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2D-C_f/SiC复合材料蠕变断裂及损伤机理研究
引用本文:张程煜,李丽华,张晓,董宁,李玫,韩栋.2D-C_f/SiC复合材料蠕变断裂及损伤机理研究[J].航空制造技术,2017(22).
作者姓名:张程煜  李丽华  张晓  董宁  李玫  韩栋
作者单位:西北工业大学超高温结构复合材料国家级重点实验室,西安,710072
基金项目:国家自然科学基金,超高温结构复合材料重点实验室创新基金,陕西省科学技术研究发展计划项目,高等学校学科创新引智计划资助项目
摘    要:研究了2D-C_f/Si C复合材料在空气中,温度分别为700℃和900℃,蠕变应力分别为50MPa、75MPa和100MPa条件下的蠕变断裂及损伤机理。运用拉森-米勒参数法拟合材料的蠕变断裂时间,使用扫描电子显微镜分析其微观组织和断口形貌以进一步揭示其蠕变断裂机理。结果表明:2D-C_f/Si C复合材料的蠕变断裂寿命与温度和应力密切相关,较高温度或应力会降低材料的蠕变断裂寿命;在蠕变过程中,材料除发生应力损伤外,还会发生氧化损伤;2D-C_f/Si C复合材料的氧化损伤比应力损伤对蠕变断裂时间有更显著的影响。

关 键 词:2D-Cf/SiC  蠕变断裂时间  蠕变损伤

Creep Rupture and Creep Damage Mechanisms of a 2D-Cf/SiC Composite
ZHANG Chengyu,LI Lihua,ZHANG Xiao,DONG Ning,LI Mei,HAN Dong.Creep Rupture and Creep Damage Mechanisms of a 2D-Cf/SiC Composite[J].Aeronautical Manufacturing Technology,2017(22).
Authors:ZHANG Chengyu  LI Lihua  ZHANG Xiao  DONG Ning  LI Mei  HAN Dong
Abstract:The tensile creep rupture and creep damage mechanism of 2D-Cf/SiC composite were investigated in present work in air. The applied temperatures are 700℃ and 900℃ , and the stresses are 50MPa, 75MPa and 100MPa, re-spectively. The creep rupture time of the material was fitted by Larson-Miller equation. The microstructures and fracture morphology were analyzed by a scanning electron microscopy. The results show that the rupture time of the 2D-Cf/SiC composite was influenced by the applied stress and temperature. Higher stress or temperature causes the shorter creep rup-ture time. During the creep, the oxidation plays critical role in determining the creep rupture time. The creep damage of 2D-Cf/SiC resulted from stress and the oxidation. Compared with the former, the damage caused by the latter made a more significant effect on the creep rupture time of the composites.
Keywords:2D-Cf/SiC  Creep rupture time  Creep damage
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