基于非线性超声的复合材料疲劳损伤演化的实时预测方法及应用

By using nonlinear ultrasonic technology to detect fatigue damage in aerospace composite materials in real time, establishing a mapping model and embedding a digital twin model, the problem of traditional methods being unable to monitor fatigue damage in composite materials is solved, and real-time, non-destructive characterization of damage and life prediction are realized.

CN122193430BActive Publication Date: 2026-07-17EAST CHINA UNIV OF SCI & TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
EAST CHINA UNIV OF SCI & TECH
Filing Date
2026-05-15
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies are insufficient for real-time and non-destructive monitoring of fatigue damage evolution in aerospace composite materials. Traditional methods are costly, time-consuming, and lack sufficient detection sensitivity, failing to meet the requirements for condition perception and life prediction of aerospace structures.

Method used

Nonlinear ultrasonic technology is used to detect ultrasonic guided wave signals in real time during fatigue loading, extract fundamental frequency and harmonic components, calculate nonlinear ultrasonic parameters, establish a mapping model between the parameters and the fatigue damage evolution state, and embed them into a digital twin model for real-time prediction.

Benefits of technology

This method enables continuous and non-destructive characterization of fatigue damage in composite materials from early initiation to failure, providing a basis for life prediction and health management of composite materials, and breaking through the technical bottleneck of traditional methods.

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Abstract

本发明涉及复合材料结构健康监测与损伤表征的技术领域,提供一种基于非线性超声的复合材料疲劳损伤演化的实时预测方法及应用,通过在航空复合材料疲劳加载过程中,同步引入非线性超声在线检测,通过激发超声信号并采集材料中的首到达波包,提取基频及其对应的二次和三次谐波分量,计算非线性超声参数以表征疲劳损伤引起的非线性响应变化;在此基础上,构建非线性超声参数与复合材料疲劳损伤演化状态之间的映射关系,并将该关系嵌入数字孪生模型中,实现疲劳损伤状态的实时更新与演化表征;通过对非线性超声参数的持续监测,可在线反演复合材料在不同疲劳阶段的损伤状态,并进一步评估其力学性能退化趋势与剩余寿命。
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