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    基于数字图像相关技术的缺口件疲劳寿命预测

    Fatigue Life Prediction of Notched Pant by Digital Image Correlation Technique

    • 摘要: 利用数字图像相关技术获取不同载荷水平下疲劳试验时U型(缺口半径0.2,1.0 mm)和V型(缺口角度45°,90°)缺口根部应变的演变,研究了载荷幅(0.5,0.7,1.0 kN)和载荷比(0,0.3,0.5)对缺口根部棘轮应变及应变幅演变的影响;基于缺口根部稳态棘轮应变速率演变和应力集中系数,分别建立考虑缺口名义应力幅和载荷比影响的缺口件疲劳寿命预测模型,并进行了预测精度分析。结果表明:随着载荷幅增加,缺口根部的棘轮应变和应变幅增大;随着载荷比增加,缺口根部的棘轮应变增大,应变幅变化不大。考虑名义应力幅和载荷比影响的疲劳寿命预测模型预测值多数分布在1.5倍误差带,最大不超过1.75倍误差带,模型准确;考虑载荷比影响时疲劳寿命预测误差相比考虑载荷幅影响时高,模型对U型缺口试样的疲劳寿命预测误差相比对V型缺口试样高。

       

      Abstract: The evolution of strains at the root of U-shaped (with notch radius of 0.2 and 1.0 mm) and V-shaped (with notch angle of 45° and 90°) notches during fatigue under different loading levels were obtained by digital image correlation technique. The effects of the load amplitude (0.5, 0.7, 1.0 kN) and the load ratio (0, 0.3, 0.5) on the ratcheting strain and strain amplitude at the notch root were investigated. On the basis of the evolution of the steady state ratcheting strain rate at the notch root and stress concentration fraction, two fatigue life prediction models were established considering the nominal stress amplitude and the load ratio effects, respectively. The results show that with the increase of load amplitude, the ratcheting strain and strain amplitude at the root of notches increased. With the increase of load ratio, the ratcheting strain at the root of notches increased, while the strain amplitude changed little. The predicted values of the fatigue life by the prediction model considering the nominal stress amplitude and load ratio were mostly within a 1.5-fold error band, with the maximum not exceeding a 1.75-fold error band. The model was accurate. The fatigue life prediction error by the model considering the influence of load ratio was higher than that considering load amplitude influencing. The model's fatigue life prediction error for U-shaped notch sample was higher than that for V-shaped notch sample.

       

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