期刊文献+

C/SiC复合材料氧化残余强度计算模型 被引量:4

CALCULATION MODEL FOR RESIDUAL STRENGTH OF C/SiC COMPOSITES AFTER OXIDATION
在线阅读 下载PDF
导出
摘要 纤维氧化会使C/SiC复合材料的强度大幅度降低,原因是纤维中出现了缺口,不仅仅产生应力集中,而且纤维强度大大降低,纤维很容易发生断裂。文中基于这一损伤机理,建立细观力学分析模型,运用统计强度理论,对C/SiC复合材料无应力氧化残余强度进行模拟计算。模型引入纤维的氧化缺口,并考虑纤维特征强度的降低,获得与氧化试验值比较一致的模拟结果,表明模型的合理性。 The oxidation of fibers may cause significant strength decline in C/SiC composites as a result of the notches produced in the oxidizing process,which not only induce stress concentration but also result in fiber strength degradation.Both the above reasons will enhance the fiber failure probability within the notch length.Based on this damage mechanism and the statistic theory,a micromechanics based model is established for oxidation residual strength calculation.The fiber notch is introduced and the fiber characteristic strength degradation is considered.However,the effect of stress concentration is neglected.The values obtained from the model are in excellent agreement with the data derived from the non-stress oxidation experiments.This indicates the reliability of the analytical model.
出处 《机械强度》 CAS CSCD 北大核心 2011年第1期106-110,共5页 Journal of Mechanical Strength
基金 国家自然科学基金资助项目(90405015)~~
关键词 C/SIC复合材料 氧化 特征强度 细观力学 残余强度 C/SiC composites Oxidation Characteristic strength Micromechanics Residual strength
  • 相关文献

参考文献9

  • 1Pailler F, Iamon J. Micromechanics based model of fatigue-oxidation for ceramic matrix composites [J].Composites Science and Technology, 2005, 65 : 369-374.
  • 2Casas L, Martinez-Esnaola J M. Modeling the effect of oxidation on the creep behavior of fiber-rei~fforced ceramic matrix composites[J]. Acta. Materialia, 2003, 51 : 3745-3757.
  • 3Mei H, Cheng L F, Zhang L T, et al. Modeling the effects of thermal and mechanical load cycling on a C/SiC composite in oxygen/argon mixtures[J]. Carbon, 2007, 45: 2195-2204.
  • 4Lara-Curzio E. Analysis of oxidation-assisted stress-rupture of continuous fiber-reinforced ceramic matrix composites at intermediate temperatures[J]. Composites, 1999, 30: 549-554.
  • 5Curtin W A, Ahn B K, Takeda N. Modeling brittle and tough stress strain behavior in unidirectional ceramic matrix composites[J]. Acta mater, 1998, 46(10): 3409-3420.
  • 6De Morais A B. Prediction of the longitudinal tensile strength of polymer matrix composites[J]. Composites Science and Technology, 2006, 66: 2990-2996.
  • 7尹洪峰,徐永东,成来飞,张立同.界面相对碳纤维增韧碳化硅复合材料性能的影响[J].硅酸盐学报,2000,28(1):1-5. 被引量:25
  • 8Lamouroux F, Naslain R, Jouin J M. Kinetics and mechanisms of oxidation of 2D woven C/SiC composites:II[J]. Theoretical Approach. J. Am. Ceram. Soc., 1994, 77(8): 2058-68.
  • 9张钧,徐永东,张立同,成来飞,董宁.3D C/SiC复合材料基体裂纹间距分布规律[J].航空材料学报,2003,23(3):11-14. 被引量:13

二级参考文献9

  • 1徐永东,张立同,成来飞,朱文超.CVI法制备三维碳纤维增韧碳化硅复合材料[J].硅酸盐学报,1996,24(5):485-490. 被引量:41
  • 2唐纳特 J B 等著 碳纤维.李仍元等译[M].北京:科学出版社,1989.11.
  • 3唐纳特 J B 等著 李仍元等译.碳纤维[M].北京:科学出版社,1989.11.
  • 4JAMET JF, LAMICQ. Comoosite thermostructures: an overview of French experience[A].Naslain R.High temperature ceramic matrix composites[M]. Bordeaux: Woodhead, 1993.
  • 5Cheng L F,Xu Y D, Zhang LT,et al. Oxidation behavior of three dimensional C/SiC composites in air and combustion gas environments[J]. Carbon,2000,38(15) : 2103--2108.
  • 6Xu YD, Zhang LT, Cheng LF. Three-Dimensional Carbon/Silicon Carbide Composites Prepared by Chemical Vapor Infiltration[J]. J Am ceram. Soc. ,1997,80(7) : 1897-- 1900.
  • 7Lackey WJ, Hanigofsky JA, Freeman GB, et al.Continuous fabrication of silicon carbide fiber tows by chemical vapor deposition[J].J Am Ceram.Soc., 1995,78(6) :1564--1570.
  • 8Cao H C,J Am Ceram Soc,1990年,73卷,6期,1691页
  • 9尹洪峰,徐永东,成来飞,张立同.界面相对碳纤维增韧碳化硅复合材料性能的影响[J].硅酸盐学报,2000,28(1):1-5. 被引量:25

共引文献36

同被引文献40

引证文献4

二级引证文献11

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