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DEVELOPMENT OF A FATIGUE DAMAGE AND LIFING ASSESSMENT METHOD FOR INCONEL 625 AND ALUMINUM 6061-T6

机译:INCONEL 625和6061-T6铝的疲劳损伤和起重评估方法的开发

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An energy based fatigue damage and lifing assessment method is developed for a high temperature material, Inconel 625, and Aluminum 6061-T6. A newly developed experimental method is used for interrogating accumulated fatigue damage and evolution for low and high cycle fatigue (LCF/HCF) at continuum scales. The proposed fatigue lifing assessment method is based on assessing the total strain energy dissipated to cause fatigue failure of a material, known as the fatigue toughness. From the fatigue toughness and experimentally determined fatigue lives at two different stress amplitudes, the cyclic parameters of the Ramberg-Osgood constitutive equation that describes the hysteresis stress-strain loop of a cycle are determined. Stress controlled mechanical fatigue tests are performed to construct room temperature stress-life (S-N) curves and to determine damage progression based on accumulated fatigue damage. The predicted fatigue life obtained from the present energy based approach is found in good agreement with experimental data.
机译:针对高温材料Inconel 625和铝6061-T6,开发了一种基于能量的疲劳损伤和起伏评估方法。一种新开发的实验方法用于询问在连续尺度上累积的疲劳损伤和低周疲劳和高周疲劳(LCF / HCF)的演变。提出的疲劳寿命评估方法是基于评估耗散导致材料疲劳破坏的总应变能,即疲劳韧性。根据疲劳韧性和通过实验确定的疲劳寿命在两个不同的应力振幅下,可以确定描述一个循环的滞后应力-应变循环的Ramberg-Osgood本构方程的循环参数。进行应力控制的机械疲劳测试以构建室温应力-寿命(S-N)曲线,并基于累积的疲劳损伤确定损伤进展。发现从当前基于能量的方法获得的预期疲劳寿命与实验数据高度吻合。

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