主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
考虑内部损伤随机性的SiCf/SiC复合材料力学性能概率分析
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南京航空航天大学航空学院

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V232. 4

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国家科技重大专项


Probabilistic Analysis of Mechanical Properties of SiCf/SiC Composites Considering Internal Damage Randomness
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College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautic

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    摘要:

    陶瓷基复合材料(CMCs)在使用过程中会产生纤维拔出、基体裂纹等内部损伤,进而对编织CMCs 的力学性能造成影响。面向2.5 维SiCf/SiC 编织CMCs,分别建立纤维束的微观有限元模型和编织CMCs 的细观有限元模型;考虑内部损伤数量及位置的随机性,建立细观模型的力学性能参数的概率分布,研究损伤率对材料强度及杨氏模量的影响规律;通过参数方法和非参数方法同时拟合考虑内部损伤随机性的CMCs 力学性能参数的概率分布。结果表明:随着损伤率的增加,编织CMCs 强度的下降速率快于刚度;非参数方法获得的经向强度和杨氏模量概率密度函数曲线与样本直方图吻合较好。

    Abstract:

    Ceramic matrix composites(CMCs) will experience internal damage such as fiber pulling out and matrix cracks during usage, which will affect the mechanical properties of braided CMCs. For SiCf/SiC 2.5-dimensional braided CMCs, a microscopic finite element model of fiber bundle and a meso finite element model of braided CMCs were established, respectively. Considering the randomness of internal damage quantity and location, the probability distributions of mechanical parameters of the meso-scopic level model was identified, and the influence of damage rate on the strength limit and Young"s modulus of the material was studied. Both parametric and non-parametric methods were used to fit the probability distribution of mechanical properties of CMCs. The results show that, with the increase of damage rate, the strength limits decrease faster than the stiffness. In addition, the probability density function curve of strength limit and Young"s modulus obtained by non-parametric method match the frequency histogram of the sample well.

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历史
  • 收稿日期:2024-02-01
  • 最后修改日期:2024-05-22
  • 录用日期:2024-05-31
  • 在线发布日期: 2025-03-13
  • 出版日期: