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C/SiC编织型复合材料热/力学性能的多尺度预测

张永正 刘磊 刘琦 徐光魁

张永正, 刘磊, 刘琦, 徐光魁. C/SiC编织型复合材料热/力学性能的多尺度预测[J]. 应用数学和力学, 2023, 44(10): 1157-1171. doi: 10.21656/1000-0887.440056
引用本文: 张永正, 刘磊, 刘琦, 徐光魁. C/SiC编织型复合材料热/力学性能的多尺度预测[J]. 应用数学和力学, 2023, 44(10): 1157-1171. doi: 10.21656/1000-0887.440056
ZHANG Yongzheng, LIU Lei, LIU Qi, XU Guangkui. Multi-Scale Prediction of Thermal and Mechanical Properties of C/SiC Braided Composites[J]. Applied Mathematics and Mechanics, 2023, 44(10): 1157-1171. doi: 10.21656/1000-0887.440056
Citation: ZHANG Yongzheng, LIU Lei, LIU Qi, XU Guangkui. Multi-Scale Prediction of Thermal and Mechanical Properties of C/SiC Braided Composites[J]. Applied Mathematics and Mechanics, 2023, 44(10): 1157-1171. doi: 10.21656/1000-0887.440056

C/SiC编织型复合材料热/力学性能的多尺度预测

doi: 10.21656/1000-0887.440056
(我刊编委刘少宝推荐)
基金项目: 

国家自然科学基金项目 11972359

详细信息
    作者简介:

    张永正(1996—),男,硕士生(E-mail: 1303584072@qq.com)

    刘琦(1989—),男,博士(E-mail: liuqi202@hrbeu.edu.cn)

    徐光魁(1986—),男,教授(E-mail: guangkuixu@mail.xjtu.edu.cn)

    通讯作者:

    刘磊(1982—),男,副研究员(通讯作者. E-mail: l.liu@cardc.cn)

  • 中图分类号: O34

Multi-Scale Prediction of Thermal and Mechanical Properties of C/SiC Braided Composites

(Recommended by LIU Shaobao, M. AMM Editorial Board)
  • 摘要: C/SiC复合材料以其优异的力学和热学性能,在航空航天、国防和化学工业等领域都得到了广泛的应用. 精准获得C/SiC复合材料的热/力学性能,对该类材料在相关领域的高效应用至关重要. 基于代表性体积单元(RVE)和周期性边界条件,考虑纤维束的体积分数、交织方式、编织维度等非均匀、多尺度特征,建立了C/SiC复合材料的微/细观单胞模型. 使用有限元软件ABAQUS在微观尺度预测了纤维束的热/力学性能,将纤维束性能引入细观模型中,分析获得了该复合材料的宏观热/力学性能. 基于此多尺度关联分析方法,在27~1 227 ℃的工作温度范围内,进一步研究了纤维束和C/SiC复合材料的热导率和热膨胀系数随温度的变化规律. 该研究对C/SiC复合材料在工程上的应用具有一定的指导意义.
    1)  (我刊编委刘少宝推荐)
  • 图  1  三维C/SiC复合材料的多尺度有限元模型

    Figure  1.  The multi-scale finite element model for 3D C/SiC composites

    图  2  细观尺度RVE的网格

    Figure  2.  Meshes of the mesoscale RVE

    图  3  周期性边界条件

    Figure  3.  Periodic boundary conditions

    图  4  计算径向热导率时的边界条件

    Figure  4.  Boundary conditions for calculating radial thermal conductivity

    图  5  计算轴向热导率时的边界条件

    Figure  5.  Boundary conditions for calculating axial thermal conductivity

    图  6  3D正交互锁编织型复合材料(单位: mm)

    Figure  6.  The 3D positive interlocking braided composite(unit: mm)

    图  7  3D正交互锁编织型复合材料单胞的网格模型

    Figure  7.  The mesh model for 3D positive interlocking braided composite cells

    图  8  弹性模量E11和Poisson比μ12的数值和实验结果的比较

    Figure  8.  Comparison of the values of Young's modulus E11 and Poisson's ratio μ12 with the experimental results

    图  9  细观尺度下5种单胞模型

    Figure  9.  5 mesoscale single-cell models

    图  10  2D 1×1编织结构热/力学系数随纤维束体积分数的变化

    Figure  10.  Variations of thermal/mechanical coefficients of 2D 1×1 braided structure with the fiber bundle volume fraction

    图  11  5种编织结构的热导率

    Figure  11.  Thermal conductivities of 5 braided structures

    图  12  5种编织结构的热膨胀系数

    Figure  12.  Thermal expansion coefficient of 5 braided structures

    表  1  单位应变边界条件

    Table  1.   Unit strain boundary conditions

    condition εx εy εz γxy γxz γyz
    1 1 0 0 0 0 0
    2 0 1 0 0 0 0
    3 0 0 1 0 0 0
    4 0 0 0 1 0 0
    5 0 0 0 0 1 0
    6 0 0 0 0 0 1
    下载: 导出CSV

    表  2  碳纤维和环氧树脂的属性

    Table  2.   Properties of the carbon fiber and the epoxy resin

    property EP828 T-900
    E1/GPa 3.40 294
    E2/GPa 3.40 6.50
    G12/GPa 1.26 18.2
    G23/GPa 1.26 6.50
    μ12 0.35 0.32
    μ23 0.35 0.41
    α11/℃-1 6.45×10-5 -5.6×10-7
    α22/℃-1 6.45×10-5 5.6×10-6
    α33/℃-1 6.45×10-5 5.6×10-6
    下载: 导出CSV

    表  3  纱线热/力学性能的预测结果

    Table  3.   Predicted results of thermal/mechanical properties of yarns

    property value (Vf=50%)
    our method AEH method[21]
    E1/GPa 4.96 4.96
    E2/GPa 4.96 4.96
    E3/GPa 148.63 148.70
    G12/GPa 2.44 2.45
    G13/GPa 3.20 3.21
    G23/GPa 3.20 3.21
    μ12 0.475 0.476
    μ13 0.336 0.335
    μ23 0.011 0.011
    α11/℃-1 4.5×10-5 4.5×10-5
    α22/℃-1 4.5×10-5 4.5×10-5
    α33/℃-1 2.0×10-7 2.0×10-7
    下载: 导出CSV

    表  4  三维正交编织复合材料热/力学性能的预测结果

    Table  4.   Prediction results of thermal/mechanical properties of 3D orthogonal braided composite

    property our method FEM method[16]
    E1/GPa 34.10 32.97
    E2/GPa 52.01 51.21
    E3/GPa 11.85 11.13
    G12/GPa 2.94 2.88
    G13/GPa 2.51 2.43
    G23/GPa 2.53 2.45
    μ12 0.062 0 0.061 7
    μ13 0.486 0 0.497 0
    μ23 0.441 0 0.456 0
    α11/℃-1 1.310×10-5 12.920×10-5
    α22/℃-1 6.930×10-6 6.890×10-6
    α33/℃-1 8.110×10-6 7.940×10-6
    下载: 导出CSV

    表  5  纤维束的弹性常数

    Table  5.   Elastic constants of fiber bundles

    E1/GPa E2/GPa E3/GPa G12/GPa G13/GPa G23/GPa μ12 μ13 μ23
    308.24 76.59 76.59 43.02 43.02 25.44 0.28 0.28 0.41
    下载: 导出CSV

    表  6  纤维束的热膨胀系数和热导率

    Table  6.   Thermal expansion coefficients and thermal conductivities of the fiber bundle

    T/℃ α11/℃-1 (α22=α33)/℃-1 k11/(W·m-1·℃-1) (k22=k33)/(W·m-1·℃-1)
    27 3.80×10-5 4.48×10-6 147.17 83.84
    227 1.00×10-6 4.90×10-6 142.91 79.66
    427 1.72×10-6 5.65×10-6 138.32 72.07
    627 2.06×10-6 5.92×10-6 133.77 64.85
    827 2.36×10-6 6.18×10-6 131.13 60.21
    1 027 2.64×10-6 6.42×10-6 125.42 54.52
    1 227 2.90×10-6 6.69×10-6 118.61 45.06
    下载: 导出CSV

    表  7  5种编织结构的弹性常数

    Table  7.   Elastic constants of 5 braided structures

    braided structure E1/GPa E2/GPa E3/GPa G12/GPa G13/GPa G23/GPa
    1×1 2D 299.22 299.22 161.23 92.50 56.40 56.40
    2×1 2D 299.94 299.94 161.80 92.71 56.49 56.49
    2×2 2D 298.23 298.23 160.18 91.77 56.15 56.15
    2.5D coss-linking 280.73 300.09 169.10 91.70 57.37 63.16
    3D orthogonal 289.49 322.89 175.19 96.76 56.60 66.04
    下载: 导出CSV
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  • 收稿日期:  2023-03-06
  • 修回日期:  2023-07-14
  • 刊出日期:  2023-10-31

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