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高速柔性转子系统非线性振动响应特征分析

洪杰 于欢 肖森 马艳红

洪杰, 于欢, 肖森, 等 . 高速柔性转子系统非线性振动响应特征分析[J]. 北京航空航天大学学报, 2018, 44(4): 653-661. doi: 10.13700/j.bh.1001-5965.2017.0266
引用本文: 洪杰, 于欢, 肖森, 等 . 高速柔性转子系统非线性振动响应特征分析[J]. 北京航空航天大学学报, 2018, 44(4): 653-661. doi: 10.13700/j.bh.1001-5965.2017.0266
HONG Jie, YU Huan, XIAO Sen, et al. Nonlinear vibration response characteristics of high-speed flexible rotor system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 653-661. doi: 10.13700/j.bh.1001-5965.2017.0266(in Chinese)
Citation: HONG Jie, YU Huan, XIAO Sen, et al. Nonlinear vibration response characteristics of high-speed flexible rotor system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 653-661. doi: 10.13700/j.bh.1001-5965.2017.0266(in Chinese)

高速柔性转子系统非线性振动响应特征分析

doi: 10.13700/j.bh.1001-5965.2017.0266
基金项目: 

国家自然科学基金 51575022

详细信息
    作者简介:

    洪杰  男, 博士, 教授, 博士生导师。主要研究方向:航空发动机转子动力学、航空发动机整机动力学、旋转机械振动控制、智能结构与新型阻尼材料等

    马艳红  女, 博士, 教授, 博士生导师。主要研究方向:航空发动机整机动力学、旋转机械振动控制、智能结构与新型阻尼材料等

    通讯作者:

    马艳红, E-mail: mayanh2002@163.com

  • 中图分类号: V231.96

Nonlinear vibration response characteristics of high-speed flexible rotor system

Funds: 

National Natural Science Foundation of China 51575022

More Information
  • 摘要:

    针对高速柔性转子多支点支承的结构特点及转子动力特性设计的需要,分析松动支承对转子动力特性的影响,仿真研究得到多支点支承高速柔性转子系统的非线性振动响应特征。研究结果表明:工作在多阶临界转速以上的转子系统,存在松动支承时,工作中的柔性转子可能存在周期、拟周期、混沌运动。进而研究了松动支承位置、不平衡量、松动间隙等参数对多支点支承柔性转子振动响应的影响,分析结果为多支点支承高速柔性转子系统的动力学设计提供了理论方法。

     

  • 图 1  采用松动支承设计的多支点支承柔性转子模型

    Figure 1.  Multi-supported flexible rotor model with bearing looseness design

    图 2  加大油膜间隙的挤压油膜阻尼器转子模型

    Figure 2.  Model of SFD rotor system with increased oil film clearance

    图 3  多支点支承高速柔性转子系统力学模型

    Figure 3.  Mechanical model of multi-supported high-speed flexible rotor system

    图 4  振幅随转速变化的分岔图

    Figure 4.  Bifurcation diagram of vibration amplitude changing with rotational speed

    图 5  随转速变化的频域瀑布图

    Figure 5.  Waterfall curve of frequency domain changing with rotational speed

    图 6  2号支点位置转子的振动响应

    Figure 6.  Vibration response of rotor at position of Support 2

    图 7  轮盘1位置转子的振动响应

    Figure 7.  Vibration response of rotor at position of Disk1

    图 8  2号、4号支点采用松动支承设计的多支点支承柔性转子系统

    Figure 8.  Multi-supported flexible rotor system with bearing clearance designed at Support 2 and Support 4

    图 9  松动支承位置不同时2号支点振幅随转速变化的分岔图

    Figure 9.  Bifurcation diagram of vibration amplitude of Support 2 changing with rotational speed when location of bearing looseness is different

    图 10  松动支承位置不同时轮盘2振幅随转速变化的分岔图

    Figure 10.  Bifurcation diagram of vibration amplitude of Disk 2 changing with rotational speed when location of bearing looseness is different

    图 11  松动支承位置不同时3号支点振幅随转速变化的分岔图

    Figure 11.  Bifurcation diagram of vibration amplitude of Support 3 changing with rotational speed when location of bearing looseness is different

    图 12  不平衡量不同时2号支点振幅随转速变化的分岔图

    Figure 12.  Bifurcation diagram of vibration amplitude of Support 2 changing with rotational speed when unbalance value is different

    图 13  支承刚度不同时2号支点振幅随转速变化的分岔图

    Figure 13.  Bifurcation diagram of vibration amplitude of Support 2 changing with rotational speed when bearing stiffness is different

    图 14  松动间隙不同时2号支点振幅随转速变化的分岔图

    Figure 14.  Bifurcation diagram of vibration amplitude of Support 2 changing with rotational speed when bearing clearance is different

    表  1  结构参数取值

    Table  1.   Values of structural parameters

    参数 数值
    m1e1/(g·mm) 10
    m2e2/(g·mm) 10
    c2/mm 7×10-4
    c4/mm 4×10-4
    c2c2/mm 2×10-4
    c4c4/mm 2×10-4
    k1/(N·m-1) 2×105
    k2/(N·m-1) 1×104
    下载: 导出CSV

    表  2  挤压油膜阻尼器参数取值

    Table  2.   Values of SFD parameters

    参数 滑油黏度/(Pa·s) 轴向承载长度/mm 轴承半径/mm
    数值 1×10-3 90 40
    下载: 导出CSV

    表  3  轮盘不平衡量取值

    Table  3.   Unbalance value of disk

    不平衡量 m1e1/(g·mm) m2e2/(g·mm)
    小不平衡量 10 10
    大不平衡量 50 50
    下载: 导出CSV

    表  4  支承刚度变化区间

    Table  4.   Variation range of bearing stiffness

    支承刚度变化范围 Ks2/(N·m-1) Ks3/(N·m-1)
    支承刚度变化范围小 0~1×105 0~1×105
    支承刚度变化范围大 0~1×107 0~1×107
    下载: 导出CSV

    表  5  松动间隙参数取值

    Table  5.   Parameter values of bearing clearance

    松动间隙 c2/mm c4/mm c2/mm c4/mm
    小松动间隙 1.4×10-3 8×10-4 2×10-4 2×10-4
    大松动间隙 7×10-3 4×10-3 2×10-3 2×10-3
    下载: 导出CSV
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出版历程
  • 收稿日期:  2017-04-28
  • 录用日期:  2017-08-02
  • 网络出版日期:  2018-04-20

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