Accelerating thick aluminum liners using pulsed powers

G. Kyrala, J. Hammerberg, R. Bowers, D. Morgan, J. Stokes, J. Cochrane, W. Anderson
{"title":"Accelerating thick aluminum liners using pulsed powers","authors":"G. Kyrala, J. Hammerberg, R. Bowers, D. Morgan, J. Stokes, J. Cochrane, W. Anderson","doi":"10.1109/PPC.1999.823654","DOIUrl":null,"url":null,"abstract":"The authors have investigated the acceleration of very thick cylindrical aluminum liners using the Pegasus II capacitor bank. These accelerated solid liners will be used to impact other objects at velocities below 1.5 km/sec, allowing them to generate and sustain shocks of a few 100 kilobar for a few microseconds. A cylindrical shell of 1100 series aluminum with an initial inner radius of 23.61 mm, an initial thickness of 3.0 mm, and a height of 20 mm, was accelerated using a current pulse of 7.15 MA peak current and a 7.4 microsecond quarter cycle time. The aluminum shell was imploded within confining copper glide planes with decreasing separation with an inward slope of 8 degrees. At impact with a cylindrical target of diameter 3-cm, the liner was moving at 1.4 km/sec and its thickness increased to 4.5 mm. Radial X-ray radiograms of the liner showed both the liner and the glide plane interface. The curvature of the inner surface of the liner was measured before impact with the 15-mm radius target. The radiograms also showed that the copper glide planes distorted as the liner radius decreased and that some axial stress is induced in the liner. The axial stresses did not affect the inner curvature significantly. Post-shot calculations of the liner behavior indicated that the thickness of the glide plane played a significant role in the distortion of the interface between the liner and the glide plane.","PeriodicalId":11209,"journal":{"name":"Digest of Technical Papers. 12th IEEE International Pulsed Power Conference. (Cat. No.99CH36358)","volume":"70 1","pages":"872-875 vol.2"},"PeriodicalIF":0.0000,"publicationDate":"1999-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Digest of Technical Papers. 12th IEEE International Pulsed Power Conference. (Cat. No.99CH36358)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PPC.1999.823654","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

The authors have investigated the acceleration of very thick cylindrical aluminum liners using the Pegasus II capacitor bank. These accelerated solid liners will be used to impact other objects at velocities below 1.5 km/sec, allowing them to generate and sustain shocks of a few 100 kilobar for a few microseconds. A cylindrical shell of 1100 series aluminum with an initial inner radius of 23.61 mm, an initial thickness of 3.0 mm, and a height of 20 mm, was accelerated using a current pulse of 7.15 MA peak current and a 7.4 microsecond quarter cycle time. The aluminum shell was imploded within confining copper glide planes with decreasing separation with an inward slope of 8 degrees. At impact with a cylindrical target of diameter 3-cm, the liner was moving at 1.4 km/sec and its thickness increased to 4.5 mm. Radial X-ray radiograms of the liner showed both the liner and the glide plane interface. The curvature of the inner surface of the liner was measured before impact with the 15-mm radius target. The radiograms also showed that the copper glide planes distorted as the liner radius decreased and that some axial stress is induced in the liner. The axial stresses did not affect the inner curvature significantly. Post-shot calculations of the liner behavior indicated that the thickness of the glide plane played a significant role in the distortion of the interface between the liner and the glide plane.
使用脉冲功率加速厚铝衬垫
作者研究了使用Pegasus II电容器组的极厚圆柱形铝衬垫的加速度。这些加速固体衬垫将用于以低于1.5公里/秒的速度撞击其他物体,使它们能够在几微秒内产生并承受100千巴的冲击。采用峰值电流为7.15 MA、周期为7.4微秒的四分之一周期脉冲,对初始内半径为23.61 mm、初始厚度为3.0 mm、初始高度为20 mm的1100系列铝圆柱壳进行加速。铝壳在受限的铜滑面内内爆,分离减小,向内倾斜8度。当撞击直径为3厘米的圆柱形目标时,衬垫以1.4公里/秒的速度移动,厚度增加到4.5毫米。衬板的x射线放射图显示衬板和滑面界面。用半径为15mm的靶撞击前测量了衬垫内表面的曲率。射线图还显示,随着衬板半径的减小,铜的滑动面发生了畸变,并在衬板内产生了一定的轴向应力。轴向应力对内曲率影响不显著。弹后计算表明,滑面厚度对滑面与衬板界面的变形有重要影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信