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

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Summary

Introduction

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

Type of Test Piece
Test Piece Preparation Process
Analysis of Failure Modes
Analysis of Failure Mechanisms
Comparison with Non Z-pins Reinforced Adhesive Joint
Stress Analysis
Unit Type and Material Parameters
Three Dimensional Distributions of Interface Stress
Findings
Conclusion
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