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石墨化处理对三维针刺C/C复合材料力学性能的影响 被引量:3

Effects of graphitization on mechanical properties of 3D needled C/C composites
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摘要 以T700碳纤维三维针刺整体毡为预制体,利用高压液相浸渍-碳化周期循环致密工艺制备三维针刺中间相沥青基C/C复合材料。用XRD、SEM及力学性能测试研究了三维针刺C/C复合材料的微观结构与弯曲断裂机制。结果表明:随着浸渍-碳化次数的增加,三维针刺C/C复合材料的密度、抗弯强度和杨氏模量逐渐增大,石墨化处理使三维针刺C/C复合材料的石墨层间距减小,石墨化度提高。经2800℃石墨化处理后,三维针刺C/C复合材料中纤维与基体间界面结合减弱,复合材料的抗弯强度减小并表现出韧性断裂特征。 Three dimensional(3D) needled mesophase pitch-based C/C composites were manufactured by high pressure liquid impregnation-carbonization and graphitized at 2600 ℃ and 2800 ℃.The polyacrylonitrile(PAN) based carbon fiber(T700) preform was prepared by three-dimensional needling.The microstructure and flexural fracture mechanism of the 3D needled C/C composites were characterized by X-ray diffraction(XRD),scanning electron microscopy(SEM) and mechanical property tests,respectively.Results indicate that the bulk density,flexural strength and Young’s modulus of the 3D needled mesophase pitch-based C/C composites increase with increasing of impregnation-carbonization times.After graphitization,the graphite layer distances of C/C composites decrease and graphitization degrees increase.When graphitizing at 2800 ℃,the flexural strength of the 3D needled C/C composite decreases because the interface bonding between carbon matrix and carbon fibers is weakened,and the 3D needled C/C composites show non-brittle fracture behavior.
出处 《材料热处理学报》 EI CAS CSCD 北大核心 2011年第2期10-15,共6页 Transactions of Materials and Heat Treatment
基金 国家自然科学基金(50672004) 国家高技术研究发展计划("863"计划)资助项目(2008AA03Z513)
关键词 C/C复合材料 中间相沥青 石墨化 微观结构 力学性能 C/C composites mesophase pitch graphitization microstructure mechanical property
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  • 1韩杰才,胡平,张幸红,孟松鹤.超高温材料的研究进展[J].固体火箭技术,2005,28(4):289-294. 被引量:58
  • 2王俊山,李仲平,敖明,许正辉,刘朗,胡子君,彭维周.掺杂难熔金属碳化物对炭/炭复合材料烧蚀机理的影响[J].新型炭材料,2006,21(1):9-13. 被引量:20
  • 3田庭燕,张玉军,孙峰,魏红康.ZrB_2-SiC复合材料抗氧化性能研究[J].陶瓷,2006(5):19-21. 被引量:8
  • 4周红英,舒武炳,刘建军,程文,邹武,黄寒星.高温热处理与C/C复合材料性能关系研究[J].固体火箭技术,2007,30(1):68-71. 被引量:13
  • 5Cheng L F. Corrosion of a 3D-C/SiC composite in salt vapor environments[J].Carbon,2002,(06):877.
  • 6Yin X W. Thermal shock behavior of 3-dimensional C/SiC composite[J].Carbon,2002,(06):905.
  • 7Schrnidt S. Advanced ceramic matrix composite materials for current and future propulsion technology applications[J].Acta Astronautica,2004,(3-9):409.
  • 8Vaidyaraman S. C/SiC material evaluation for aircraft brake applications[A].Munich,Germany,2001.802.
  • 9Krenkel W. C/C-SiC composites for hot structures and advanced friction systems[J].Ceramic Engineering and Science Proceedings,2003,(04):583.
  • 10Cai Y Z. Low-cost preparation and frictional behaviour of a three-dimensional needled carbon/silicon carbide composite[J].Journal of the European Ceramic Society,2009,(03):497.

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