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薄壁机匣-非线性能量阱多频共振捕获与靶向减振机理

刘绅 马英群 赵巍 雒伟伟 任三群 赵庆军

刘绅, 马英群, 赵巍, 等. 薄壁机匣-非线性能量阱多频共振捕获与靶向减振机理[J]. 航空动力学报, 2026, 41(9):20250027 doi: 10.13224/j.cnki.jasp.20250027
引用本文: 刘绅, 马英群, 赵巍, 等. 薄壁机匣-非线性能量阱多频共振捕获与靶向减振机理[J]. 航空动力学报, 2026, 41(9):20250027 doi: 10.13224/j.cnki.jasp.20250027
Liu Shen, Ma Yingqun, Zhao Wei, et al. Multi-frequency resonance capture and targeted vibration suppression mechanism in thin-walled casing-nonlinear energy sink[J]. Journal of Aerospace Power, 2026, 41(9):20250027 doi: 10.13224/j.cnki.jasp.20250027
Citation: Liu Shen, Ma Yingqun, Zhao Wei, et al. Multi-frequency resonance capture and targeted vibration suppression mechanism in thin-walled casing-nonlinear energy sink[J]. Journal of Aerospace Power, 2026, 41(9):20250027 doi: 10.13224/j.cnki.jasp.20250027

薄壁机匣-非线性能量阱多频共振捕获与靶向减振机理

doi: 10.13224/j.cnki.jasp.20250027
基金项目: 国家自然科学基金(12402408); 国家自然科学基金“叶企孙”联合基金(U2441278)
详细信息
    作者简介:

    刘绅(1995-),男,博士,研究方向为航空发动机整机振动控制。E-mail:liushen@iet.cn

    通讯作者:

    赵庆军(1977-),男,研究员,博士,主要从事航空发动机气动热力学研究。E-mail:zhaoqingjun@iet.cn

  • 中图分类号: V232.3;TB535.1;O322

Multi-frequency resonance capture and targeted vibration suppression mechanism in thin-walled casing-nonlinear energy sink

  • 摘要:

    引入具有非线性刚度特征的动力吸振器(非线性能量阱)至三自由度系统开展对主系统多阶频率振动抑制的研究,在此基础上扩展至具有连续介质特性的航空发动机真实机匣结构。在理论分析方面,基于复变量平均法揭示了三自由度非线性系统中非线性能量阱实现瞬态共振捕获和靶向能量传递的内在机理和必要条件,得到了多自由度系统中非线性能量阱的动力学响应特性。在规律分析方面,开展三自由度非线性系统中不同非线性刚度和阻尼参数对非线性能量阱能量耗散特性影响规律研究,得出了多自由度系统中非线性能量阱最优振动耗散特性。基于振动能量可视化分析方法,非线性能量阱设计方法扩展至真实航空发动机组合机匣结构,成功可视化捕捉到振动能量从机匣振源传递至非线性能量阱的过程,从振动能量的角度揭示了非线性能量阱对机匣结构的靶向能量吸收与耗散特性,单个非线性能量阱有效抑制机匣三阶模态振动,振幅分别降低25.1%、25.3%和25.2%,实现了非线性能量阱对薄壁机匣结构的宽频振动抑制。

     

  • 图 1  含NES的三自由度非线性系统示意图

    Figure 1.  Schematic diagram of a three-degree-of-freedom nonlinear system with NES

    图 2  非线性系统频率-能量曲线

    Figure 2.  Frequency-energy curve of the nonlinear system

    图 3  NES与质点1振幅比

    Figure 3.  Amplitude ratio of NES to m1

    图 4  NES与质点2振幅比

    Figure 4.  Amplitude ratio of NES to m2

    图 5  不同脉冲激励下NES能量耗散比例

    Figure 5.  Energy dissipation ratio of NES under different pulse excitations

    图 6  各质点响应结果(C点)

    Figure 6.  Response results of each particle (point C

    图 7  各质点局部位移-时间响应结果(C点)

    Figure 7.  Local displacement-time response results of each particle (point C

    图 8  质点1位移傅里叶变换和系统能量耗散对比(C点)

    Figure 8.  Comparison of Fourier transform of displacement of m1 and system energy dissipation (point C)

    图 9  各质点响应结果

    Figure 9.  Response results of each particle

    图 10  系统能量耗散对比

    Figure 10.  Comparison of system energy dissipation

    图 11  不同参数下NES能量耗散特性

    Figure 11.  Energy dissipation characteristics of NES with different parameters

    图 12  不同激励下不同参数NES能量耗散特性

    Figure 12.  Energy dissipation characteristics of NES with different parameters under various excitations

    图 13  预屈曲梁结构

    Figure 13.  Pre-buckled beam structure

    图 14  连接NES的航空发动机机匣结构

    Figure 14.  Engine casing structure with connected NES

    图 15  航空发动机机匣尺寸(单位:mm)

    Figure 15.  Engine casing dimensions (unit:mm)

    图 16  结构声强矢量场计算流程

    Figure 16.  Calculation process of structural intensity field

    图 17  激励曲线

    Figure 17.  Excitation curve

    图 18  脉冲激励下机匣振动能量矢量云图

    Figure 18.  Vibration energy vector cloud map on the casing under pulse excitation

    图 19  点Ⅰ位移响应曲线

    Figure 19.  Displacement response curve at point Ⅰ

    图 20  点Ⅰ位移响应傅里叶变换结果

    Figure 20.  Fourier transform results of displacement response at point Ⅰ

    图 21  点Ⅰ位移响应曲线(初始阶段)

    Figure 21.  Displacement response curve at point Ⅰ (initial stage)

    图 22  点Ⅰ位移响应傅里叶变换结果(初始阶段)

    Figure 22.  Fourier transform results of displacement response at point Ⅰ (initial stage)

    图 23  点Ⅰ位移响应对比

    Figure 23.  Comparison of displacement response at point Ⅰ

    图 24  点Ⅰ位移响应对比(初始阶段)

    Figure 24.  Comparison of displacement response at point Ⅰ (initial stage)

    图 25  点Ⅰ位移响应傅里叶变换对比

    Figure 25.  Comparison of Fourier transform of displacement response at point Ⅰ

    图 26  点Ⅱ位移响应对比

    Figure 26.  Comparison of displacement response at point Ⅱ

    图 27  点Ⅱ位移响应对比(初始阶段)

    Figure 27.  Comparison of displacement response at point Ⅱ (initial stage)

    图 28  点Ⅰ与NES质点位移响应

    Figure 28.  Displacement responses of point I and NES mass

    图 29  点Ⅰ与NES质点位移响应(初始阶段)

    Figure 29.  Displacement response of point I and NES mass(initial stage)

    图 30  点Ⅱ位移响应对比

    Figure 30.  Comparison of displacement response at point Ⅱ

    图 31  点Ⅱ位移响应傅里叶变换对比

    Figure 31.  Comparison of Fourier transform of displacement response at point Ⅱ

    图 32  机匣振动能量矢量云图

    Figure 32.  Casing vibration energy vector cloud map

    表  1  不同模态分支下系统动力学特性

    模态分支 各质点运动相位 振幅比变化趋势 NES靶向吸收振动能量
    S111+++ 质点1与NES同相运动;
    质点2与NES同相运动
    随着振动能量的耗散,An/A1绝对值
    逐渐增加,An/A2绝对值逐渐增加
    NES实现了对质点1和质点2的瞬态共振捕获,靶向吸收其振动能量
    S111++− 质点1与NES反相运动;
    质点2与NES反相运动
    随着振动能量的耗散,An/A1绝对值
    逐渐减小,An/A2绝对值逐渐减小
    NES未实现靶向吸收振动能量的功能
    S111+−− 质点1与NES反相运动;
    质点2与NES同相运动
    随着振动能量的耗散,An/A1绝对值
    逐渐增加,An/A2绝对值逐渐增加
    NES实现了对质点1和质点2的瞬态共振捕获,靶向吸收其振动能量
    S111+−+ 质点1与NES同相运动;
    质点2与NES反相运动
    随着振动能量的耗散,An/A1绝对值
    逐渐减小,An/A2绝对值逐渐减小
    NES未实现靶向吸收振动能量的功能
    下载: 导出CSV
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  • 收稿日期:  2025-01-16
  • 网络出版日期:  2026-06-06

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