A new method for estimating fatigue life of notched specimen
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A new method for estimating fatigue life of notched specimen

机译:一种估算缺口标本疲劳寿命的新方法

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Highlights?A new method for fatigue life prediction of notch components is proposed.?The stress distributions of notch root are analyzed by finite element method.?The fatigue life of notch specimen is estimated by the proposed method.AbstractFatigue life of engineering structure contains two parts: crack initiation life and crack propagation life. Fracture mechanics is adopted to estimate crack propagation life in the real engineering structures and has made some achievements. Actually, the existing study indicated that fatigue crack initiation is also an important period in the whole fatigue life. So, a new method to predict the whole fatigue life of notch components is proposed based on the theory of damage mechanics in this paper. The damage evolution equation of notch specimen under tension compression loading is obtained based on closed-form solution. The stress distributions of notch root are analyzed by finite element method. The whole fatigue life of notch specimen is estimated by the proposed method when
机译:<![cdata [ 亮点 提出了一种新方法,用于陷波组件的疲劳寿命预测。 缺口根的应力分布通过有限元方法进行分析。 陷波样本的疲劳寿命由所提出的方法估算。 抽象 工程结构的疲劳寿命包含两部分:裂缝启动寿命和裂缝繁殖寿命。采用骨折力学来估算实际工程结构中的裂缝繁殖寿命,并取得了一些成就。实际上,现有的研究表明,疲劳裂纹引发也是整个疲劳寿命的重要时期。因此,基于本文损坏力学理论,提出了一种预测陷波部件的整个疲劳寿命的新方法。基于闭合溶液获得张力压缩负荷下凹口样品的损伤演化方程。通过有限元法分析槽根根的应力分布。凹口标本的整个疲劳寿命估计是所提出的方法

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