4.7 Article

Laser ablation of CFRP surfaces for improving the strength of bonded scarf composite joints

Journal

COMPOSITE STRUCTURES
Volume 296, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2022.115881

Keywords

Composite laminates; Adhesive bonding; Surface treatment; Joint strength; Surface properties

Funding

  1. King Abdullah University of Science and Technology (KAUST) , Office of Sponsored Research (OSR) [OSR-2017-CRG6-3388.01]

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Repairing damaged composite parts using the scarf technique requires carefully selecting treatment methods for the composite surface. Laser treatment, specifically using a CO2 laser, has shown potential in improving joint strength by altering the surface characteristics. This study investigates the influence of CO2 laser treatment on the surface characteristics and joint strength of carbon fiber-reinforced plastic laminates. The results suggest that a laser fluence of 3.6 J/m(2) is safe and can improve joint strength in certain types of laminates.
Repairing damaged composite parts using scarf technique requires a careful selection of treatment methods for composite surface. Laser treatment is one of the emerging techniques to treat the milled composite surface by unlocking various levels of morphological changes and, thus, optimizing joint strength. However, laser parameters, e.g., energy density (fluence), should be carefully determined to ensure the acceptable structural recovery. Here, the influence of CO2 laser with relatively high fluence (ablation effect) on the surface characteristics (roughness, morphology, wettability) and scarf joint strength with associated failure modes of unidirectional (UD) and quasi-isotropic (QI) carbon fiber-reinforced plastic (CFRP) laminates is studied. We found that the ablation effect using CO2 laser at 3.6 J/m(2) was considered safe for UD laminates as their joint strength was comparable with that treated by manual sanding. The ablation at higher fluence (8.4 J/m(2)) reduced the joint strength in UD laminates due to severe damage occurred in 0 degrees fibers that triggered adhesive failure. In QI laminates, 3.6 J/m(2) laser fluence could improve joint strength since the cohesive failure was activated in off-axis plies (90 degrees, +45 degrees, -45 degrees).

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