空间可展开天线支撑结构热致振动与抑制OA
Thermally induced vibration and suppression of space deployable antenna support structures
针对在进出地球阴影时,空间可展开天线支撑结构在循环动态温度载荷下产生热致变形,诱发结构振动问题,建立了结构动力学模型,给出了复合材料杆件等效热力学材料参数,开展了热致振动响应分析.给出了被动式非线性黏性阻尼器(PNVD)的设计和非线性流体阻尼表达式,提出了一种基于非线性流体阻尼的空间可展开天线支撑桁架结构热致振动抑制方法.空间可展开天线支撑结构模态阻尼试验结果表明,安装阻尼器前后,结构基频变化不大于1%,模态阻尼比提升大于2%.
A structural dynamics model was established to address the issue of thermal deformation and structural vi-bration of large space deployable antenna support structures under cyclic dynamic temperature loads when entering and exiting the Earth's shadow.Equivalent thermodynamic material parameters of composite material members were provided,and thermal vibration response analysis was conducted.The nonlinear fluid damping model of Passive Non-linear Viscous Damper(PNVD)is presented,and a spatially deployable antenna support truss structure thermal vibra-tion suppression method based on nonlinear fluid damping is proposed.The experimental results of modal damping of large deployable antenna support structures show that before and after installing dampers,the fundamental frequency of the structure changes by no more than 1%,and the modal damping ratio increases by more than 2%.
罗成;林贵平;罗敏;郭元东
北京航空航天大学 航空科学与工程学院,北京 100191北京航空航天大学 航空科学与工程学院,北京 100191北京空间飞行器总体设计部,北京 100094北京航空航天大学 航空科学与工程学院,北京 100191
航空航天
空间可展开天线热致振动非线性阻尼振动抑制航天器
space deployable antennathermally induced vibrationnonlinear dampingvibration suppressionspacecraft
《航空学报》 2026 (14)
76-84,9
国家级项目 National Level Project
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