二维码(扫一下试试看!) | 典型薄膜空间结构耦合动力学仿真分析 | Coupling Dynamics Simulation Analysis for Typical Membrane Space Structures | 投稿时间:2017-02-17 | DOI:10.15918/j.tbit1001-0645.2018.04.003 | 中文关键词:薄膜结构耦合动力学仿真分析 | English Keywords:membrane structurecoupling dynamicssimulation analysis | 基金项目:民用航天"十三五"预研项目(D020205) | | 摘要点击次数:882 | 全文下载次数:661 | 中文摘要: | 对典型薄膜空间结构运动过程进行动力学仿真,通过有限元仿真计算求解薄膜空间结构运动过程的动力学响应,分析结构展开过程的构型变化、应力分布情况;通过分析薄膜空间结构系统动能变化研究其运动过程及展开稳定性问题.利用非线性有限元软件SAMCEF Mecano对自碰撞、矩形展开和弹性气球充气扩展3种典型薄膜空间结构进行有限元建模,通过定义薄膜与薄膜的自接触、薄膜与柔性结构接触完成耦合状态下的数值仿真运算.仿真结果表明,运用SAMCEF Mecano可以实现薄膜空间结构典型运动方式的耦合动力学仿真分析;薄膜空间结构动力学特性受不同运动方式影响;薄膜结构展开速率越小其展开稳定性越好. | English Summary: | A dynamics simulation of the motion process of typical membrane space structures was made, and the dynamic response in the motion process of membrane space structures was solved by the finite element method to analyze the configuration transformation and the stress distribution in the deployable process. The motion process and the deployment stability of membrane space structures was studied by analyzing the system kinetic energy change of membrane space structures. The finite element models of typical membrane space structures, which included self-collision, rectangle deployment and inflatable balloon extension, were established by SAMCEF Mecano and then the numerical simulation based on coupling method was completed by defining the self-contact of membrane structures and the contact between membrane structures and flexible structures. The simulation results show that coupling dynamic simulation of typical membrane space structures is reliable by using SAMCEF Mecano. The dynamic properties are effected by different motion modes and the deployment stability is better when deployment rate is lower. | 查看全文查看/发表评论下载PDF阅读器 | |
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