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基于组合频响函数的动力总成刚体模态参数识别
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  • 英文篇名:Powertrain Rigid Modal Parameter Identification Based on Combined Frequency Response Function
  • 作者:费振南 ; 范让林 ; 张楚源 ; 屈少举 ; 宋鹏俊
  • 英文作者:Fei Zhennan;Fan Ranglin;Zhang Chuyuan;Qu Shaoju;Song Pengjun;School of Mechanical Engineering, University of Science and Technology Beijing;Dongfeng Motor Corporation Technical Center;
  • 关键词:动力总成 ; 刚体模态参数识别 ; 组合频响函数
  • 英文关键词:Powertrain;;Rigid body modal parameters identification;;Combined frequency response function
  • 中文刊名:QCJS
  • 英文刊名:Automobile Technology
  • 机构:北京科技大学机械工程学院;东风汽车公司技术中心;
  • 出版日期:2019-05-10 17:03
  • 出版单位:汽车技术
  • 年:2019
  • 期:No.524
  • 基金:国家自然科学基金资助项目(51175034)
  • 语种:中文;
  • 页:QCJS201905015
  • 页数:5
  • CN:05
  • ISSN:22-1113/U
  • 分类号:62-66
摘要
动力总成刚体模态是悬置系统设计的重要参数,为得到完整6阶刚体模态参数,阐述了基于组合频响函数的动力总成刚体模态试验与参数识别流程,并组合不同单激励点模态试验的频响函数结果进行参数识别。经模态置信矩阵检测,组合频响函数识别结果的模态振型正交性良好,不同组间模态频率稳定且模态振型一致。在准确测量动力总成刚体动力学参数和悬置三向动刚度的基础上,建立了含抗扭杆的动力总成-悬置系统12自由度刚体模态仿真模型。试验与仿真结果表明,两者模态频率吻合良好且主振动方向完全一致,即通过不同激励点的组合频响函数识别6阶刚体模态的方法与流程可行且准确。
        The rigid modal parameters are essential to the design of powertrain mounting system. In order to obtain the complete 6-order rigid modal parameters, the powertrain rigid modal experiment and parameter identification process are elaborated based on combined frequency response function. And the parameters are identified by combining the frequency function results of modal experiment at different single excitation points. Modal assurance criterion shows the modal shapes from the combined frequency response function identification results are orthogonal, the modal frequencies from different combinations are stable and the modal shapes are consistent. Based on the accurate measurement of powertrain rigid body dynamic parameters and dynamic stiffness of mounts in three directions, the 12-DOFs rigid modal model for powertrain mounting system with torque-struct is established and simulated. Experiment and simulation modal frequencies are in good agreement and the main vibration direction is identical, so it can be concluded that the 6-order rigid modal parameter identification by the combined frequency response function of different excitation points is feasible,and the results are accurate.
引文
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