纤维增强复合材料考虑损伤的温度胀缩细观力学模型

Micro-mechanical model of thermal expansion/contraction for damaged fiber reinforced composites

  • 摘要: 采用细观力学方法,建立了纤维增强复合材料(FRC)包含基体微裂纹和纤维/基体脱粘的热胀/冷缩理论模型。模型考虑了基体、界面中不同分布取向的微裂纹在升温和降温过程中张开、闭合情况的差异,及其对复合材料平均热胀/冷缩系数(CTE/CTC)的影响,同时还考虑了细观应力分布不均匀的因素。建立了细观有限元模型对理论模型进行验证。研究发现:复合材料损伤后CTE和CTC不一致,且取决于损伤模式:基体微裂纹损伤使得复合材料的横向CTE高于无损材料,而横向CTC低于无损材料,但对纵向CTE/CTC影响不大;纤维界面脱粘能较明显地减小复合材料的纵向CTC,但对横向CTC的影响可忽略。

     

    Abstract: Considering damages of matrix micro-cracks and fiber/matrix debonding, the thermal expansion/contraction theoretical model of fiber reinforced composite (FRC) was developed by using micro-mechanical method. In the model, differences of opening and closing conditions of micro-cracks in different orientations, both in matrix and fiber/matrix interface corresponding to heating and cooling and their effects on average coefficient of thermal expansion/contraction (CTE/CTC) were explored. The model has also taken the ununiformity of stresses in micro-scale into account. Micro finite element model was built to validate the theoretical model. The results reveal that CTE and CTC of damaged FRC are not identical and their discrepancy depends on damage modes. The matrix micro-crack damage could promote transverse CTE of FRC higher than nondestructive material's and decrease transverse CTC lower than nondestructive material's, however it has little effect on longitudinal CTE/CTC. Fiber/matrix interface debonding could bring notable reduction of longitudinal CTC, but be ignorable to transverse CTC.

     

/

返回文章
返回