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合金反应熔渗法制备C/C-SiC-HfC复合材料(英文) 被引量:5

C/C-SiC-HfC Composite Prepared by Alloyed Reactive Melt Infiltration
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摘要 采用22Hf78Si合金反应熔渗法制备了高性能低成本的C/C-SiC-HfC复合材料。首先采用化学气相渗透法增密碳纤维预制体得到多孔C/C复合材料预制体,然后在1700℃下反应熔渗22Hf78Si合金制备得到C/C-SiC-HfC复合材料。XRD分析表明复合材料由碳、SiC和HfC相组成。C/C-SiC-HfC复合材料的抗弯强度为237MPa,断裂模式为假塑性断裂模式。采用激光测试了反应熔渗C/C-SiC-HfC复合材料的抗烧蚀性能,复合材料的线烧蚀率为0.038mm/s,大大低于C/SiC复合材料的线烧蚀率0.081mm/s。烧蚀后复合材料烧蚀表面形成了一层HfO2烧蚀层,有效提高了复合材料的抗烧蚀性能。 A high performance and low cost HfC modified C/C-SiC composite (C/C-SiC-HfC) was prepared by 22Hf78Si alloyed melt infiltration. Carbon fiber felt was firstly densified by pyrolytic carbon using chemical vapor infiltration to obtain a porous C/C preform. 22Hf78Si alloyed melt was then infiltrated into the porous preform at 1700℃ to prepare the C/C-SiC-HfC composite. XRD analysis indicates that the resulting composite is composed of carbon, SiC and HfC. The as-received C/C-SiC-HfC composite, with the flexural strength of 237MPa, displays a pseudo-ductile fracture behavior. Ablation resistance of C/C-SiC-HfC composite was tested by a pulse laser. The linear ablation rate is 0. 038ram/s, which is much lower than that of C/SiC composite, 0. 081mm/s. A HfO2 barrier layer is formed on the ablation surface, which effectively protects the composite from severe ablation.
作者 张鹏
出处 《材料科学与工程学报》 CAS CSCD 北大核心 2015年第2期173-177,共5页 Journal of Materials Science and Engineering
关键词 C/C-SiC-HfC复合材料 微观组织 抗弯强度 抗烧蚀性能 反应熔渗法 C/C-SiC-HfC composite microstructure flexural strength ablation resistance reactive melt infiltration
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参考文献12

  • 1Y.H. Zhang, Z.C. Xiao, J.P. Wang, J.F. Yang, Z. H. Jin. Effect of pyrocarbon content in C/C preforms on microstructure and mechanical properties of the C/C-SiC composites[J]. Mater Sei Eng A, 2009, 502(1-2):64-69.
  • 2张玉娣,张长瑞.CVI-PIP工艺制备C/SiC复合材料及其显微结构研究[J].材料科学与工程学报,2004,22(5):657-659. 被引量:12
  • 3W. Krenkel. Application of fiber reinforced C/C-SiC ceramic [J]. Ceram. Forum. Int., 2003, 80(8):31-38.
  • 4Z. Wang, S. M, Dong, Y.S. Ding, et al. Mechanical properties and microstructures of C/SiC-ZrC composites using T700SC carbon fibers as reinforcements [J]. Ceram. Int. ,2011, 37.. 695 -700.
  • 5S.F. Tang, J.Y. Deng, S.J. Wang, W.C. Liu, K. Yang. Ablation behaviors of ultra-high temperature ceramic composites [J]. Mater. Sci. Eng., A2007, 465:1-7.
  • 6H.J. Li, D.J. Yao, Q. G. Fu, et al. Anti-oxidation and ablation properties of carbon/carbon composites infiltrated by hafnium boride [J]. Carbon, 2013, 52:418-426.
  • 7S.P. Li, K.Z. Li, H.J. Li, Y.L. Li, Q.L. Yuan. Effect of HfC on the ablative and mechanical properties of C/C composites [J]. Materials Science and Engineering A, 2009, 517:61-67.
  • 8C. Li, K. Li, H. Li, H. Ouyang, Y. Zhang, L. Guo. Mechanical and thermophysical properties of carbon/ carboncomposites with hafnium carbide[J]. Ceram. Int. , 2013, 39(6): 6769-6776.
  • 9Y.G. Tong, S. X. Bai, H. Zhang, K. Chen. C/C-SiC composite prepared by Si-10Zr alloyed melt infiltration [J]. Ceram. Int., 2012, 38:3301-3307.
  • 10Y. Wang, X.J. Zhu, L.T. Zhang, L.F. Cheng. Reaction kineties and ablation properties of C/C-ZrC composites fabricated by reactive melt infiltration [J]. Ceram. Int., 2011, 37(4): 1277-1283.

二级参考文献4

  • 1Sanokawa Yutaka, et al. Application of Continuous Fiber Reinforced Silicon Carbide Matrix Composites to a Ceramic gas terbine Model for Automobiles[J]. Ceramic Engineering & Science Proceedings, 1997,(4) :221 ~ 228.
  • 2B,Harnisch, et al. Ultralight Weight C/SiC Mirrors and Structures[J].ESA Bulletin 95,1998, (8): 148 ~ 152.
  • 3A. Ortona, et al. SiC-SiCf CMC manufacturing by hybrid cvi-pip techniques: process optimization[ J ]. Fusion Engineering and Design, 2000,(51-52) :159~ 163.
  • 4Vishak Sampath, Srinivas Palanki. Optimization of Isothermal-Isobaric Chemical Vapor Infiltratione [ J ]. Computers chemical engnineer,1998, (22) :773 ~ 776.

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