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材料初始缺陷对平纹编织C/SiC复合材料热残余应力的影响研究
引用本文:白国栋,童小燕,姚磊江.材料初始缺陷对平纹编织C/SiC复合材料热残余应力的影响研究[J].航空工程进展,2020,11(3):332-337.
作者姓名:白国栋  童小燕  姚磊江
作者单位:西北工业大学 航空学院,西安 710072;西北工业大学 无人机特种技术重点实验室,西安 710072,西北工业大学 无人机特种技术重点实验室,西安 710072,西北工业大学 无人机特种技术重点实验室,西安 710072
基金项目:国家重点研发计划(2016YFB0700503);国家自然科学基金(51772244,11072195)
摘    要:C/SiC热残余应力影响材料服役性能,而初始缺陷影响热残余应力,因此有必要对平纹编织C/SiC复 合材料的初始缺陷与热残余应力的关系进行研究。通过试样截面扫描电镜(SEM)图像对材料各类初始缺陷的分布特征进行测量和统计,建立含初始缺陷的宏观材料的代表体积单元(RVE)和纤维束 RVE有限元模型;采用 稳态变温法及有限元细观计算力学(FECM)方法预测含初始缺陷的纤维束 RVE有效性能参数及热残余应力。结 果表明:应力预测值与试验值吻合较好,得到了各类初始缺陷与宏观材料热残余应力之间的定量映射关系。

关 键 词:C/SiC  稳态变温法  初始缺陷  热残余应力  RVE模型
收稿时间:2019/10/10 0:00:00
修稿时间:2019/10/28 0:00:00

Influence of Initial Defects on Thermal Residual Stress of Plain Weave C/SiC Composites
baiguodong,tongxiaoyan and yaoleijiang.Influence of Initial Defects on Thermal Residual Stress of Plain Weave C/SiC Composites[J].Advances in Aeronautical Science and Engineering,2020,11(3):332-337.
Authors:baiguodong  tongxiaoyan and yaoleijiang
Institution:Northwestern Polytechnical University,Northwestern Polytechnical University,Northwestern Polytechnical University
Abstract:The thermal residual stress of C/SiC affects the service performance of the material. In order to explore the influence of initial defects on the thermal residual stress, the steady change temperature method and the finite element computational mechanics (FECM) method are used to determine the relationship with thermal residual stress and initial defects of plain weave C/SiC composites. The distribution characteristics of various initial defects of the material were measured and statistically analyzed by scanning electron microscopy (SEM) of the sample. The representative volume unit (RVE) and the fiber bundle RVE finite element model of the macroscopic material with initial defects were established to predict effective performance parameters and thermal residual stress of fiber bundle RVE, and obtain the quantitative relationship between various initial defects and thermal residual stress of macroscopic materials.
Keywords:C/SiC Composites  Steady variable temperature method  Initial Defects  Thermal Residual Stress  RVE model
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