{"title":"带尾端连接的旋转电枢结构设计及其电磁发射性能验证","authors":"Yong Liu;Tao Zhang;Kai Huang;Yanhui Chen;Wanying Wang;Wei Fan;Wei Guo","doi":"10.1109/TPS.2024.3475750","DOIUrl":null,"url":null,"abstract":"Electromagnetic-driven projectile spin launching technology is an important way to achieve high-precision firing in the railgun, but there is still a lack of sufficient research on the structural design of the tail-connected revolving armature and experimental verification of the spin launching performance. In this article, first, a structural design scheme of a revolving armature with a tail-end connection is established and compared with the conventional armature structural design scheme. Second, the finite element calculation model of interference assembly is adopted, and the influence law of the improved armature structure parameters on the initial mechanical performance is obtained. The theoretical calculation results show that the change of armature structural parameters has a great influence on the contact area and little influence on the maximum equivalent stress. The contact force decreases sharply with the increase of the interference position L2, throat radius r, and crack width \n<inline-formula> <tex-math>$c\\_w$ </tex-math></inline-formula>\n of the tail, and increases sharply with the increase of the tail thickness t and interference amount \n<inline-formula> <tex-math>$\\Delta $ </tex-math></inline-formula>\n. Finally, the electromagnetic launching experiments with different launching energies are carried out on test projectiles with conventional armature and tail-connected armature. The experimental results show that the revolving armature with a tail-end connection can effectively improve the rotation speed, but it will also have some negative effects on the muzzle velocity and the contact state between the armature and the rail in the bore.","PeriodicalId":450,"journal":{"name":"IEEE Transactions on Plasma Science","volume":"52 8","pages":"3335-3342"},"PeriodicalIF":1.3000,"publicationDate":"2024-10-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Structural Design of Revolving Armature With Tail End Connection and Its Electromagnetic Launching Performance Verification\",\"authors\":\"Yong Liu;Tao Zhang;Kai Huang;Yanhui Chen;Wanying Wang;Wei Fan;Wei Guo\",\"doi\":\"10.1109/TPS.2024.3475750\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Electromagnetic-driven projectile spin launching technology is an important way to achieve high-precision firing in the railgun, but there is still a lack of sufficient research on the structural design of the tail-connected revolving armature and experimental verification of the spin launching performance. In this article, first, a structural design scheme of a revolving armature with a tail-end connection is established and compared with the conventional armature structural design scheme. Second, the finite element calculation model of interference assembly is adopted, and the influence law of the improved armature structure parameters on the initial mechanical performance is obtained. The theoretical calculation results show that the change of armature structural parameters has a great influence on the contact area and little influence on the maximum equivalent stress. The contact force decreases sharply with the increase of the interference position L2, throat radius r, and crack width \\n<inline-formula> <tex-math>$c\\\\_w$ </tex-math></inline-formula>\\n of the tail, and increases sharply with the increase of the tail thickness t and interference amount \\n<inline-formula> <tex-math>$\\\\Delta $ </tex-math></inline-formula>\\n. Finally, the electromagnetic launching experiments with different launching energies are carried out on test projectiles with conventional armature and tail-connected armature. The experimental results show that the revolving armature with a tail-end connection can effectively improve the rotation speed, but it will also have some negative effects on the muzzle velocity and the contact state between the armature and the rail in the bore.\",\"PeriodicalId\":450,\"journal\":{\"name\":\"IEEE Transactions on Plasma Science\",\"volume\":\"52 8\",\"pages\":\"3335-3342\"},\"PeriodicalIF\":1.3000,\"publicationDate\":\"2024-10-23\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Plasma Science\",\"FirstCategoryId\":\"101\",\"ListUrlMain\":\"https://ieeexplore.ieee.org/document/10733837/\",\"RegionNum\":4,\"RegionCategory\":\"物理与天体物理\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"PHYSICS, FLUIDS & PLASMAS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Plasma Science","FirstCategoryId":"101","ListUrlMain":"https://ieeexplore.ieee.org/document/10733837/","RegionNum":4,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"PHYSICS, FLUIDS & PLASMAS","Score":null,"Total":0}
引用次数: 0
摘要
电磁驱动弹丸自旋发射技术是轨道炮实现高精度发射的重要途径,但目前在尾端连接旋转衔铁的结构设计和自旋发射性能的实验验证方面仍缺乏足够的研究。本文首先建立了尾端连接旋转电枢的结构设计方案,并与传统电枢结构设计方案进行了比较。其次,采用过盈装配的有限元计算模型,得出改进后的衔铁结构参数对初始机械性能的影响规律。理论计算结果表明,电枢结构参数的改变对接触面积影响较大,而对最大等效应力影响较小。接触力随尾部过盈位置 L2、喉管半径 r 和裂纹宽度 $c\_w$ 的增大而急剧减小,随尾部厚度 t 和过盈量 $\Delta $ 的增大而急剧增大。最后,对传统衔铁和尾部连接衔铁的试验弹进行了不同发射能量的电磁发射实验。实验结果表明,尾端连接的旋转衔铁能有效提高旋转速度,但也会对枪口速度和衔铁与枪膛内导轨的接触状态产生一些负面影响。
Structural Design of Revolving Armature With Tail End Connection and Its Electromagnetic Launching Performance Verification
Electromagnetic-driven projectile spin launching technology is an important way to achieve high-precision firing in the railgun, but there is still a lack of sufficient research on the structural design of the tail-connected revolving armature and experimental verification of the spin launching performance. In this article, first, a structural design scheme of a revolving armature with a tail-end connection is established and compared with the conventional armature structural design scheme. Second, the finite element calculation model of interference assembly is adopted, and the influence law of the improved armature structure parameters on the initial mechanical performance is obtained. The theoretical calculation results show that the change of armature structural parameters has a great influence on the contact area and little influence on the maximum equivalent stress. The contact force decreases sharply with the increase of the interference position L2, throat radius r, and crack width
$c\_w$
of the tail, and increases sharply with the increase of the tail thickness t and interference amount
$\Delta $
. Finally, the electromagnetic launching experiments with different launching energies are carried out on test projectiles with conventional armature and tail-connected armature. The experimental results show that the revolving armature with a tail-end connection can effectively improve the rotation speed, but it will also have some negative effects on the muzzle velocity and the contact state between the armature and the rail in the bore.
期刊介绍:
The scope covers all aspects of the theory and application of plasma science. It includes the following areas: magnetohydrodynamics; thermionics and plasma diodes; basic plasma phenomena; gaseous electronics; microwave/plasma interaction; electron, ion, and plasma sources; space plasmas; intense electron and ion beams; laser-plasma interactions; plasma diagnostics; plasma chemistry and processing; solid-state plasmas; plasma heating; plasma for controlled fusion research; high energy density plasmas; industrial/commercial applications of plasma physics; plasma waves and instabilities; and high power microwave and submillimeter wave generation.