摘要
针对空间挠性桁架的低频振动抑制问题,提出串联松弛型阻尼器的方案。建立集成松弛型阻尼器的桁架结构有限元模型,通过仿真分析机动工况和稳态工况下采用阻尼器抑制桁架结构振动的效果,研究阻尼器参数以及布局对振动抑制效果的影响,获取阻尼器的最佳参数值及安装位置。结果表明安装阻尼器后,机动工况下桁架末端位移幅值10 s内衰减70%以上,稳态工况下共振峰降低80%以上,抑制振动效果较好。该研究为大型挠性部件的振动抑制提供新的思路,对实际工程具有指导意义。
Aiming at the problem of low frequency vibration suppression of space flexible truss of satellites,the scheme of installing relaxation dampers was proposed.A finite element model of the truss structure with relaxation dampers was established,and the satellite maneuvering conditions and steady-state conditions were simulated.The influence of the damper parameters and layout on the vibration suppression effect of the truss was studied.The optimum parameters and installation position of dampers were obtained.The results show that with relaxation dampers installed,the displacement amplitude of truss end under maneuvering conditions was attenuated by more than 70 % within 10 s,the resonance peak under steady-state conditions was reduced by 80 %.Relaxation damper has a great vibration suppression effect for low frequency vibration of truss structure.The damping coefficient,stiffness,and stiffness ratio of the relaxation damper have obvious impact on the low-frequency vibration suppression effect.This work provides a new idea for the vibration suppression of large flexible components and has a guiding significance for actual engineering.
作者
朱琛
周晓东
刘兴天
赵枝凯
赵发刚
ZHU Chen;ZHOU Xiaodong;LIU Xingtian;ZHAO Zhikai;ZHAO Fagang(Shanghai Institute of Satellite Engineering,Shanghai 201109,China;Shanghai Aerospace Equipment Micro-vibration Environment Simulation Engineering Technology Research Center,Shanghai 201109,China;Shanghai Academy of Spaceflight Technology,Shanghai 201109,China)
出处
《噪声与振动控制》
CSCD
北大核心
2022年第6期31-37,共7页
Noise and Vibration Control
基金
国家自然科学基金面上资助项目(51875363)。
关键词
振动与波
松弛型阻尼
桁架结构
低频振动
振动抑制
最优阻尼
vibration and wave
relaxation damper
truss structure
low frequency vibration
vibration suppression
optimal damping