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纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展

程小全 杜晓渊

程小全, 杜晓渊. 纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展[J]. 北京航空航天大学学报, 2021, 47(7): 1311-1322. doi: 10.13700/j.bh.1001-5965.2020.0229
引用本文: 程小全, 杜晓渊. 纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展[J]. 北京航空航天大学学报, 2021, 47(7): 1311-1322. doi: 10.13700/j.bh.1001-5965.2020.0229
CHENG Xiaoquan, DU Xiaoyuan. Research development of fatigue life prediction and damage analysis model of fiber-reinforced composite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(7): 1311-1322. doi: 10.13700/j.bh.1001-5965.2020.0229(in Chinese)
Citation: CHENG Xiaoquan, DU Xiaoyuan. Research development of fatigue life prediction and damage analysis model of fiber-reinforced composite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(7): 1311-1322. doi: 10.13700/j.bh.1001-5965.2020.0229(in Chinese)

纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展

doi: 10.13700/j.bh.1001-5965.2020.0229
详细信息
    通讯作者:

    程小全. E-mail: xiaoquan_cheng@buaa.edu.cn

  • 中图分类号: TB332

Research development of fatigue life prediction and damage analysis model of fiber-reinforced composite

More Information
  • 摘要:

    随着纤维增强复合材料主承力结构在多领域内的广泛应用,疲劳成为复合材料结构设计必须面对的问题,出现了大量用于复合材料结构疲劳寿命预测及损伤演化的分析模型与方法。目前的复合材料疲劳性能分析模型可以分为疲劳寿命模型、唯象模型和渐进损伤模型。对这3类模型的发展情况进行了综述和对比分析。其中,疲劳寿命模型原理相对简单,适用于工程结构的寿命估算;唯象模型建立了材料剩余强度/刚度与循环数的数学关系,可以预测结构的寿命与材料剩余力学性能;渐进损伤模型不仅可以预测结构寿命和材料剩余力学性能,还能分析结构疲劳损伤机理。对各类疲劳性能分析模型的发展趋势进行了讨论。指出了降低实施成本和提高通用型是各类疲劳性能分析模型有待解决的问题。

     

  • 图 1  典型等寿命曲线[6]

    Figure 1.  Typical constant fatigue life curve[6]

    图 2  不同CLD模型[15]

    Figure 2.  Different CLD models[15]

    图 3  最大循环应力σmax下剩余强度边界变化示意图[31]

    Figure 3.  Schematic of residual strength boundaries at maximum cyclic stress σmax[31]

    图 4  疲劳载荷下的刚度[46]

    Figure 4.  Definition of stiffness under fatigue load[46]

    图 5  复合材料疲劳过程中典型的正规化模量下降曲线与特征损伤状态[58]

    Figure 5.  Typical normalized modulus degradation curve and characteristic damage state during the fatigue life of composite laminate[58]

    图 6  Shokrieh渐进损伤模型运行流程

    Figure 6.  Operation flowchart of Shrokrieh's progressivedamage model

    图 7  面心阵列分布的复合材料细观单胞模型[80]

    Figure 7.  Mesoscopic unit cell model with face-centered array distribution of composite[80]

    图 8  cohesive单元Ⅰ型、Ⅱ型和混合型裂纹加载对应的应力位移曲线

    Figure 8.  Stress displacement curves for cohesive elements under Ⅰ, Ⅱ and hybrid crack loading modes

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  • 收稿日期:  2020-06-01
  • 录用日期:  2020-08-30
  • 网络出版日期:  2021-07-20

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