ECC单轴拉伸疲劳变形特性及寿命预测

Fatigue deformation characteristics and life prediction of ECC under uniaxial tension

  • 摘要: 工程水泥基复合材料(ECC)多用于结构的抗震补强,其疲劳性能是工程中关注的重点。利用疲劳试验机对ECC试件进行单轴拉伸循环加载试验,分析了动力变形、损伤模型和疲劳寿命的发展规律。结果表明:单向拉伸疲劳荷载下,ECC应力-应变曲线呈疏-密-疏特点;残余应变呈三阶段发展,采用六次多项式进行拟合描述,相关系数基本大于0.9;针对第二阶段定义应变率及应变增长率两个物理量,发现拉应力比越高,应变率越大,第二阶段循环比越短;应变增长率在0.0028~0.0098之间变化,其随着拉应力比的增加而减小。用疲劳变形模量定义损伤变量,建立以循环寿命比n/N=0.7为分界点的两阶段疲劳损伤演变方程。针对应力比S=0.85进行验证,评估疲劳损伤程度并预估剩余寿命,其与试验结果对比相关性较高。

     

    Abstract: Engineering cementitious composite (ECC) is widely used in structural seismic strengthening, and its fatigue performance is the focus of engineering. The uniaxial tensile cyclic loading test of ECC specimens was carried out by fatigue testing machine, and the development law of dynamic deformation, damage model and fatigue life was analyzed. The results show that under uniaxial tensile fatigue load, the stress-strain curve of ECC is sparse-dense-sparse. Residual strain develops in three stages and is described by six polynomial fitting. The correlation coefficient is basically greater than 0.9. Two physical quantities, strain rate and strain growth rate, are defined for the second stage. It is found that the higher the tensile stress ratio is, the larger the strain rate is and the shorter the cycle ratio is in the second stage. Strain growth rate varies from 0.0028 to 0.0098 and decreases with the increase of tensile stress ratio. The damage variable is defined by fatigue deformation modulus, and the two-stage fatigue damage evolution equation is established with the cycle life ratio n/N=0.7. The stress ratio S=0.85 was verified, and the fatigue damage degree of the specimen was evaluated and the remaining life was predicted, which was highly correlated with the test results.

     

/

返回文章
返回