期刊文献+

添加Al对MSI制备C/C-SiC复合材料组织和力学性能的影响 被引量:14

Influence of adding Al on the microstructure and mechanical properties of C/C-SiC composites fabricated by MSI
在线阅读 下载PDF
导出
摘要 以聚丙烯腈(PAN)基炭纤维(Cf)针刺整体毡为预制体,用化学气相渗透(CVI)法制备炭纤维增强炭基体(C/C)的多孔坯体,采用熔融渗硅(MSI)法制备C/C-SiC复合材料,研究了渗剂中添加Al对复合材料组织结构和力学性能的影响。结果表明:C/C坯体反应溶渗硅后复合材料的物相组成为SiC相、C相及残留Si相。随着渗剂中Al量的增加,材料组成相中的Al相也增加而其它相减少;SiC主要分布在炭纤维周围,残留Si相分布在远离炭纤维处,而此处几乎不含Al;当渗剂中Al量由0增加到10%时,复合材料的抗弯强度由116.7 MPa增加到175.4 MPa,提高了50.3%,断裂韧性由5.8 MPa.m1/2增加到8.6 MPa.m1/2,提高了48.2%。Al相的存在使复合材料基体出现韧性断裂的特征。 C/C-SiC composites were fabricated by molten silicon infiltration (MSI) to C/C preforms prepared by chemical vapor infiltration (CVI). The influences of adding Al in molten Si infiltrating agent on the microstructure and mechanical properties of the composites was studied. The results show that the composites fabricated by infiltrating Si into C/C preforms contain SiC, C and residual Si phases. With the increasing of the amount of adding Al in the agent, the amount of Al phase in the composites increases and the amounts of other phases such as SiC and Si phase decrease. SiC phase distributes around the carbon fiber, and Si phase exists far away from the carbon fiber where there is nearly no Al phase. The bending strength and the fracture toughness increase with the increase of the amount of adding Al. When the amount of Al increases from 0 to 10%, the bending strength increases from 116.7 MPa to 175.4 MPa and the fracture toughness from 5.8 MPa·m^1/2 to 8. 6 MPa·m^1/2 , that is, by 50.3% and 48.2% respectively. The Al phase makes the fracture mechanism of the composite become toughness fracture.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2006年第5期34-38,共5页 Acta Materiae Compositae Sinica
基金 国家自然科学基金项目(50472078) 高校博士点基金项目(20040533006)
关键词 C/C-SIC复合材料 C/C坯体 熔渗Si 添加Al 显微组织 力学性能 C/C- SiC composite C/C preform molten silicon infiltration adding Al microstructure mechanical properties
作者简介 通讯作者:易茂中,教授,博士生导师,主要从事C/C、C/C-陶瓷复合材料、材料摩擦学、材料表面工程方面的研究E-mail:yimaozhong@126.com
  • 相关文献

参考文献15

  • 1傅恒志.未来航空发动机材料面临的挑战与发展趋向[J].航空材料学报,1998,18(4):52-61. 被引量:132
  • 2Katsumi Yoshida,Budiyanto,Masamitsu Imai,et al.Processing and microstructure of silicon carbide fiber-reinforced silicon carbide composite by hot pressing[J].Journal of Nuclear Materials,1998,258/263(2):1960-1965.
  • 3王艳香,谭寿洪,江东亮.反应烧结碳化硅的研究与进展[J].无机材料学报,2004,19(3):456-462. 被引量:29
  • 4曹英斌,张长瑞,陈朝辉,周新贵.C_f/SiC陶瓷基复合材料发展状况[J].宇航材料工艺,1999,29(5):10-14. 被引量:19
  • 5Hermann Hald.Operational limits for reusable space transportation systems due to physical boundaries of C/SiC materials[J].Aerospace Science and Technology,2003,7(8):551-559.
  • 6Appiah F A,Wang Z L,Lackey W J.Characterization of interface in C-fiber-reinforced laminated C-SiC matrix composites[J].Carbon,2000,38(6):831-838.
  • 7Srivastava V K,Maile K,Udoh A.Effect of damage on flexural modulus of C/C-SiC composites[J].Mat Sci Eng,2003,A354(1/2):292-297.
  • 8Lee Jae-Seol,Imai M,Yano T.Fabrication and mechanical properties of oriented SiC short-fiber-reinforced SiC composite by tape casting[J].Mat Sci Eng,2003,A339(1/2):90-95.
  • 9Willam B Hillig.Making ceramic composites by melt infiltration[J].American Ceramic Society Bulletin,1994,73(4):56-62.
  • 10Rice R W.Materials design and processing of high temperature ceramic matrix composites[J].Ceram Eng Sci Proc,1981,2(7/8):493-499.

二级参考文献73

共引文献192

同被引文献234

引证文献14

二级引证文献74

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