期刊文献+

热压烧结制备SiC_w/ZrB_2陶瓷复合材料的研究 被引量:6

ZrB_2 Matrix Ceramic Composites by Hot-Pressed and SiC Whisker Reinforced
下载PDF
导出
摘要 在烧结温度和压力为1800℃和30MPa条件下热压烧结制备ZrB2-20%(体积分数,下同)SiCw陶瓷复合材料,并研究两种不同SiC晶须对材料的显微组织与力学性能的影响。结果表明,复合材料的弯曲强度和断裂韧性与SiC晶须的长径比有关,长径比越大材料的性能越好,弯曲强度和断裂韧性最高为651MPa和5.97MPa·m1/2;与单相的ZrB2材料及SiC颗粒增强ZrB2复合材料相比,断裂韧性有显著提高;其主要增韧机制为裂纹偏转、晶须桥连和拔出。 ZrB2 based ceramic matrix composites containing two kinds of SiC whiskers were produced at 1800℃ under a uniaxial load of 30 MPa by hot-pressing. The microstructure and mechanical properties of the two composites were investigated. The results show that the flexural strength and fracture toughness of composites are related with the aspect ratio of SiC whisker: the larger the aspect ratio is, the better of the properties of materials. The maximum flexural strength and the fracture toughness are 651 MPa and 5.97 MPa.m^1/2, respectively. The mechanical properties, especially the fracture toughness, are much higher than that of monolithic ZrB2 and SiC particles reinforced ZrB2 composites due to the main toughening mechanisms of crack deflection, whisker bridging and pullout.
机构地区 哈尔滨工业大学
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2009年第9期1634-1637,共4页 Rare Metal Materials and Engineering
基金 国家自然科学基金(50602010)
关键词 ZRB2 SIC晶须 热压烧结 力学性能 ZrB2 SiC whisker hot-pressing sintering mechanical property
  • 相关文献

参考文献16

  • 1Upadhya K, Yang J M, Hoffman W P. Am Ceram Soc Bull[J], 1997, 76:51.
  • 2Levine S R, Opila E J, Halbig M C et al. JEuro Ceram Soc[J], 2002, 22:2757.
  • 3Adam L G, William G F, Gregory E H. J Am Ceram Soc[J], 2004, 87:1170.
  • 4Becher P F, Wei G C. JAm Ceram Soc[J], 1984, 67:267.
  • 5Frank D G, John J P. JAm Ceram Soc[J], 1985, 68(181): C200.
  • 6Deng J X, Ai X. Materials Research Bulletin[J], 1998, 33:575.
  • 7Jiang X, Chen Y, Sun X W. J Euro Ceram Soc[J], 1999, 19: 2033.
  • 8Lin G Y, Lei T C, Wang S X. Ceram Intern[J], 1996, 22:199.
  • 9Monteverde F, Guicciardi S, Bellosi A. Mater Sci Eng A[J], 2003, 346:310.
  • 10Sun L, Pan J S. MaterLett[J], 2002, 53:63.

二级参考文献8

  • 1李金平,孟松鹤,韩杰才,易法军,许承海.双相颗粒混合增韧ZrB_2陶瓷复合材料的研究[J].哈尔滨工业大学学报,2005,37(6):727-729. 被引量:12
  • 2Levine Stanley R,Opila Elizabeth J,Halbig Michael C,et al.Evaluation of ultra-high temperature ceramics for aeropropulsion use[J].Journal of the European Ceramic Society,2002,22:2757-2767.
  • 3Opeka M M,Talmy I G,Zaykoski J A.Oxidation-based materials selection for 2000 ℃+hypersonic aerosurfaces:Theoretical considerations and historical experience [J].Journal of Materials Science,2004,39:5887-5904.
  • 4Opeka Mark M,TalmyInna G,Wuchina Eric J,et al.Mechanical,thermal,and oxidation properties of refractory hafnium and zirconium compounds[J].Journal of the European Ceramic Society,1999,19:2405-2414.
  • 5Gasch M,Ellerby D,Irby E,et al.Processing,properties and arc jet oxidation of hafnium diboride/silicon carbide ultra high temperature ceramics [J].Journal of Materials Science,2004,39:5925-5937.
  • 6Wang C R,Yang J M,Hoffman W.Thermal stability of refractory carbide/boride composites [J].Materials Chemistry and Physics,2002,74:272-281.
  • 7张文.突破热障[J].国外科技动态,1998(8):30-31. 被引量:4
  • 8徐强,张幸红,韩杰才,赫晓东.先进高温材料的研究现状和展望[J].固体火箭技术,2002,25(3):51-55. 被引量:41

共引文献9

同被引文献128

引证文献6

二级引证文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部