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柔性联轴器平行不对中轴系振动特性分析

赵博 谷伟伟 潘渤 王延博

赵博,谷伟伟,潘渤, 等. 柔性联轴器平行不对中轴系振动特性分析[J]. 机械科学与技术,2022,41(11):1693-1697 doi: 10.13433/j.cnki.1003-8728.20200555
引用本文: 赵博,谷伟伟,潘渤, 等. 柔性联轴器平行不对中轴系振动特性分析[J]. 机械科学与技术,2022,41(11):1693-1697 doi: 10.13433/j.cnki.1003-8728.20200555
ZHAO Bo, GU Weiwei, PAN Bo, WANG Yanbo. Vibration Characteristics Analysis of Rotor System with Flexible Coupling Parallel Misalignment[J]. Mechanical Science and Technology for Aerospace Engineering, 2022, 41(11): 1693-1697. doi: 10.13433/j.cnki.1003-8728.20200555
Citation: ZHAO Bo, GU Weiwei, PAN Bo, WANG Yanbo. Vibration Characteristics Analysis of Rotor System with Flexible Coupling Parallel Misalignment[J]. Mechanical Science and Technology for Aerospace Engineering, 2022, 41(11): 1693-1697. doi: 10.13433/j.cnki.1003-8728.20200555

柔性联轴器平行不对中轴系振动特性分析

doi: 10.13433/j.cnki.1003-8728.20200555
基金项目: 中国华能集团有限公司总部科技项目( HNKJ21-H59 )
详细信息
    作者简介:

    赵博(1989−),工程师,硕士,研究方向为转子动力学及旋转机械振动故障诊断,zhaoboj@tpri.com.cn

  • 中图分类号: O347.6;TH113

Vibration Characteristics Analysis of Rotor System with Flexible Coupling Parallel Misalignment

  • 摘要: 考虑联轴器弯曲、扭转和横向柔度的影响,分析了转子轴承系统在联轴器平行不对中情况下的振动特性。计及转子的径向位移、偏转角和扭转角自由度,并考虑轴承特性的各向异性,利用各自由度之间的耦合关系,通过第二类拉格朗日方程建立了平行不对中多转子系统的动力学控制方程。通过数值方法求解非线性方程,得到了稳定运行时转子振动的时域波形、频谱及轴心轨迹。平行不对中程度对振动的影响分析表明,在实际可能发生的平行不对中量级下,即不对中量与转子长度之比小于10−3时,横向振动始终以基频分量为主,扭转振动有明显的二倍频分量,未表现出明显的非线性特性。
  • 图  1  联轴器平行不对中轴系模型示意图

    图  2  被驱动转子转速变化趋势

    图  3  进入稳态后转子扭转振动频谱

    图  4  进入稳态后转子轮盘处X方向和Y方向横向振动波形

    图  5  进入稳态后转子轮盘处X方向振动频谱

    图  6  进入稳态后转子在轮盘处的轴心轨迹

    图  7  不同不对中程度下转子横向和扭转振动幅值

    图  8  不同联轴器刚度下转子横向和扭转振动幅值

    表  1  转子系统参数

    部件参数数值
    联轴器等效扭转刚度$ {k_{cr}} $102 N·m/rad
    等效弯曲刚度$ {k_{cb}} $10 N·m/rad
    等效横向刚度$ {k_{ct}} $105 N/m
    平行不对中量$ \delta $1×10−3 m
    轴承X方向刚度$ {k_x} $106 N/m
    Y方向刚度$ {k_y} $1.5×106 N/m
    X方向阻尼$ {C_x} $0.1 N·s/m
    Y方向阻尼$ {C_y} $0.1 N·s/m
    转子集中质量m1.2 g
    极转动惯量$ {I_{p1}} $、$ {I_{p2}} $1.125×10−3 kg·m3
    直径转动惯量$ {I_{d2}} $5.625×10−4 kg·m3
    轴承间距$ l $0.6 m
    轮盘到半联轴器距离$ {l_c} $0.1 m
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-02-28
  • 刊出日期:  2023-02-04

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