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

被引:6
|
作者
Cheng, Fei [1 ,2 ]
Yang, Guangming [1 ]
Hu, Yunsen [3 ]
Yuan, Bingyan [3 ]
Hu, Xiaozhi [3 ]
机构
[1] Southwest Univ Sci & Technol, Sch Mat Sci & Engn, Mianyang 621010, Peoples R China
[2] Southwest Univ Sci & Technol, Engn Res Ctr Biomass Mat, Minist Educ, Mianyang 621010, Peoples R China
[3] Univ Western Australia, Dept Mech Engn, Perth, WA 6009, Australia
基金
中国国家自然科学基金;
关键词
Compressive strength; Carbon Fiber Reinforced Polymer (CFRP); Aramid pulp; Interleaving; Interfacial reinforcing; II DELAMINATION TOUGHNESS; EPOXY COMPOSITES;
D O I
10.1016/j.cja.2023.08.009
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.(c) 2023 Production and hosting by Elsevier Ltd. on behalf of 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/).
引用
收藏
页码:459 / 470
页数:12
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