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Prediction of residual fatigue life using nonlinear ultrasound

机译:非线性超声预测残余疲劳寿命

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Prediction of fatigue life of components during service is an on-going and unsolved challenge for the NDT and structural health monitoring community. It has been demonstrated by a number of researchers that nonlinear guided waves or the acoustic nonlinear signature of fatigued cracked material provides clear signs of the progressive fatigue damage in the material, unlike linear guided waves. However, even with nonlinear acoustic-ultrasound methods there is a necessity to compare the current nonlinear feature to a previously measured cracked material state to assess the absolute residual fatigue life. In this paper, a new procedure based on the measurement of the second-order acoustic nonlinearity is presented which is able to assess the fatigue life of a metallic component without the need of a baseline. The NazarovSutin crack nonlinearity equation and the Paris law are combined in order to obtain an analytical solution able to evaluate the theoretical second-order quadratic nonlinear parameters as a function of the crack growth and fatigue life that evolve during cyclic loading in metals. The model makes the assumption that the crack surface topology has variable geometrical parameters. The method was tested on aluminum alloy specimens AA2024-T351, containing fatigue fracture of different sizes, and excellent correlation was obtained between the theoretical and measured second-order nonlinear parameter. Then, it was demonstrated clearly that by measuring the nonlinear parameters it is possible to estimate crack size and fatigue life. Finally, advantages and limitations of the procedure are discussed.
机译:对无损检测和结构健康监测界来说,预测组件在服务期间的疲劳寿命是一项持续而未解决的挑战。许多研究人员已经证明,与线性导波不同,非线性裂纹或疲劳裂纹材料的声学非线性特征为材料中的渐进性疲劳破坏提供了清晰的信号。但是,即使使用非线性声学-超声波方法,也有必要将当前的非线性特征与先前测量的破裂材料状态进行比较,以评估绝对残余疲劳寿命。在本文中,提出了一种基于二阶声学非线性测量的新程序,该程序无需基线即可评估金属部件的疲劳寿命。将NazarovSutin裂纹非线性方程和Paris法则结合起来,以获得能够评估理论上的二次非线性参数的解析解决方案,该参数是金属循环载荷过程中裂纹扩展和疲劳寿命的函数。该模型假设裂纹表面拓扑具有可变的几何参数。该方法在铝合金试件AA2024-T351上进行了测试,该试件包含不同尺寸的疲劳断裂,并且在理论值和实测二阶非线性参数之间获得了极好的相关性。然后,清楚地表明,通过测量非线性参数,可以估算裂纹尺寸和疲劳寿命。最后,讨论了该程序的优点和局限性。

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