LIU Feifei, LIU Songping, LI Zhiying, LI Legang, YANG Yusen, FU Tianhang, CHANG Haifeng. Characterisation and Evaluation of Defects in Composite Skin–Rib Joint Using Mono-Pulse Ultrasonic Method[J]. Aeronautical Manufacturing Technology, 2023, 66(22): 36-45.
LIU Feifei, LIU Songping, LI Zhiying, LI Legang, YANG Yusen, FU Tianhang, CHANG Haifeng. Characterisation and Evaluation of Defects in Composite Skin–Rib Joint Using Mono-Pulse Ultrasonic Method[J]. Aeronautical Manufacturing Technology, 2023, 66(22): 36-45. DOI: 10.16080/j.issn1671-833x.2023.22.036.
Characterisation and Evaluation of Defects in Composite Skin–Rib Joint Using Mono-Pulse Ultrasonic Method
The skin–rib joint is a very important form in carbon fiber composite panels. Because of the complex in geometric structure
internal layer
defect behavior and orientation of fibers therein
defect characterisation
detection and evaluation have been the technical difficulties and focus in their applications. In this paper
a new method for defect characterization and evaluation is proposed using mono-pulse ultrasonic (MU) wave. The experimental results show that the echo signals resulted from the skin–rib joints have very good time-domain resolution under MU reflection condition. When echo signal is close to one pulse cycle
the ultrasonic surface detection dead zone can reach a single layer thickness (about 0.125 mm). Delamination
disbanding
adhesive layer
resin layer and internal layer variation in the skin–rib joints can be characterized
detected and evaluated. The minimum deviation of detected defect is close to 0.0 mm
and the maximum deviation is about 1.0 mm compared with their designed sizes. The depth positioning deviation of detected defect is less than 0.5 prepreg ply thickness. It provides a very effective ultrasonic characterisation and evaluation method for the composite panels. Good practical application has been obtained.