弹体尾翼上下料专机结构设计分析  

Structural Design and Analysis of the Special Robot for Projectile Tail Wing Loading and Unloading

作　　者：董浩男 舒启林[2] Dong Haonan;Shu Qilin

机构地区：[1]沈阳理工大学机械工程学院,辽宁沈阳110159 [2]沈阳理工大学,辽宁沈阳110159

出　　处：《一重技术》2024年第6期15-18,31,共5页CFHI Technology

摘　　要：针对信息化战场中弹药的生产效率及安全问题,通过工业机器人代替人工完成弹体自动拧紧专机自动上、下料工作。设计满足生产需求的尾翼夹持机构,完成部件选型;通过改善布局,分析机械臂运动轨迹,求解正运动方程,以提高弹体生产效率和安全,为国防事业做出贡献。In view of the projectile production efficiency and safety issues related to the information battlefield,this paper carries out research on the special automatic tightening industrial robots for replacement of manual works by applying automatic projectile body loading and unloading methods.This study has designed the tail wing clamping mechanism that meets the production requirement,and completed component selection;at the same time,by improving structural configuration,analyzing the motion trail of the robot arm and solving the position motion equation,improvement has been made on efficiency and safety of projectile production,thus makes contribution to the national defense industry.

关 键 词：工业机器人 自动上下料 夹持机构 运动轨迹 

分 类 号：TJ410.5[兵器科学与技术—火炮、自动武器与弹药工程]