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碳纤维湿法缠绕用高模量高韧性环氧树脂基体 被引量:16

TOUGHNESS EPOXY RESIN WITH HIGH MODULUS FOR CARBON FIBER WET FILAMEMT WINDING
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摘要 设计了一系列针对碳纤维湿法缠绕的环氧树脂基体,测试了树脂浇注体及其复合材料的力学性能和热机械性能,研究了树脂基体对碳纤维复合材料界面性能的影响。试验结果表明,对韧性树脂体系,树脂基体的模量是发挥纤维强度的关键因素,模量的提升将大幅提高复合材料的综合性能。经复配和优化的树脂体系兼具高模量和高韧性,其T700碳纤维复合材料NOL环拉伸强度达到2480MPa,T800碳纤维复合材料NOL环拉伸强度达到2780MPa,玻璃化温度(Tg)超过200℃,具有优异的界面性能和耐热性能。 High-performance carbon fiber has been widely used in commercial and military fields because of its high strength, light weight and high stiffness. A series of epoxy resins were designed for carbon fiber wet filament winding. Meanwhile the mechanical property and thermal mechanical property of these resins and their carbon fiber composites were analyzed. The effect of resin matrix' s structure and property on the composite was studied based on the analysis. The results show that, for stiffness resins, the modulus of matrix is a key property to gain high-performance carbon fiber composite. With the help of the optimized resin system, the carbon fiber composite possess excellent interfacial properties and heat-resistance properties. The tensile strength of T700 CF composite NOL rings is 2480MPa, that of T800 CF composite NOL rings is 2780MPa, and the glass transition temperature (Tg) is higher than 200 ℃.
出处 《玻璃钢/复合材料》 CAS CSCD 2009年第2期72-77,共6页 Fiber Reinforced Plastics/Composites
关键词 碳纤维 湿法缠绕 环氧树脂 复合材料 carbon fiber wet filament winding epoxy resin, composite
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参考文献17

  • 1Donnet JB, Bansal RC. Carbon Fiber, 2nd edn. New York: Marcel Dekker, 1990.
  • 2Bader M. G.. Selection of composite materials and manufacturln- groutes for cost-effective performance [ J ]. Composites A, 2002, 33 : 913-934.
  • 3Peter Morgan. Carbon Fibers and their Composites. New York : Taylor & Franicis Group, 2005.
  • 4Shanglin Gao, Mader E, Zhandarov SF. Carbon fiber and composites with epoxy resins : topography, fractography and interphases [ J ]. Carbon, 2004, 42(3) : 515-529.
  • 5Tanaka Y, Mika TF. In Epoxy Resins, Chemistry and Technology. In: May CA Tanaka Y, editors. New York: Dekker, 1973.
  • 6陈伟明,王成忠,周同悦,杨小平.高性能T800碳纤维复合材料树脂基体[J].复合材料学报,2006,23(4):29-35. 被引量:44
  • 7陈平,蹇锡高,陈辉,高巨龙,韩冰,朱兴松.碳纤维复合材料发动机壳体用韧性环氧树脂基体的研究[J].复合材料学报,2002,19(2):24-27. 被引量:40
  • 8苏祖君,梁国忠,曾金芳,王华强.湿法缠绕用次中温固化的环氧树脂配方[J].纤维复合材料,2004,21(3):6-8. 被引量:13
  • 9Weiming Chen, Yunhua Yu, Peng Li, Chengzhong Wang, Tongyue Zhou, Xiaoping Yang. Effect of new epoxy matrix for T800 carbon fiber/epoxy filament wound composites [ J ]. Composites Science and Technology, 2007, 67 (9) : 2261-2270.
  • 10B. W. Knight. The technique of filament winding [ J ]. Composites, 1970, 1(4) : 228-233.

二级参考文献26

  • 1王斌,金志浩,丘哲明,刘爱华.几种高性能纤维的表面性能及其对界面粘接的影响[J].固体火箭技术,2004,27(3):224-228. 被引量:20
  • 2韩冰.碳纤维复合材料火箭发动机壳体用韧性环氧树脂基体[M].哈尔滨:哈尔滨理工大学,2000.9-10.
  • 3H E Kissinger.Analytical Chemistry,1957,29:1072
  • 41 w Crane,et al.Journal of Polymer Scienee,1972,12:120
  • 5谢丹 过松如 杭颂.复合材料缠绕制品的环氧树脂配方研究[M]..第十一届全国复合材料学术会议论文集[C].,2000.45-48.
  • 6Fjeldly A,Olsen T,Rysjedal J H,et al.Influence of the fiber surface treatment and hot wet environment on the mechanical behavior of carbon/epoxy composites[J].Composites Part A,2001,32(3):373-378.
  • 7Bogoeva-Gaceva G,M(a)der E,H(a)ussler L,et al.Characterization of the surface and interphase of plasma-treated HM carbon fibers[J].Composite Part A,1997,28(5):445-452.
  • 8Hughess J D H.The carbon fiber/epoxy interface:A review[J].Composite Science and Technology,1991,41(2):147-159.
  • 9Lee J,Soutis C.Thickness effect on the compressive strength of T800/924C carbon fibre-epoxy laminates[J].Composites Part A,2005,36(2):213-227.
  • 10Ivens J,Albertsen H,Wevers M,et al.Interlaminar fracture toughness of CFRP influenced by fiber surface treatment Ⅱ:Modeling of the interface effect[J].Composite Science and Technology,1995,54(2):147-159.

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