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Characterisation of composite skin–stiffener bonding interface and fine-defect evaluation using mono-pulse ultrasonic detection

  • Feifei Liu*
  • , Zhenggan Zhou
  • , Songping Liu*
  • , Legang Li
  • , Tianhang Fu
  • , Haifeng Chang
  • *此作品的通讯作者
  • Beihang University
  • China Aviation Industry Corporation
  • AVIC Composite Corporation Ltd.

科研成果: 期刊稿件文章同行评审

摘要

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.

源语言英语
文章编号102681
期刊NDT and E International
131
DOI
出版状态已出版 - 10月 2022

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