Laminated composite materials are formed by laminating two or more layers of the same or different materials. Due to the excellent mechanical properties
laminate composite materials are widely used in aerospace and navigation fields. However
during the production and service stage
defects such as disbond and delamination between
layers have greatly affected the stability of component. Currently
the commonly used contact ultrasonic testing has limitations such as large blind area
small field of view
many artifacts and water coupling. Combining the advantages of laser ultrasound and air-coupled ultrasound
a non-contact laser ultrasonic testing system consisting of eight elements 250 kHz air-coupled transducer is developed to detect thin laminated composite materials with thickness of 0.8 mm metal–carbon fiber and 0.3 mm metal–metal
respectively. The system can not only clearly display multiple disbond defects inside the sample
but also successfully identify micro cavity defects formed by bonding layer indentation and bubbles. The imaging field and SNR are up to 220 mm and 35 dB
respectively. Besides
compared to high-frequency phased array and X-ray testing
the system exhibits excellent imaging contrast
resolution
and sensitivity. The experimental results show that the developed large-field air-coupled laser ultrasonic testing system has broad application prospects in the large laminated composite materials.
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Related Author
ZHENG Bo
LUO Jinchao
GENG Junhao
MA Linsen
HAN Wei
CHENG Yu
LIU Zhenhao
XU Zhenye
Related Institution
Civil Aviation Flight University of China, Guanghan
AVIC XAC Commercial Aircraft Co., Ltd.
Northwestern Polytechnical University
NDT & E Laboratory, Dalian University of Technology
Key Lab of High Performance Electromagnetic Window for Aviation Science and Technology, AVIC Research Institute for Special Structures of Aeronautical Composites