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发射井内弹-筒系统抗爆减震设计
引用本文:周岸峰,郭振,李道奎,周仕明,姜人伟.发射井内弹-筒系统抗爆减震设计[J].国防科技大学学报,2023,45(1):102-109.
作者姓名:周岸峰  郭振  李道奎  周仕明  姜人伟
作者单位:国防科技大学 空天科学学院, 湖南 长沙 410073;空天任务智能规划与仿真湖南省重点实验室, 湖南 长沙 410073;中国运载火箭技术研究院 北京宇航系统工程研究所, 北京 100076;国防科技大学 空天科学学院, 湖南 长沙 410073;中国运载火箭技术研究院 北京宇航系统工程研究所, 北京 100076
基金项目:湖南省自然科学基金资助项目(2021JJ30770)
摘    要:为提高井下冷发射导弹的生存能力,对其开展了抗爆减震设计研究,建立了弹-筒系统在不同减震方式下的有限元仿真模型,计算了弹-筒系统在爆炸地冲击作用下的动态响应,比较了悬吊式、下支承式、斜吊式等多种减震系统的减震效果,并分析了减震器刚度和阻尼对减震效果的影响。结果表明:悬吊式减震系统的减震效果略好于下支承式,斜吊式最差,合理减小减震器刚度和阻尼可以明显提升悬吊式减震系统的减震效果。

关 键 词:发射井  弹-筒系统  有限元  爆炸地冲击  减震系统
收稿时间:2020/12/30 0:00:00

Blast resistant and shock absorption design for missile-canister system in silo
ZHOU Anfeng,GUO Zhen,LI Daokui,ZHOU Shiming,JIANG Renwei.Blast resistant and shock absorption design for missile-canister system in silo[J].Journal of National University of Defense Technology,2023,45(1):102-109.
Authors:ZHOU Anfeng  GUO Zhen  LI Daokui  ZHOU Shiming  JIANG Renwei
Institution:College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions, Changsha 410073, China;Beijing Institute of Astronautical Systems Engineering, China Academy of Launch Vehicle Technology, Beijing 100076, China; College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China;Beijing Institute of Astronautical Systems Engineering, China Academy of Launch Vehicle Technology, Beijing 100076, China
Abstract:To improve the survival ability of cold launch missile in silo, the research on blast resistant and shock absorption design had been performed. Finite element models were established for missile-canister system in different shock absorption ways. The dynamic responses under blast-induced ground shock were calculated. The vibration reducing performances of several shock absorption systems were compared, including vertical suspension mode, lower supporting mode and slant suspension mode. Meanwhile, the influences of stiffness and damping on the shock absorbing performance were investigated. The results show that the vibration reducing performance of vertical suspension mode is slightly better than that of lower supporting mode, and that of slant suspension mode is worst. The vibration reducing performance of vertical suspension shock absorption system can be significantly improved by properly decreasing its stiffness and damping.
Keywords:silo  missile-canister system  finite element  blast-induced ground shock  shock absorption system
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