: 10.15892/j.cnki.djzdxb.2017.02.007

Abstract

In order to improve the initial emission velocity and the battlefield concealment of surface-to-air missile, a new type of multipole electromagnetic emitter for surface-to-air missile was designed. The structural device of multipole electromagnetic launcher produced electromagnetic ejection force for the ejection coil, and the multipole coil was used to generate a continuous axial accelerating force. Taking a monopole six polar moment coil as an example, electromagnetic field finite element method was used to simulate the launching process and the design procedure of the launcher was proposed. Taking the emission performance of a certain type of surface-to-air missile as the index, according to the principle of emitter and the simulation model to calculate the coil and the circuit parameters of the emitter, the design of multipole electromagnetic launcher of surface-to-air missile was realized.

参考文献

[1]
ZHU Y W, WANG Y, YAN Z M, et al. Multipole field electromagnetic launcher[J]. IEEE Transactions on Magnetics, 2010, 46 (7): 2622- 2627.
[2]
王豫, 罗文博, 严仲明,等. 多极矩电磁发射技术研究进展[J]. 计算机仿真, 2014, 30 (4): 1165- 1172.
[3]
罗文博. 多极矩电磁发射系统优化设计与实验研究[D]. 成都: 西南交通大学, 2014: 8- 41.
[4]
邹本贵, 孙学锋, 曹延杰,等. 舰载导弹电磁线圈垂直发射方案设计[J]. 弹箭与制导学报, 2013, 33 (5): 45- 48.
[5]
ZHU Y W, WANG Y, CHEN W R, et al. Analysis and evaluation of three-stage twisty octapole field Electromagnet-ic launcher[J]. IEEE. Transactions on Plasma Science, 2012, 40 (5): 1399-4406.
[6]
MUSOLINO A, RAUGI M, TELLINI B. 3-D field analysis in tubular induction launcher with armature transaction on verse motion[J]. IEEE Transactions on Magnetics, 1999, 35 (1): 154-4159.
[7]
朱英伟. 多极矩场电磁推进模式研究与系统设计[D]. 成都: 西南交通大学, 2011: 77- 80.
文章导航

/