Study on the interface and failure characteristics of joints between epoxy adhesive and duralumin alloy

In the realm of optomechanical joints, the roughness of the component frequently limits the bonded joint's stability and dependability. This study investigates the failure mechanisms and interfacial stress transfer characteristics of bonded structures with six controlled roughness levels to elucidate roughness-dependent adhesion behavior. Shear experiments have been carried out to analyze the failure mechanisms of bonded joints. The results indicate that when roughness increases, shear strength first rises and subsequently falls. When the surface roughness of the duralumin alloy is 4.2 ± 0.75 μm, the shear strength reaches its maximum value of 11.97 MPa. After analyzing the surface characteristics of substrates with various degrees of roughness, the results show that increasing surface roughness can significantly change the substrate's surface energy, wettability, and contact area while also greatly changing the bonding quality. The fractographic evaluation identified interfacial debonding and cohesive-adhesive hybrid failure as the predominant fracture mechanisms. Specimens exhibiting hybrid failure demonstrated enhanced interfacial load transfer capability through synergistic contributions from both adhesive-substrate bonding and bulk adhesive deformation. This research offers an important reference for the manufacture and application of epoxy adhesive and duralumin alloy joints. It has a guiding significance for improving the performance and reliability of joints.

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Publication Details

Journal
Science Progress
Published
2025-04-01
DOI
https://doi.org/10.1177/00368504251348966
Citations
3
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
2.59

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article

Study on the interface and failure characteristics of joints between epoxy adhesive and duralumin alloy

Xinyu Cang, Dacheng Zhang, Xiangke Zheng, Zhiguo Li et al.
3 citations
Science Progress
Mechanical Behavior of Composites
2.59
article

Study on the interface and failure characteristics of joints between epoxy adhesive and duralumin alloy

Xinyu Cang, Dacheng Zhang, Xiangke Zheng, Zhiguo Li, Ning Hu, Zhengshang Da, Linsen Shu
article en
3 citations

Abstract

In the realm of optomechanical joints, the roughness of the component frequently limits the bonded joint's stability and dependability. This study investigates the failure mechanisms and interfacial stress transfer characteristics of bonded structures with six controlled roughness levels to elucidate roughness-dependent adhesion behavior. Shear experiments have been carried out to analyze the failure mechanisms of bonded joints. The results indicate that when roughness increases, shear strength first rises and subsequently falls. When the surface roughness of the duralumin alloy is 4.2 ± 0.75 μm, the shear strength reaches its maximum value of 11.97 MPa. After analyzing the surface characteristics of substrates with various degrees of roughness, the results show that increasing surface roughness can significantly change the substrate's surface energy, wettability, and contact area while also greatly changing the bonding quality. The fractographic evaluation identified interfacial debonding and cohesive-adhesive hybrid failure as the predominant fracture mechanisms. Specimens exhibiting hybrid failure demonstrated enhanced interfacial load transfer capability through synergistic contributions from both adhesive-substrate bonding and bulk adhesive deformation. This research offers an important reference for the manufacture and application of epoxy adhesive and duralumin alloy joints. It has a guiding significance for improving the performance and reliability of joints.

Science ProgressVol. 108(2)
Xidian University (CN), Shaanxi University of Technology (CN), Chinese Academy of Sciences (CN), Xi'an Institute of Optics and Precision Mechanics (CN)
National Natural Science Foundation of China, Chinese Academy of Sciences Key Project
Affordable and clean energy
Openalex Percentile: Top 11%
Mechanical Behavior of Composites
2.59
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