Preparation and properties of carbon fiber reinforced epoxy resin composites interlaminate-toughened by polyethersulfone ultrafine-fiber non-woven fabric

被引:0
|
作者
Zhang D. [1 ,2 ]
Bao J. [2 ,3 ,4 ]
Zhong X. [2 ,3 ,4 ]
Wang D. [5 ]
Zhang T. [5 ]
Chen X. [1 ,2 ]
机构
[1] AECC Beijing Institute of Aeronautical Materials, Beijing
[2] National Key Laboratory of Advanced Composites, Beijing
[3] AVIC Composite Center, Beijing
[4] AVIC Composite Corporation Ltd., Beijing
[5] Beijing Institute of Fashion Technology, School of Material Science and Technology, Beijing
关键词
blended spinning; carbon fiber; composites; epoxy resin; interlaminar toughing;
D O I
10.13801/j.cnki.fhclxb.20210909.004
中图分类号
学科分类号
摘要
To improve the compression strength after impact of epoxy-based composites, polyethersulfone (PES) ultrafine-fiber non-woven fabric was fabricated from polyethersulfone-Nylon 6 (PES-PA6) blended fibers using solution-stripping method, which is more suitable for batch preparation. Then the obtained non-woven fabric was applied in the interlaminar toughing of carbon fiber reinforced epoxy resin-based composites. Interlaminar fracture toughness under mode I (GIC), interlaminar fracture toughness under mode II (GIIC), compressive strength after impact (CAI) and interlaminar fracture micro-morphology of composites were tested to research the influence of the non-woven fabric on the interlaminar toughness of composites and the corresponding mechanism of interla-minar toughing. The result indicates that after epoxy resin-based composites are interlaminate-toughened with the non-woven fabric, the GIC value is raised to 312 J/m2 from 289 J/m2 and GIIC value is improved to 3649 J/m2 from 1391 J/m2. Also, the post-impact damage area of tested specimens is reduced from 1050 mm2 to 204 mm2 after toughing treatment, and the corresponding post-impact compressive strength is increased from 228 MPa to 307 MPa. © 2022 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
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页码:3767 / 3775
页数:8
相关论文
共 23 条
  • [1] CHEN Xiangbao, ZHANG Baoyan, XING Liying, Application and development of advanced polymer matrix composites, Materials China, 28, 6, pp. 2-12, (2009)
  • [2] DU Shanyi, Advanced composite materials and aerospace engineering, Acta Materiae Compositae Sinica, 24, 1, pp. 1-12, (2007)
  • [3] MA Limin, ZHANG Jiazhen, YUE Guangquan, Et al., Application of composites in new generation of large civil aircraft[J], Acta Materiae Compositae Sinica, 32, 2, pp. 317-322, (2015)
  • [4] ENDO M., Composites for aircraft and aerospace application[J], Sen'I Gakkaishi, 70, 9, pp. 508-511, (2014)
  • [5] BAO Jianwen, ZHONG Xiangyu, ZHANG Daijun, Et al., Progress in high strength intermediate modulus carbon fiber and its high toughness resin matrix composites in China, Journal of Materials Engineering, 48, 8, pp. 33-48, (2020)
  • [6] CHEN Shaojie, Composite technology and large aircraft, Acta Aeronautica et Astronautic Sinica, 29, 3, pp. 605-610, (2008)
  • [7] LIU Daijun, CHEN Yali, Application of advanced polymer matrix composites in aviation industry, Journal of Materials Engineering, S1, pp. 194-198, (2008)
  • [8] QIAO Haitao, LIANG Bin, ZHANG Junying, Et al., Development and application of adhesive materials for advanced composite bonding[J], Journal of Materials Engineering, 46, 12, pp. 38-47, (2018)
  • [9] ZHANG Zonghua, LIU Gang, ZHANG Hui, Et al., Influence of nano-alumina particles on glass transition temperature of high-performance epoxy resin, Journal of Materials Engineering, 9, pp. 39-44, (2014)
  • [10] LIU Gang, ZHANG Daijun, ZHANG Hui, Et al., Mechanical properties of nanoparticles modified epoxy matrix and composites, Journal of Materials Engineering, 1, pp. 47-53, (2010)