蠕变-疲劳交互作用下试样几何约束对裂纹扩展行为的影响

Lei Zhao, Lianyong Xu
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引用次数: 0

摘要

蠕变-疲劳相互作用会加速裂纹扩展行为,改变裂纹扩展模式,这与单纯蠕变或疲劳状态下的裂纹扩展模式不同。此外,裂纹尖端前的约束会影响裂纹扩展速率与断裂力学之间的关系,从而影响含缺陷高温构件寿命预测的准确性。在本研究中,为了揭示不同试件几何形状对蠕变疲劳状态下约束的作用,采用了五种不同类型的裂纹试件(包括c环拉伸CST、致密拉伸CT、单缺口拉伸SENT、单缺口弯曲SENB、中拉伸MT)。基于考虑蠕变损伤、疲劳损伤和相互作用损伤的非线性蠕变-疲劳相互作用损伤模型,采用有限元方法模拟了裂纹扩展和损伤演化行为。给出了不同试样几何形状下(Ct)avg的表达式。然后分析了蠕变疲劳条件下不同试样几何形状下裂纹扩展行为的变化规律。CT和CST表现出最高的裂纹扩展速率,是MT中最低裂纹扩展速率的10倍。这表明试样几何形状的差异影响了裂纹尖端之前的面内约束水平。此外,引入了与载荷无关的约束参数Q*来关联裂纹扩展速率。在给定的(Ct)avg值下,裂纹扩展速率的变化顺序与Q*的减小顺序相同,在对数-对数曲线上表现为线性关系。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effect of Constraint Induced by Specimen Geometries on Crack Growth Behavior Under Creep-Fatigue Interaction
Creep-fatigue interaction would accelerate the crack growth behaviour and change the crack growth mode, which is different from that presenting in pure creep or fatigue regimes. In addition, the constraint ahead of crack tip affects the relationship between crack growth rate and fracture mechanics and thus affects the accuracy of the life prediction for high-temperature components containing defects. In this study, to reveal the role of constraint caused by various specimen geometries in the creep-fatigue regime, five different types of cracked specimens (including C-ring in tension CST, compact tension CT, single notch tension SENT, single notch bend SENB, middle tension MT) were employed. The crack growth and damage evolution behaviours were simulated using finite element method based on a non-linear creep-fatigue interaction damage model considering creep damage, fatigue damage and interaction damage. The expression of (Ct)avg for different specimen geometries were given. Then, the variation of crack growth behaviour with various specimen geometries under creep-fatigue conditions were analysed. CT and CST showed the highest crack growth rates, which were ten times as the lowest crack growth rates in MT. This revealed that distinctions in specimen geometry influenced the in-plane constraint level ahead of crack tip. Furthermore, a load-independent constraint parameter Q* was introduced to correlate the crack growth rate. The sequence of crack growth rate at a given value of (Ct)avg was same to the reduction of Q*, which shown a linear relation in log-log curve.
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