长柔结构弯扭耦合颤振临界风速改进正则摄动高阶展开预测方法和系统

By using an improved regular perturbation high-order expansion method, the problem of solving the equal frequency condition in the prediction of critical wind speed for bending-torsional coupling flutter of long and flexible structures is solved. It realizes the explicit expression of the analytical solution, simplifies the calculation and clearly reveals the influence of parameters, and is applicable to the wind-resistant design of long-span bridges and other structures.

CN122263252BActive Publication Date: 2026-07-17CHONGQING UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHONGQING UNIV
Filing Date
2026-05-26
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing perturbation methods struggle to handle conditions with equal or similar frequencies in predicting critical wind speeds for bending-torsional coupled flutter in long, flexible structures, leading to difficulty in solving the problem or even failure. Furthermore, traditional methods cannot clearly reveal the influence mechanism of parameters on flutter instability.

Method used

An improved method for canonical perturbation high-order expansion is proposed. By distinguishing frequency conditions, an explicit analytical solution is derived, the bridge motion control matrix equation is constructed and perturbation expansion is performed, long-term terms are eliminated, and eigenvalues ​​and eigenvectors are solved step by step to explicitly express the modal frequency, damping ratio and phase difference. This method is applicable to both equal and unequal frequency conditions.

Benefits of technology

It achieves efficient and accurate prediction under different frequency ratio conditions, simplifies the calculation process, clearly reveals the contribution mechanism of structural parameters to flutter instability, and provides a scientific basis for wind-resistant design.

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Abstract

本发明公开了一种长柔结构弯扭耦合颤振临界风速改进正则摄动高阶展开预测方法及系统。本发明方法包括:步骤一:基于Scanlan自激力模型采集气动与结构参数;步骤二:构建弯扭耦合控制矩阵方程并引入小参数进行摄动展开;步骤三:运用改进正则摄动法,区分频率相等与不等情况,通过构造特征值消除长期项,逐阶求解特征值与模态向量;步骤四:推导模态频率、阻尼比、振幅比及相位差的显式解析解;步骤五:通过单次迭代确定模态频率并直接求解阻尼比,以判定颤振临界风速。本发明将复杂非线性问题拆解为分量的线性叠加,获得了参数的显式闭合解,仅需单次迭代即可完成计算,显著简化了分析流程,并能清晰揭示各结构、气动参数对颤振失稳的影响机制。
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