文章摘要
邓杨芳,范晓孟,张根,吴长波,钟燕,何爱杰,殷小玮.预氧化Cf/SiC陶瓷基复合材料及其构件的抗疲劳特性研究[J].材料导报,2018,32(4):631-635
预氧化Cf/SiC陶瓷基复合材料及其构件的抗疲劳特性研究
Anti-fatigue Performance Study of Pre-oxidized 2D-Cf/SiC Ceramic Matrix Composites
  
DOI:10.11896/j.issn.1005-023X.2018.04.025
中文关键词: 碳纤维 陶瓷基复合材料 振动疲劳 失效模式
英文关键词: carbon fiber, ceramic matrix composites, vibration fatigue, damage mode
基金项目:基金项目:国家自然科学基金(51372204)
作者单位E-mail
邓杨芳 中国航发四川燃气涡轮研究院,成都 610500 fang_nwpu@163.com 
范晓孟 西北工业大学超高温结构复合材料重点实验室,西安 710072  
张根 中国航发四川燃气涡轮研究院,成都 610500  
吴长波 中国航发四川燃气涡轮研究院,成都 610500  
钟燕 中国航发四川燃气涡轮研究院,成都 610500  
何爱杰 中国航发四川燃气涡轮研究院,成都 610500  
殷小玮 西北工业大学超高温结构复合材料重点实验室,西安 710072  
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中文摘要:
      采用在线销钉集成技术实现了二维Cf/SiC复杂构件的近尺寸成型,并考察预氧化Cf/SiC销钉集成构件的高周疲劳寿命及破坏模式。实验结果表明:Cf/SiC构件在不同激振加速度条件下均表现为由销钉断裂所引起的整体分层破坏,层板连接处为Cf/SiC构件的振动疲劳薄弱部位。通过ANSYS振动应力分析和微观组织分析可以推论出,疲劳试验时,裂纹容易沿着层板间的基体扩展,在基体开裂失效后,全部应力施加于销钉处,最终在疲劳应力作用下销钉发生断裂,导致构件整体分层破坏。
英文摘要:
      In this paper, the two-dimensional (2D) carbon fiber reinforced silicon carbide matrix composites (Cf/SiC) with complex shape were prepared by the online integration technique, and then the vibration fatigue test was carried out to investigate the vibration fatigue life and damage models after the pre-oxidation. The work demonstrated the delamination damage mode at different excitation acceleration, which was caused by the pin fracture, and the delamination joint is weak part of Cf/SiC. Through the analysis of ANSYS stress and microstructure, it can be concluded that, in the vibration test, cracks propagated easily in the interlayer matrix due to the lack of fiber toughening mechanism, and then the stress was concentrated on the pin with the failure of interlayer matrix. So the composites failed by the pin fracture and the interlayer delamination were damaged.
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