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燃气轮机可倾瓦轴承-拉杆转子系统振动控制实验

韩东江 蔡艺谋 毕春晓 杨金福

韩东江, 蔡艺谋, 毕春晓, 等. 燃气轮机可倾瓦轴承-拉杆转子系统振动控制实验[J]. 航空动力学报, 2025, 40(4):20240501 doi: 10.13224/j.cnki.jasp.20240501
引用本文: 韩东江, 蔡艺谋, 毕春晓, 等. 燃气轮机可倾瓦轴承-拉杆转子系统振动控制实验[J]. 航空动力学报, 2025, 40(4):20240501 doi: 10.13224/j.cnki.jasp.20240501
HAN Dongjiang, CAI Yimou, BI Chunxiao, et al. Vibration control experiments of gas turbine tilting pad bearing-rod rotor system[J]. Journal of Aerospace Power, 2025, 40(4):20240501 doi: 10.13224/j.cnki.jasp.20240501
Citation: HAN Dongjiang, CAI Yimou, BI Chunxiao, et al. Vibration control experiments of gas turbine tilting pad bearing-rod rotor system[J]. Journal of Aerospace Power, 2025, 40(4):20240501 doi: 10.13224/j.cnki.jasp.20240501

燃气轮机可倾瓦轴承-拉杆转子系统振动控制实验

doi: 10.13224/j.cnki.jasp.20240501
基金项目: 航空发动机和燃气轮机重大专项(2017-Ⅳ-0010-0047); 中国科学院青年创新促进会项目(2021141)
详细信息
    作者简介:

    韩东江(1986-),男,副研究员,博士,主要从事轴承-转子动力学特性研究。E-mail:handongjiang@iet.cn

  • 中图分类号: V231.9

Vibration control experiments of gas turbine tilting pad bearing-rod rotor system

  • 摘要:

    设计并搭建燃气轮机可倾瓦轴承-拉杆转子系统振动特性实验平台,开展拉杆转子模态实验、不同预紧力下振动特性实验和基于压电陶瓷微位移作动器的振动控制实验,实验结果表明:拉杆转子弯曲模态频率随预紧力增加而增加,拉杆预紧力矩从15 N·m增加到40 N·m,拉杆转子第1阶与第2阶模态频率分别增加2.66%和5.43%;拉杆转子系统前两阶临界转速下的不平衡响应随拉杆预紧力的增加而降低,在一定范围内,拉杆预紧力的增加能够推迟轴系出现低频涡动的起始转速,提高轴系的稳定性;压电陶瓷微位移作动器对拉杆转子不平衡响应振动控制具有积极作用。相关研究结果为后续开展拉杆转子系统耦合振动谐调控制提供了实验基础。

     

  • 图 1  高速电动机驱动的可倾瓦轴承-拉杆转子系统实验平台

    Figure 1.  Experimental platform of tilting pad bearing-rod rotor system driven by high-speed motor

    图 2  拉杆转子结构示意图及实物图

    Figure 2.  Rod rotor structure diagram and physical diagram

    图 3  传感器布置图

    Figure 3.  Sensor layout diagram

    图 4  拉杆转子悬吊模态实验图

    Figure 4.  Rod rotor modal experiment diagram

    图 5  拉杆转子模态频率随预紧力矩变化特性

    Figure 5.  Characteristics of rod rotor modal frequency with Preloading torque

    图 6  可倾瓦轴承的主刚度和主阻尼系数随承载能力系数变化曲线

    Figure 6.  Main stiffness and main damping coefficient of tilting pad bearing change with bearing capacity coefficient

    图 7  可倾瓦轴承的交叉刚度和交叉阻尼系数随承载能力系数变化曲线

    Figure 7.  Cross-stiffness and cross-damping coefficients of tilting pad bearings vary with load-carrying capacity coefficient

    图 8  不同拉杆预紧力矩下转子升速过程不平衡响应(压气机端左45°位置)

    Figure 8.  Unbalanced response of the rotor during the acceleration process under different rod preloads (45° left of the compressor end)

    图 9  预紧力矩为25 N·m下升速过程轴心轨迹

    Figure 9.  Axis trajectory of the acceleration process under the preload of 25 N·m

    图 10  低频涡动发生转速随预紧力矩变化规律

    Figure 10.  Variation law of low frequency whirl speed with preload force

    图 11  含压电陶瓷微位移作动器的可倾瓦轴承示意图及实际结构图

    Figure 11.  Schematic diagram and actual structure diagram of tilting pad bearing with piezoelectric ceramic micro-displacement actuator

    图 12  转子升速过程轴心轨迹

    Figure 12.  Axis orbits during the rotor acceleration process

    图 13  不同驱动电压下拉杆转子不平衡响应的变化规律

    Figure 13.  Variation law of unbalanced response of tie rod rotor under different driving voltages

    表  1  拉杆转子的关键尺寸

    Table  1.   Key dimensions of rod rotor mm

    参数数值
    轴承跨距859.50
    压气机端长度586.50
    鼓筒长度135.00
    鼓筒内径60.00
    涡轮端长度340.00
    拉杆中心处直径115.00
    模化盘外径144.00
    压气机端拉杆直径10.00
    涡轮端拉杆直径8.00
    模化盘中心孔内径14.00
    下载: 导出CSV

    表  2  可倾瓦轴承参数

    Table  2.   Tilting pad bearing parameters

    参数 数值
    轴承半径R/mm 30
    轴承长L/mm 40
    载荷/N 340.55
    工作转速/(r/min) 36000
    瓦块张角α/(°) 65
    支点偏置 0.6
    预负荷系数m 0.75
    平均黏度μa/(mPa·s) 11.4997
    下载: 导出CSV

    表  3  不同预紧力条件下拉杆转子临界转速特征(压气机端左45°位置)

    Table  3.   Critical speed characteristics of rod fastening rotor under different preload conditions (45° left position of compressor end)

    参数 预紧力矩/(N·m)
    25 30 35
    临界转速/
    (r/min)
    第1阶 8520 8646 9074
    第2阶 13510 13720 13875
    临界转速对应的
    响应幅值/μm
    第1阶 128.1 122.7 104.9
    第2阶 112.4 105.1 92.3
    下载: 导出CSV

    表  4  压电陶瓷微位移作动器影响试验组

    Table  4.   Piezoelectric ceramic micro displacement actuator influence test group

    实验
    序号
    压电陶瓷微位移作动器参数 备注
    驱动器输入电压/V 作动器执行位移/μm
    1 0 0 闭环控制
    2 30 2 闭环控制
    3 50 3.3 闭环控制
    4 70 4.7 闭环控制
    5 80 5.3 闭环控制
    下载: 导出CSV

    表  5  升速过程不同驱动电压下前两阶临界转速的振动响应

    Table  5.   Vibration response of the first two critical speeds under different driving voltages during the acceleration process

    实验序号 第1阶临界转速 第2阶临界转速
    转速/(r/min)(变化率) 振动幅值/μm(变化率) 转速/(r/min)(变化率) 振动幅值/μm(变化率)
    1 6841 13.80 12239 10.95
    2 6910(−1%) 9.50(31.16%) 12399(−1.3%) 7.9(27.85%)
    3 6910(−1%) 10.52(23.77%) 12337(−0.8%) 8.65(21.00%)
    4 6945(−1%) 11.08(19.71%) 12349(−0.9%) 9.40(14.16%)
    5 6896(−1.5%) 12.35(10.51%) 12288(−0.4%) 10.34(5.57%)
    下载: 导出CSV

    表  6  降速过程不同驱动电压下前两阶临界转速的振动响应

    Table  6.   Vibration response of the first two critical speeds under different driving voltages during the deceleration process

    实验序号 第1阶临界转速 第2阶临界转速
    转速/(r/min)(变化率) 振动幅值/μm(变化率) 转速/(r/min)(变化率) 振动幅值/μm(变化率)
    1 6692 13.70 12163 11.09
    2 6882(−2.8%) 9.95(27.37%) 12374(−1.73%) 8.35(24.71%)
    3 6812(−1.8%) 10.99(19.78%) 12288(−1.03%) 8.66(21.91%)
    4 6819(−1.9%) 11.44(16.50%) 12202(−0.32%) 9.39(15.32%)
    5 6805(−1.7%) 12.48(8.9%) 12200(−0.30%) 10.03(9.56%)
    下载: 导出CSV
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  • 收稿日期:  2024-07-26
  • 网络出版日期:  2024-11-07

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