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Full Length Article | Open Access

Improvement of interleaving Aramid pulp micro-fibers on compressive strengths of carbon fiber reinforced polymers with and without impact

Fei CHENGa,b( )Guangming YANGaYunsen HUcBingyan YUANcXiaozhi HUc
School of Materials Science and Engineering, Southwest University of Science and Technology, Mianyang 621010, China
Engineering Research Center of Biomass Materials, Ministry of Education, Southwest University of Science and Technology, Mianyang 621010, China
Department of Mechanical Engineering, University of Western Australia, Perth WA6009, Australia

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Compressive strengths and elastic moduli of Carbon Fiber Reinforced Polymer (CFRP) composites can be noticeably improved by multiple ultra-thin interlays with non-woven Aramid Pulp (AP) micro/nano-fibers. 10-ply CFRP specimens with 0, 2, 4, 6, 8 g/m2 AP were tested under uniaxial compression. Those flexible AP fibers, filling the resin-rich regions and further constructing the fiber bridging at the ply interfaces, can effectively suppress delamination growth and lead to very good improvements both in the compressive strength and the elastic modulus. The CFRP specimen with an optimum interlay thickness has a distinct shear failure mode instead of the typical delamination cracking along the direction of continuous carbon fibers. Compressive Strengths After Impacts (CAI) of 12.35 J were also measured, up to 90% improvement in CAI has been observed. It is concluded those ultra-thin interlays of non-woven AP micro/nano-fibers are beneficial to design and manufacture “high strength” CFRP composites.

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Chinese Journal of Aeronautics
Pages 459-470

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Cite this article:
CHENG F, YANG G, HU Y, et al. Improvement of interleaving Aramid pulp micro-fibers on compressive strengths of carbon fiber reinforced polymers with and without impact. Chinese Journal of Aeronautics, 2023, 36(10): 459-470. https://doi.org/10.1016/j.cja.2023.08.009

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Received: 18 September 2022
Revised: 25 October 2022
Accepted: 14 December 2022
Published: 18 August 2023
© 2023 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/).