兵工自动化2026，Vol.45Issue(4)：28-32,48,6.DOI:10.7690/bgzdh.2026.04.006
弹体尾翼自动拧紧专机的结构设计
Structure Design of Special Machine for Automatically Screwing Missile Body and Tail Wing
彭崇振 1舒启林 1金沣1
作者信息
- 1. 沈阳理工大学机械工程学院,沈阳 110158
- 折叠
摘要
Abstract
In order to solve the problem of huge demand and low production efficiency of ammunition,an automatic tightening device for ammunition is designed by taking the assembly of ammunition body and empennage as an example.The system includes the clamping structure of the empennage and the missile body,the tightening structure of the empennage,the control of the tightening torque,etc.The automatic tightening of the empennage of the missile body is realized through the PLC remote control.The results show that the device can make the automatic assembly of the projectile body and the empennage,ensure the assembly quality of the projectile body,reduce the error of manual operation,improve the production efficiency,and provide a new idea for the automatic assembly of ammunition,which is of great significance in military equipment.关键词
弹体装配/拧紧控制/结构设计Key words
missile body assembly/tightening control/structure design分类
军事科技引用本文复制引用
彭崇振,舒启林,金沣..弹体尾翼自动拧紧专机的结构设计[J].兵工自动化,2026,45(4):28-32,48,6.
