Dixième anniversaire

A mono-pulse ultrasonic (MU)-based detection method was developed for the detailed characterisation of the carbon-fibre skin–stiffener bonding interface and the quantitative evaluation of the fine defects therein. Specimens exhibiting artificial defects and actual skin–stiffener components were used as test specimens. A MU experimental system was constructed. Experiments were performed to elucidate reflection behaviour and signal and morphological characteristics of skin–stiffener joints, and the microstructural morphologies were compared. Defect detectability was experimentally studied at different sample depths. The results showed that the reflected-signal pulse width was ∼1 period. The ultrasonic dead zone reached a single pre-preg-ply thickness (∼ 0.125 mm). The de-lamination, de-bonding, adhesive and resin layers, and changes in the bonding-interface layup, were well determined. The minimum and maximum deviations of the detected-defect sizes were ∼ 0.0 and 1.0 mm, respectively. The de-lamination depth-positioning deviation was < 0.5 of a pre-preg ply

Acoustics · Adhesive · Composite material · Lamination · Layer (electronics · Optics · Physics · Pulse (music · Reflection (computer programming · SIGNAL (programming language · Ultrasonic sensor · Material Properties and Processing · Materials Science · Mechanical Behavior of Composites · Ultrasonics and Acoustic Wave Propagation