首页> 外文期刊>IEEE Transactions on Plasma Science >The Experimental Test Results of a Two-Section Linear Induction Launcher
【24h】

The Experimental Test Results of a Two-Section Linear Induction Launcher

机译:两段线性感应发射器的实验测试结果

获取原文
获取原文并翻译 | 示例

摘要

A linear induction launcher (LIL) is an air-cored coilgun. Its barrel consists of an array of cylindrical drive coils and the barrel can be a single section or divided into several sections. A single-section barrel can be easily driven by energizing the coils in a polyphase fashion to accelerate the moving part of the LIL, the projectile. A multisection barrel, on the other hand, offers higher muzzle velocities for the projectile. From breech to muzzle, each section is energized with an increasing frequency. However, several problems arise when a multisection barrel is used. Some of them are currently reported in the literature. For example, a retarding force on the projectile has been observed while the projectile passes from one section to another. The initial position of the projectile also affects the launching performance. Some experiments can be useful to determine the optimum conditions to reach maximum possible muzzle velocity. This article concerns the design, implementation, and experimental test of a laboratory-scale, two-section LIL to examine the effects of various parameters on the launching performance.
机译:线性感应发射器(LIL)是一种空气芯线圈。其桶由圆柱形驱动线圈阵列组成,筒可以是单个部分或分成几个部分。通过在多相方式中激励线圈可以容易地驱动单个镜筒,以加速LIL的移动部分,射弹。另一方面,多极体桶为射弹提供更高的枪口速度。从臀位到枪口,每个部分都随着频率的增加而通电。然而,当使用多分钟筒时出现了几个问题。其中一些目前在文献中报告。例如,已经观察到射弹上的延迟力,而射弹从一个部分转到另一个部分。射弹的初始位置也会影响发射性能。一些实验可用于确定最佳条件以达到最大可能的枪口速度。本文涉及实验室规模的设计,实施和实验测试,两节LIL检查各种参数对发射性能的影响。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号