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Damage detection method for thin-wall structure

A technology for damage detection and thin-walled structures, which is applied to measuring devices, instruments, and the use of sound waves/ultrasonic waves/infrasonic waves to analyze solids, etc. It can solve the problem of low imaging accuracy and achieve precise and specific results.

Pending Publication Date: 2022-05-10
NORTHWESTERN POLYTECHNICAL UNIV
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AI Technical Summary

Problems solved by technology

However, the traditional OMP algorithm can only achieve small damage imaging, the main reason is that for a few pixels in a small area, due to the relatively small distance, the propagation time difference of the Lamb wave is almost equal to 0, resulting in In order to achieve the sparse representation of the signal by finding the best matching atom when the OMP algorithm is used, only one pixel can be obtained in the corresponding area as the main damaged pixel. point, ignoring other possible damaged pixels
Therefore, through the traditional OMP algorithm, the pixel points must be equal to the size of the damage in order to better realize damage localization imaging, which results in low imaging accuracy; and when the pixel points are small, it is difficult to realize the detection of existing damage in the structure. Lesion Imaging in Larger Lesions

Method used

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  • Damage detection method for thin-wall structure
  • Damage detection method for thin-wall structure
  • Damage detection method for thin-wall structure

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experiment example

[0132] A specific experimental example is given below to further illustrate the technical effect of the technical solution.

[0133]The content of this experiment example uses Abaqus finite element simulation to simulate when there is a single type of damage or multiple types of damage in the thin-walled structure, and then performs damage imaging based on the data obtained from the simulation, and finally analyzes the detection method through the evaluation of the damage imaging performance. Among them, the size of the thin-walled structure used in the simulation is 500×500×2mm, the excitation adopts the five-period Lamb wave with the center frequency of 100 modulated by Hann window, and the excitation method is single-point excitation to generate the A0 mode in the thin-walled structure Lamb waves. In this section, the performance of the thin-walled structure damage detection method provided in this embodiment is analyzed by comparing the damage images obtained by the thin-w...

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Abstract

The invention relates to the field of modern aircraft large-size thin-wall structure damage detection, in particular to a thin-wall structure damage detection method. Response signals of N (N-1) paths of Lamb waves and reference signals of the N (N-1) paths of Lamb waves are obtained; determining a damage scattering signal based on the response signal and the reference signal; performing noise reduction on the damage scattering signal through an over-complete dictionary; determining the damage probability of the L * M virtual units according to an OMP algorithm, and obtaining N (N-1) damage elliptical bands through probability imaging; superposing or multiplying the N (N-1) damaged elliptical bands to obtain the damage probability of the L * M virtual units, and obtaining a thin-wall structure damage image through probability imaging; according to the embodiment, qualitative judgment and quantitative judgment of the damage position are achieved, and the result is more accurate and specific.

Description

technical field [0001] The invention relates to the field of large-scale structure damage detection of modern aircraft, in particular to a thin-walled structure damage detection method. Background technique [0002] Affected by dynamic / static loads, working conditions, material properties, and external factors, modern aircraft structures tend to have performance degradation trends and more serious structural damage, which affects their normal work and may further cause safety hazards, and even It was a catastrophic accident. In addition, in the stage of aircraft design and manufacture, because it is difficult to accurately predict the distribution of factors affecting structural life in service, even the most perfect design is difficult to avoid the risks brought about by changes in service conditions. As people's requirements for the safety, reliability and economical operation of modern aircraft are becoming more and more prominent, the development of a reliable and effic...

Claims

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Application Information

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IPC IPC(8): G01N29/04G01N29/06
CPCG01N29/041G01N29/0654G01N29/069G01N2291/023G01N2291/0423
Inventor 丑帅尚柏林张子豪张玉刚刘小锋周德响钟亮
Owner NORTHWESTERN POLYTECHNICAL UNIV
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