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Full Length Article | Open Access

Bolt insertion damage and mechanical behaviors investigation of CFRP/CFRP interference fit bolted joints

Yangjie ZUOaTing YUEbRuisong JIANGa( )Zengqiang CAOcLiu YANGd
School of Aeronautics and Astronautics, Sichuan University, Chengdu 610065, China
Xi’an Space Engine Co. Ltd, Xi’an 710100, China
School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China
Xi’an ASN Technology Group Co. Ltd, Xi’an 710072, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Interference fit has advantages in improving fatigue behaviors of composite bolted joints; however, interference fit bolt insertion tends to cause damages in laminates weakening joint mechanical properties. Therefore, an experimental study was conducted to investigate bolt insertion damages of Carbon Fiber Reinforced Polymer (CFRP)/CFRP interference fit bolted joints. Mechanical behaviors of joints were also evaluated experimentally under both quasi-static loads and cyclic loads. Scanning Electron Microscope (SEM) and high-resolution X-ray micro-CT scan were used to examine micro damages in laminates. Damage and failure behaviors of joints were characterized. The results demonstrated that the hole entrance in upper laminate and the laminate boundary near the hole wall were the most critical regions for damages during bolt insertions. However, the influence of those damages on quasi-static failure loads and fatigue failure modes of joints was minimal. Delamination and matrix cracking occurred first in laminates following fiber and matrix fracture in quasi-static tensile tests. Interference fit could improve the fatigue resistance of the laminate hole; however, the bolt seemed to suffer a more critical local fatigue loading condition. This paper can contribute to composite structure designs, especially in understanding damage and failure behaviors of composite bolted joints.

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Chinese Journal of Aeronautics
Pages 354-365

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Cite this article:
ZUO Y, YUE T, JIANG R, et al. Bolt insertion damage and mechanical behaviors investigation of CFRP/CFRP interference fit bolted joints. Chinese Journal of Aeronautics, 2022, 35(9): 354-365. https://doi.org/10.1016/j.cja.2022.01.027

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Received: 25 March 2021
Revised: 06 May 2021
Accepted: 17 June 2021
Published: 03 February 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).