Delamination properties and in situ damage monitoring of z-pinned carbon fiber/epoxy composites-Reference-Cited by-同舟云学术

Delamination properties and in situ damage monitoring of z-pinned carbon fiber/epoxy composites

Published:2021-01-01 Issue:1 Volume:28 Page:415-425
ISSN:2191-0359
Container-title:Science and Engineering of Composite Materials
language:en
Short-container-title:

Author:

Che Zhe¹,Wang Han²,Wang Shaokai¹³,Gu Yizhuo¹³,Li Min¹³

Affiliation:

1. Key Laboratory of Aerospace Advanced Materials and Performance (Ministry of Education), School of Materials Science and Engineering, Beihang University , No. 37 Xueyuan Road, Haidian District , Beijing 100191 , China

2. State Key Laboratory of Fluid Power and Mechatronic System, School of Mechanical Engineering, Zhejiang University , Hangzhou 310027 , China

3. Ningbo Institute of Technology, Beihang University , Ningbo 315800 , China

Abstract

Abstract Carbon-fiber-reinforced composites with layer stacking structures are sensitive to delamination crack. To improve the interlaminar properties and further explore the capability of in situ damage monitoring of the laminate, CCF300 and CCF800 carbon fiber pins were selected to fabricate the z-pinned composites. Compared with the control sample, the G IC values of CCF300 and CCF800 z-pinned composites are increased by 398 and 378%, respectively. This indicates that the delamination resistance improvement of the laminates is dominated by the z-pin debonding and pull-outs. The electrical resistance of the laminates was utilized to in situ monitor the crack propagation within the composite laminate. The results show that the presence of the z-pins enhances the sensitivity of damage detection. The ΔR/R 0 of CCF800 z-pinned composite is nearly three times that of the control sample at the moment the crack length reaches 110 mm. Crack length–displacement curves were obtained according to the relationship between ΔR and Δa, which clearly displayed the steady or stick-slip crack growth of the laminates with or without z-pins, respectively. Visualization of the crack growth process can provide a novel method for the delamination failure analysis of the composite.

Publisher

Walter de Gruyter GmbH

Subject

Materials Chemistry,Ceramics and Composites

Link

https://www.degruyter.com/document/doi/10.1515/secm-2021-0041/pdf

Reference38 articles.

1. Hamer S, Leibovich H, Intrater R, Zussman E, Sherman D. Mode I interlaminar fracture toughness of Nylon 66 nanofibrilmat interleaved carbon/epoxy laminates. Polym Compos. 2011;32(11):1781–9.

2. Arai M, Hirokawa JI, Hanamura Y, Ito H, Hojo M, Quaresimin M. Characteristic of mode I fatigue crack propagation of CFRP laminates toughened with CNF interlayer. Compos Part B. 2014;65:26–33.

3. Wang J, Ma C, Chen G, Dai P. Interlaminar fracture toughness and conductivity of carbon fiber/epoxy resin composite laminate modified by carbon black-loaded polypropylene non-woven fabric interleaves. Compos Struct. 2020;234:111649.

4. An WJ, Kim CH, Choi JH, Kweon JH. Static strength of RTM composite joint with I-fiber stitching process. Compos Struct. 2019;210:348–53.

5. Ahmed S, Zheng X, Zhang D, Yan L. Impact response of carbon/kevlar hybrid 3D woven composite under high velocity impact: experimental and numerical study. Appl Compos Mater. 2020;27(3):1–21.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The delamination performance of composite laminates with bionic high toughness regions;Composites Part A: Applied Science and Manufacturing;2024-06

2. Non-contact detection of the interfacial microdefects in metal/CFRP hybrid composites using air-coupled laser ultrasound;Structural Health Monitoring;2024-03-16

3. Investigation on fracture behavior of unidirectional bamboo laminate with self-tapping screws reinforcement;Case Studies in Construction Materials;2023-12

4. Aligned carbon nanotube composite belts stitching of laminated composites for enhanced fracture toughness and enriched functionalities;Polymer Composites;2022-12-09