弹炮一体武器平台导弹发射架缓冲机构设计  

Design of Buffer Mechanism for Missile Launcher of Missile and Artillery Integrated Weapon Platform

作　　者：姚新科 张庆辉 徐宏斌[1] 李辉[1] 程伟峰 YAO Xinke;ZHANG Qinghui;XU Hongbin;LI Hui;CHENG Weifeng(Xi’an Modern Control Technology Research Institute,Xi’an 710065,China)

机构地区：[1]西安现代控制技术研究所,西安710065

出　　处：《弹箭与制导学报》2020年第4期136-139,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对弹炮一体武器平台炮射冲击影响导弹系统工作稳定性的问题,设计了导弹发射架缓冲机构。通过对原导弹发射架火炮射击振动试验测试数据的分析,设计了金属丝网三向隔振缓冲机构,并在冲击振动台上进行了摸底和试验验证。结果表明,导弹发射架缓冲机构有效降低了火炮射击振动对导弹的冲击载荷,使加速度峰值、导弹轴线精度满足设计要求,且电子弹性能正常。Aiming at the problem that the artillery fire impact on the missile and artillery integrated weapon platform effected the working stability of the missile system,a buffer mechanism of the missile launcher was designed.Based on the analysis of the test data onto firing vibration test for the artillery with the original missile launcher,a wire mesh three-way vibration isolation and buffer mechanism were designed,which was tested and verified on the impact vibration platform.The results show that the buffer mechanism of the missile launcher can effectively reduce the impact load of the missile,make the peak acceleration and the precision of the missile axis meet the design requirements,and the electronic missile performance works well.

关 键 词：弹炮一体 缓冲机构 冲击 振动 

分 类 号：TJ410.3[兵器科学与技术—火炮、自动武器与弹药工程] TJ768.2