Abstract
The mechanical properties of Z-pins reinforced composites adhesively bonded single-lap joints (SLJs) under un-directional tension loading are investigated by experimental and numerical methods. Three kinds of joint configurations, including SLJs with three/two rows of Z-pins and “I” array of Z-pins, are investigated by tension test. The failure modes and mechanism of reinforced joints with different Z-pins numbers and alignment are analyzed, and the comparison is performed for the failure strengths of no Z-pins and Z-pins reinforced joints. According to experimental results, failure modes of three kinds of joints are all mixed failure. It turns out that the Z-pins are pulled out ultimately. The strength of joints of more Z-pins at the end of the overlap area is relatively bigger for the joint of the same Z-pins numbers. The strength of joints with Z-pins compared with non Z-pins joints is growing at 16%. Finally, the three-dimensional distribution of interfacial stress in the lap zone of three kinds of Z-pins reinforced joints is simulated, and the numerical results are in good agreement with the experimental results. It is effective that the numerical calculation of stress analysis is verified.
Highlights
Under in-plane tensile load, the joint is seriously affected by shear stress concentration, which can lead to delamination damage of composites
The innovation of this study is to reveal the strengthening mechanism of Z-pins in joint failure, compare the strength of Z-pins reinforced joints with or without Z-pins, conduct experimental research on Z-pins reinforced joints with different arrangement modes, obtain the law of influence of Z-pins distribution mode on joint failure, and analyze the law of distribution of interfacial stress field of Z-pins reinforced single-lap joint
Studying on the failure behavior of composites adhesively bonded single-lap joint (SLJ) with three different Z-pins arrangements by experimental and numerical analysis methods, the failure mode and failure mechanism of each joint are investigated and analyzed, and failure strengths of different types of Z-pins reinforced composite SLJs are compared with non Z-pins reinforced composite SLJs
Summary
Composites are extensively applied to aerospace, automobile, ship, ocean and other fields with the advancement of science and technology. Bianchi et al [22] proposed a finite element model to analyze the strength property, structural deformation and delamination fracture behavior of Z-pins reinforced composites T-joints. For further research of the mechanical behavior of Z-pins reinforced composite SLJs, tensile experiments of unidirectional static load and numerical studies are carried out for Z-pins reinforced SLJs of T700/TDE86 unidirectional composite, and the failure modes and failure mechanisms of three types of Z-pins reinforced composite SLJs are analyzed. The innovation of this study is to reveal the strengthening mechanism of Z-pins in joint failure, compare the strength of Z-pins reinforced joints with or without Z-pins, conduct experimental research on Z-pins reinforced joints with different arrangement modes, obtain the law of influence of Z-pins distribution mode on joint failure, and analyze the law of distribution of interfacial stress field of Z-pins reinforced single-lap joint
Published Version (Free)
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have