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Full Length Article | Open Access

Improving Mode Ⅱ delamination resistance of curved CFRP laminates by a Pre-Hole Z-pinning (PHZ) process

Xuebei TENGaYingjie XUa,b( )Weihong ZHANGaXinyu HUIaWeiwei LIUaChengyan MAc
State IJR Center of Aerospace Design and Additive Manufacturing, Northwestern Polytechnical University, Xi’an 710072, China
Shaanxi Engineering Laboratory of Aerospace Structure Design and Application, Northwestern Polytechnical University, Xi’an 710072, China
Shandong Institute of Non-Metallic Materials, Jinan 250031, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

This paper presents an experimental investigation of the Mode Ⅱ delamination resistance of curved CFRP laminates reinforced with Z-pins. A Pre-Hole Z-pinning (PHZ) process is developed to reduce the in-plane damage of the Z-pinned laminates. The microstructural observation of the Z-pinned laminate specimens indicates that the PHZ process can effectively decrease the defects including the Z-pin offset angle and the area of eyelet zone. The influences of the volume fraction and diameter of Z-pin on the fracture toughness and the delamination crack growth rate of the specimens under End Notch Flexure (ENF) loading are then determined experimentally. The test results show that Z-pin increases the interlayer stiffness of the laminate. The delamination crack growth rate is reduced with the increase of Z-pin diameter and volume fraction, and a reduction up to 40% is achieved compared with the specimens without pins. Furthermore, the Mode Ⅱ fracture toughness is significantly improved with the increase of Z-pin volume fraction. When Z-pin volume fraction increases by 1%, the achieved fracture toughness is about 200% higher compared to the unpinned laminates.

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Chinese Journal of Aeronautics
Pages 316-324

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Cite this article:
TENG X, XU Y, ZHANG W, et al. Improving Mode Ⅱ delamination resistance of curved CFRP laminates by a Pre-Hole Z-pinning (PHZ) process. Chinese Journal of Aeronautics, 2023, 36(2): 316-324. https://doi.org/10.1016/j.cja.2022.09.018

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Received: 10 September 2021
Revised: 21 November 2021
Accepted: 31 December 2021
Published: 26 September 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/).