高级检索
    姜学艳, 包骐乐, 代巧. 非对称循环载荷下TA2工业纯钛疲劳损伤行为的预测[J]. 机械工程材料, 2024, 48(7): 70-76. DOI: 10.11973/jxgccl230309
    引用本文: 姜学艳, 包骐乐, 代巧. 非对称循环载荷下TA2工业纯钛疲劳损伤行为的预测[J]. 机械工程材料, 2024, 48(7): 70-76. DOI: 10.11973/jxgccl230309
    JIANG Xueyan, BAO Qile, DAI Qiao. Fatigue Damage Behavior Prediction of TA2 Commercial Pure Titanium under Asymmetric Cyclic Loading[J]. Materials and Mechanical Engineering, 2024, 48(7): 70-76. DOI: 10.11973/jxgccl230309
    Citation: JIANG Xueyan, BAO Qile, DAI Qiao. Fatigue Damage Behavior Prediction of TA2 Commercial Pure Titanium under Asymmetric Cyclic Loading[J]. Materials and Mechanical Engineering, 2024, 48(7): 70-76. DOI: 10.11973/jxgccl230309

    非对称循环载荷下TA2工业纯钛疲劳损伤行为的预测

    Fatigue Damage Behavior Prediction of TA2 Commercial Pure Titanium under Asymmetric Cyclic Loading

    • 摘要: 对TA2工业纯钛进行应力控制的非对称载荷疲劳试验,研究了不同最大应力(245,253,270,300 MPa)下纯钛的疲劳寿命和断口形貌,分析了非对称循环载荷下的应变演变以及应力-应变响应;基于连续损伤力学理论,建立了基于棘轮应变和总应变能密度的疲劳损伤演变预测模型,对纯钛的疲劳损伤过程进行预测,并与试验结果进行对比。结果表明:随着最大应力的降低,TA2工业纯钛的疲劳寿命延长。当最大应力为245,253 MPa时,塑性韧断区面积较小,断口中出现疲劳裂纹扩展区,失效机制为疲劳开裂及裂纹扩展失效,疲劳应变演变由加载初始阶段、稳定阶段和失效阶段组成,随最大应力的增加,塑性应变能密度以及相同疲劳寿命对应的平均应变均增大。当最大应力为270,300 MPa时,断口主要由纤维状的塑性韧断区组成,失效机制为循环塑性大变形失效,此时疲劳应变演化的稳定阶段不明显,随最大应力的增加,塑性应变能密度增大幅度较大,且当循环次数达到70%疲劳寿命时,270 MPa最大应力下的平均应变较大。基于棘轮应变的疲劳损伤演变预测模型对于疲劳中后期(循环次数不低于40%疲劳寿命)损伤值的预测效果较好,最大相对误差不超过12.5%;基于总应变能密度的疲劳损伤演变预测模型预测的损伤值相对误差基本在23%以内,整体预测稳定性较差。

       

      Abstract: The asymmetric cyclic load fatigue tests controlled by force of commercial pure titanium TA2 were carried out, and the fatigue life and fracture morphology of the pure titanium under different maximum stresses (245, 253,270,300 MPa) were studied, and the strain evolution and stress-strain response under asymmetric cyclic loads were analyzed. Based on the theory of continuous damage mechanics, the fatigue damage evolution prediction models based on ratchet strain and total strain energy density were established to predict the fatigue damage of the pure titanium, and the predicted results were compared with the test results. The results show that the fatigue life of the commercial pure titanium TA2 increased with the decrease of the maximum stress. When the maximum stress was 245, 253 MPa, the area of plastic ductile fault zone was small, fatigue crack growth zone appeared in the fracture, and the failure mechanism was fatigue crack and crack growth failure; the evolution of fatigue strain was composed of initial loading stage, stable stage and failure stage; with the increase of maximum stress, the plastic strain energy and the average strain corresponding to the same fatigue life increased. When the maximum stress was 270, 300 MPa, the fracture was mainly composed of fiber-like plastic ductile fracture zone, and the failure mechanism was cyclic plastic large deformation failure; the stability stage of fatigue strain evolution was not obvious; the plastic strain energy increased greatly with the increase of the maximum stress, and the average strain under the maximum stress of 270 MPa was larger when the cycle number reached 70% fatigue life. The fatigue damage evolution prediction model based on ratchet strain had a good prediction effect on damage values in the middle and late fatigue period (cycle number of no less than 40% fatigue life) with the maximum relative error no more than 12.5%. The relative error of damage value predicted by the fatigue damage evolution prediction model based on the total strain energy density was basically less than 23%, and the overall prediction stability was poor.

       

    /

    返回文章
    返回