Ultrasonic array testing and evaluation method of multilayer bonded structures

被引:0
|
作者
Zhou Z. [1 ]
Wang J. [1 ]
Li Y. [2 ]
Wang F. [3 ]
Wei Q. [3 ]
机构
[1] School of Mechanical Engineering and Automation, Beihang University, Beijing
[2] Ningbo Innovation Research Institute of Beihang University, Ningbo
[3] Shanghai Spaceflight Precision Machinery Institute, Shanghai
关键词
de-bonding; multi-layer structure; non-destructive testing; reflection coefficient; ultrasonic array;
D O I
10.13700/j.bh.1001-5965.2022.0084
中图分类号
学科分类号
摘要
In the ultrasonic detection for multi-layer bonding structures of metal and non-metal materials such as rubber, the signal to noise ratio of debonding defect is low, and the defect identification is difficult, due to the significant difference in acoustic impedance between media and large ultrasonic attenuation. In order to improve the detection ability of de-bonding defects in multilayer structures, a novel ultrasonic detection and evaluation method based on linear array ultrasonic transducers is proposed. Firstly, the propagation characteristics of ultrasonic waves at the bonding interface are analyzed, and the spectral relationship of the reflection coefficient in a multilayer system is described. Further, a numerical simulation analysis model is built in accordance with the stiffness matrix transfer model of multilayer medium, which is used to realize the design and calculation of the ultrasonic array focusing scheme and detection process. These methods are based on the 3D CAD inspection model. Finally, by analyzing the amplitude spectrum characteristics of interface echo signals under different bonding states, a C-scan imaging method using amplitude spectrum characteristics is proposed. The experiment results show that the method proposed can effectively improve the detection efficiency of multilayer bonded structures and improve the signal-to-noise ratio of detection results, and reduce the complexity of C-scan imaging characterization of de-bonding defects. © 2023 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
引用
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页码:3207 / 3214
页数:7
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