Online Deformation Measurement of Laser Repair Substrate Based on Orthogonal Sampling Moiré

Shi, Weiqing; Zhang, Chenghao; Xie, Huimin

doi:10.3390/app12115469

Cited by 4 publications

(1 citation statement)

References 25 publications

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“…Nickel-based alloys are commonly used superalloys which have been widely used in the manufacture of critical hot-section parts of aeroengines, such as blades [1,2]. However, under the condition of multi-physics coupling, the blades are very prone to fatigue-related damage or destruction [3].…”

Section: Introductionmentioning

confidence: 99%

A Novel Parameter for Fatigue Damage Assessment of Laser-Repaired Nickel-Based Alloy

et al. 2022

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The fatigue damage assessment of laser-repaired components is critical to their service safety. However, since laser repairing is an advanced green remanufacturing technology, the current research on its fatigue mechanical behavior and fatigue damage evaluation methods is still immature. In addition, the relevant models used for the fatigue damage evaluation can only indicate the fatigue limit of components, which cannot describe the damage accumulation process of the components during the fatigue testing. Therefore, there is an urgent need to develop a fatigue damage evaluation method that can describe the fatigue damage accumulation and evolution to reveal the damage evolution mechanism during the fatigue test. In this study, based on the 3D-DIC technique, new damage parameters, i.e., strain average value and strain standard deviation, are proposed to quantitatively describe the damage status of the nickel-based components during the stress-based fatigue process. Then, based on the new damage parameters, a strain average value/strain standard deviation damage curve method is proposed to describe the damage status evolution of the components during the fatigue testing and evaluate its fatigue damage. For example, in the tensile fatigue test, the strain average value/strain standard deviation damage curves of the substrate component and the laser-repaired component can be divided into two damage stages. In the first damage stage, the damage increases slowly with the increase in the cycle number, whereas in the second damage stage, the damage increases rapidly with the increase in the cycle number. At this time, there is a demarcation point between the first damage stage and second damage stage in the strain average value damage curve and strain standard deviation damage curve. The cycle number of the demarcation point can be used as a reference value for the fatigue failure of the laser-repaired component. In addition, the electron backscatter diffraction (EBSD) technique was used to verify the validity of the evaluation results from the novel damage parameters.

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Section: Introductionmentioning

confidence: 99%