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叶片缘板阻尼特性的自由振动测试

彭泰 王延荣 李迪 李鸿光 杜晨鸿 石霖

彭泰, 王延荣, 李迪, 等. 叶片缘板阻尼特性的自由振动测试[J]. 航空动力学报, 2025, 40(9):20230742 doi: 10.13224/j.cnki.jasp.20230742
引用本文: 彭泰, 王延荣, 李迪, 等. 叶片缘板阻尼特性的自由振动测试[J]. 航空动力学报, 2025, 40(9):20230742 doi: 10.13224/j.cnki.jasp.20230742
PENG Tai, WANG Yanrong, LI Di, et al. Free vibration test of damping characteristics for model blade with underplatform damper[J]. Journal of Aerospace Power, 2025, 40(9):20230742 doi: 10.13224/j.cnki.jasp.20230742
Citation: PENG Tai, WANG Yanrong, LI Di, et al. Free vibration test of damping characteristics for model blade with underplatform damper[J]. Journal of Aerospace Power, 2025, 40(9):20230742 doi: 10.13224/j.cnki.jasp.20230742

叶片缘板阻尼特性的自由振动测试

doi: 10.13224/j.cnki.jasp.20230742
基金项目: 国家科技重大专项(2017-Ⅳ-0002-0039)
详细信息
    作者简介:

    彭泰(1999-),男,硕士生,主要从事航空发动机结构强度及振动研究

    通讯作者:

    李迪(1983-),男,博士生,主要从事航空发动机结构强度研究。E-mail:lidi831616@163.com

  • 中图分类号: V231.92

Free vibration test of damping characteristics for model blade with underplatform damper

  • 摘要:

    设计了一种自由衰减振动试验,通过对叶片模拟件施加一阶弯曲振动方向载荷并释放后激发其一阶自由振动,对其关键位置应变及加速度时域信号进行测试分析,一次试验即可获得较大振动应力范围内的临界阻尼比特性曲线。试验结果显示:阻尼器的特性曲线与仿真计算结果吻合较好;峰值阻尼比与阻尼器的惯性载荷无关;接触面积不同的阻尼器提供的阻尼比大致相同;阻尼效果与伸根段长度呈正相关。

     

  • 图 1  加速度传感器测量信号及其包络线

    Figure 1.  Acceleration sensor response and envelope

    图 2  叶片及缘板阻尼器试验件模型

    Figure 2.  Model of blade and underplatform damper test pieces

    图 3  缘板阻尼器安装示意图

    Figure 3.  Underplatform damper installation diagram

    图 4  缘板阻尼器安装方法

    Figure 4.  Underplatform damper installation method

    图 5  模态位移提取示意图

    Figure 5.  Diagram of extracting modal displacement

    图 6  阻尼比特性曲线仿真结果(斜接触面安装阻尼器)

    Figure 6.  Damping ratio characteristic curve simulation results (damper installed on incline contact surface)

    图 7  自由衰减振动试验数据

    Figure 7.  Damped free vibration test data

    图 8  未安装缘板阻尼器时自由衰减阻尼比特性曲线

    Figure 8.  Damping characteristic curve of free vibration without underplatform damper

    图 9  叶片试验件阻尼特性(斜接触面安装缘板阻尼器,惯性载荷为120 N)

    Figure 9.  Damping characteristics of blade test piece (damper installed on incline contact surface, inertial load 120 N)

    图 10  叶片试验件阻尼特性(斜接触面安装缘板阻尼器,不同惯性载荷)

    Figure 10.  Damping characteristics of blade test piece (damper installed on incline contact surface, different inertial loads)

    图 11  叶片试验件阻尼特性(直接触面安装缘板阻尼器,不同惯性载荷)

    Figure 11.  Damping characteristics of blade test piece (damper installed on vertical contact surface, different inertial loads)

    图 12  叶片试验件阻尼特性(不同阻尼器试验件)

    Figure 12.  Damping characteristics of blade test pieces (different damper test pieces)

    图 13  各叶片试验件的阻尼特性

    Figure 13.  Damping characteristics of each blade test pieces

    表  1  缘板阻尼器减振参数

    Table  1.   Vibration reduction parameters of underplatform damper

    参数 数值
    斜接触面径向模态位移$ {A_{{\text{x,r}}}} $/mm 116
    斜接触面周向模态位移$ {A_{{{{\mathrm{x}},{\text{θ}} }}}} $/mm 97
    直接触面径向模态位移$ {A_{{\text{z,r}}}} $/mm −116
    直接触面周向模态位移$ {A_{{{{\mathrm{z}},{\text{θ}}}}}} $/mm 103
    考查点模态等效应力${\sigma _{{\text{ref}}}}$/105 MPa 4.58
    模态动能$ {W_{{\text{ref}}}} $/106 J 2.14
    摩擦因数$\mu $ 0.3
    切向接触刚度$ {K_{\text{d}}}/{\text{(N/mm)}} $ 30000
    下载: 导出CSV

    表  2  缘板阻尼器试验件斜接触区尺寸

    Table  2.   Dimension of inclined contact area of underplatform damper test pieces mm

    试验件序号斜接触区长度斜接触区宽度
    13316
    22216
    31116
    下载: 导出CSV

    表  3  试验件的叶片伸根段长度

    Table  3.   Length of blade root extending section of test pieces mm

    试验件序号伸根沿叶高方向长度
    128
    238
    348
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-11-26
  • 网络出版日期:  2025-04-15

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