Effect of low-temperature plasma surface modification on the adhesive performance of CFRP

被引:0
|
作者
Wang D. [1 ]
Li Y. [1 ]
Liu Z. [2 ]
Zou T. [2 ]
机构
[1] College of Aeronautical Engineering, Civil Aviation University of China, Tianjin
[2] College of Safety Science and Engineering, Civil Aviation University of China, Tianjin
基金
中国国家自然科学基金;
关键词
adhesive property; CFRP; low temperature plasma; surface modification; wettability;
D O I
10.13801/j.cnki.fhclxb.20220516.003
中图分类号
学科分类号
摘要
Ar, N2 and O2 were used as low-temperature plasma excitation gases to treat the surface of carbon fiber reinforced plastics (CFRP). The effects of plasma gas, discharge power and treatment time on the physicochemical properties, including wettability, roughness, microscopic morphology and chemical components of CFRP surface, were characterized by contact angle measurement, AFM, SEM and XPS. The adhesive joint property was investigated through tensile shear experiment and failure morphology analysis. Compared with untreated, the tensile shear strength of CFRP adhesive joints after Ar, N2 and O2 plasma treatment can significantly improve the bonding performance of CFRP, and when the plasma discharge power is 800 W and treatment time is 20 s, the adhesive joint strength increases by 138%, 172% and 253%, respectively. The surface test analysis shows that the improvement of CFRP adhesive strength after argon plasma treatment is mainly induced by improving the surface cleanliness and increasing the surface area for interfacial adhesive, and the failure modes of samples changes from interfacial failure to mixed failure mode with cohesive failure as the main mode. Compared with Ar, a greater number of polar chemical groups (− NH2) are generated on the CFRP surface after N2 plasma treatment, which increase the surface activity and further improve the interfacial adhesive strength between CFRP and adhesive. Compared with the above two gases, O2 plasma etch the CFRP surface more vigorously, as well as reorganize the surface chemical groups, forming a more polar − COOH functional group, so that the specimen adhesive strength is improved most effectively, and the specimen failure mode changes from interface failure to substrate failure. In addition, under the excessively high density and energy of the active particles, the adhesive performance will be reduced to some extent with the expansion of the pores by plasma etching. © 2023 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
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页码:2026 / 2037
页数:11
相关论文
共 31 条
  • [1] MA Limin, ZHANG Jiazhen, YUE Guangquan, Et al., Application of composite in new generation of large civil aircraft[J], Acta Materiae Compositae Sinica, 32, 2, pp. 317-322, (2015)
  • [2] KATNAM K B, DA SILVA L F M, YOUNG T M., Bonded repair of composite aircraft structures: A review of scientific challenges and opportunities[J], Progress in Aerospace Sciences, 61, pp. 26-42, (2013)
  • [3] BARILE C, CASAVOLA C, DE C F., Mechanical comparison of new composite materials for aerospace applications[J], Composites Part B: Engineering, 162, pp. 122-128, (2019)
  • [4] SUN Zhenqi, WU Anru, Application of advanced composite in aircraft structures, Materials Reports, 29, 11, pp. 61-64, (2015)
  • [5] DENG S, DJUKIC L, PATON R, Et al., Thermoplastic-epoxy interactions and their potential applications in joining composite structures− A review[J], Composites Part A: Applied Science and Manufacturing, 68, pp. 121-132, (2015)
  • [6] QIN G, NA J, MU W, Et al., Effect of continuous high temperature exposure on the adhesive strength of epoxy adhesive CFRP and adhesively bonded CFRP-aluminum alloy joints[J], Composites Part B: Engineering, 154, pp. 43-55, (2018)
  • [7] PARK S M, ROY R, KWEON J H, Et al., Strength and failure modes of surface treated CFRP secondary bonded single-lap joints in static and fatigue tensile loading regimes[J], Composites Part A: Applied Science and Manufacturing, 134, (2020)
  • [8] DI B Y, JOSHI S C, ONG L S., Interfacial bonding between CFRP and mechanically-treated aluminum liner surfaces for risers[J], Composite Structures, 188, pp. 374-386, (2018)
  • [9] BUCHMANN C, LANGER S, FILSINGER J, Et al., Analysis of the removal of peel ply from CFRP surfaces[J], Composites Part B: Engineering, 89, pp. 352-361, (2016)
  • [10] HU Y, YUAN B, CHENG F, Et al., NaOH etching and resin pre-coating treatments for stronger adhesive bonding between CFRP and aluminium alloy[J], Composites Part B: Engineering, 178, (2019)