巢青1,孙剑芬2,孙志刚2,宋迎东2.金属基复合材料力学性能研究进展[J].航空发动机,2018,44(4):91-98
金属基复合材料力学性能研究进展
Research Progress in Mechanical Properties of Metal Matrix Composites
  
DOI:
中文关键词:  金属基复合材料  静态拉伸  疲劳性能  界面  力学性能  航空发动机
英文关键词:Metal Matrix Composites  static tensile  fatigue property  interface  mechanical properties  aeroengine
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作者单位E-mail
巢青1,孙剑芬2,孙志刚2,宋迎东2 1. 中航机电系统有限公司北京1000282. 南京航空航天大学能源与动力学院南京210016 chaoq@avic.com 
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中文摘要:
      为了探明金属基复合材料的发展方向,并为其进一步研究提供理论依据,介绍了金属基复合材料静态拉伸及疲劳力学 性能的研究现状,研究了其界面模型的发展情况。结果表明:金属基复合材料轴向拉伸载荷作用下的宏- 细观统一本构模型发展 已相当成熟,并已得到试验验证,但其在偏轴拉伸载荷和疲劳载荷作用下的本构模型仍需深入研究和验证。对金属基复合材料界面 性能的研究已取得一定成果,但并未获得较准确的界面参数。
英文摘要:
      In order to find out the development direction of Metal Matrix Composites and provide theoretical basis for further research, the research status of static tensile and fatigue mechanical properties of Metal Matrix Composites were introduced,and the development of interface model of Metal Matrix Composites was studied. The results show that the macro-micro unified constitutive model of Metal Matrix Composites under axial tensile loading has been well developed and verified by experiments. However,its constitutive model under eccentric tensile and fatigue loads still needs to be further studied and verified. Some achievements had been made in the study of interfacial properties of Metal Matrix Composites,but no accurate interface parameters have been obtained.
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