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基于Simcenter 3D的液压升降台刚柔耦合仿真

Rigid-Flexible Coupling Simulation of Hydraulic Lifting Platform Based on Simcenter 3D
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摘要 根据某项目需求,需设计一台液压升降台。为保证该设计方案可行性和安全性,需对设计方案进行仿真验证。采用刚体动力学仿真及有限元分析技术,从多角度对模型转台关键机构进行仿真计算模拟,得到各构件的运动数据及受力特性,确保该升降台机构设计方案的可行性和安全性。借助西门子Simcenter 3D仿真平台建立升降台动力学仿真模型,以实际负载和运行速度为边界条件,对模型进行充分计算。对升降台关键部位进行柔性体设置,创建动态耦合模型,对薄弱部位仿真分析,计算刚度与强度校核,为驱动部件选型以及薄弱点改进设计提供参考依据。 According to the demand of a project,we need to design a hydraulic lifting platform.In order to ensure the feasibility and safety of the design scheme,the design scheme needs to be verified by simulation.By adopting the rigid body dynamics simulation and finite element analysis technology,the key mechanism of the model turntable is simulated from multiple angles,and the motion data and force characteristics of each component are obtained to ensure the feasibility and safety of the design scheme of the lifting platform mechanism.With the help of Siemens SimCenter3D simulation platform,the dynamic simulation model of lifting platform was established,and the actual load and running speed were taken as boundary conditions to fully calculate the model.The key parts of the lifting platform were set up with flexible body,the dynamic coupling model was created,the weak parts were simulated and analyzed,and the stiffness and strength were calculated to provide a reference for the selection of driving parts and the improvement of the design of weak points.
作者 王鹏飞 吴文超 陈一凡 王淑秀 叶敏 王瑞 Wang Pengfei;Wu Wenchao;Chen Yifan;Wang Shuxiu;Ye Min;Wang Rui(Shanghai Aircraft Design and Research Institute,Shanghai,200090,China)
出处 《仪器仪表用户》 2021年第9期23-26,97,共5页 Instrumentation
基金 上海市高端智能装备首台突破专项(ZB-ZBST-01-20-0090)。
关键词 液压升降台 多体动力学 刚柔耦合 模拟仿真 hydraulic lifting platform multibody dynamics rigid-flexible coupling simulation
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  • 1廉自生,刘楷安.虚拟样机中的柔性化方法分析[J].煤矿机械,2005,26(4):59-61. 被引量:8
  • 2邓宏光,孙大刚,游思坤,王海滨.剪叉式升降平台建模及关键参数研究[J].机电工程技术,2005,34(7):20-22. 被引量:33
  • 3Trauis Langbecker. Kinematic Analysis of Deployable Scissor Structures [J]. International Journal of Space Structures (S0266-3511), 1999, 14(1): 1-15.
  • 4B P Nagaraj. Kinematics of Pantograph Masts [J]. Mechanism and Machine Theory (S0094-114X), 2009, 44(4): 822-834.
  • 5Zhao Jingshan. The Mechanism Theory and Application of Deployable Structure Based on SLE [J]. Mechanism and Machine Theory (S0094-114X), 2009, 44(2): 324-335.
  • 6V I Dranovskii. On the Dynamics of Deployment of an Orbital Structure with Elastic Elements [J]. International Applied Mechanics (S1063-7095), 2006, 42(8): 959-965.
  • 7Liu Tao. Simulative Calculation and Optimal Design of Scissor Lifting Mechanism [C]// 2009 Chinese Control and Decision Conference. Guilin, China, 2009: 2079-2082.
  • 8H Spackman. Mathematical Analysis of Actuator Forces in a Scissor Lift [R]. USA: Naval Command, Control and Ocean Surveillance Center, 1994: 2-14.
  • 9GB/T2348-93液压气动系统及元件缸内径及活塞杆外径[S].
  • 10张志涌 等.精通Matlab 6.5版[M].北京:北京航空航天出版社,2003..

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