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Experimental and Numerical Investigations on Machining Induced Surface Integrity in Inconel-100 Nickel-Base Alloy

机译:Inconel-100镍基合金加工诱导表面完整性的实验性和数值研究

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Nickel-base alloys such as Inconel-100(IN-100) are still the most preferred material for jet engine and gas turbine components.Machining induced surface integrity plays a vital role for component fatigue life and reliability.This studyinvestigates the effects of machining conditions (tool geometry, coating, and cutting parameters) on the resultant residual stress, microhardness and grain size inmachiningIN-100. Experimental results for measured forces, residual stress, microhardness, and grain size have been presented. In addition, finite element modeling based investigations have been performed to predict not only residual stresses but also microstructureincluding dynamic recrystallization by implementing the Johnson-Mehl-Avrami-Kolmogorov model. Numerical modeling results were compared with experimental measurements in residual stresses, grain size and microhardness. The effects of cutting conditions on machining induced residual stress, microhardness, and average grain size have been reported.
机译:镍基合金如Inconel-100(IN-100)仍然是喷气发动机和燃气轮机组件的最优选的材料。加工诱导的表面完整性对组件疲劳寿命和可靠性起着至关重要的作用。本研究了加工条件的影响(刀具几何,涂层和切割参数)在所得残余应力,微硬度和晶粒尺寸内inmachinginin-100。已经提出了测量力,残余应力,显微硬度和晶粒尺寸的实验结果。此外,已经进行了有限元建模的研究,以预测残留应力,而且通过实施Johnson-Mehl-Avrami-Kolmogorov模型来预测残留应力,还可以预测剩余的压力,而且是微观的重结晶。将数值建模结果与残余应力,晶粒尺寸和微硬度进行了比较。已经报道了切割条件对加工诱导的残余应力,微硬度和平均晶粒尺寸的影响。

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