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Effects of the γ″-Ni3Nb Phase on Fatigue Behavior of Nickel-Based 718 Superalloys with Different Heat Treatments

机译:γ″ -Ni3Nb相对不同热处理镍基718合金的疲劳行为的影响

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摘要

The effects of the γ″-Ni Nb phase on fatigue behavior of nickel-based 718 superalloys with standard heat treatment, hot isostatic pressing + solution treatment + aging, and hot isostatic pressing + direct aging were investigated by scanning electron microscope, transmission electron microscopy, and fatigue experiments. The standard heat treatment, hot isostatic pressing + solution treatment + aging, and hot isostatic pressing + direct aging resulted in the formation of more and smaller γ″ phases in the matrix in the nickel-based 718 superalloys. However, the grain boundaries of the hot isostatic pressing + direct aging sample showed many relatively coarse disk-like γ″ phases with major axes of ~80 nm and minor axes of ~40 nm. The hot isostatic pressing + direct aging sample with a stress amplitude of 380 MPa showed the longest high cycle fatigue life of 5.16 × 10 cycles. Laves phases and carbide inclusions were observed in the crack initiation zone, and the cracks propagated along the acicular δ phases in the nickel-based 718 superalloys. The precipitation of fine γ″ phases in the matrix and relatively coarse γ″ phases in the grain boundaries of the hot isostatic pressing + direct aging sample can hinder the movement of dislocation.
机译:通过扫描电子显微镜,透射电子显微镜研究了γ” -Ni Nb相对标准热处理,热等静压+固溶处理+时效,热等静压+直接时效的镍基718高温合金疲劳行为的影响。和疲劳实验。标准的热处理,热等静压+固溶处理+时效和热等静压+直接时效导致在镍基718高温合金的基体中形成越来越多的γ''相。然而,热等静压+直接时效样品的晶界显示出许多相对粗糙的盘状γ''相,其长轴为〜80 nm,短轴为〜40 nm。应力幅值为380 MPa的热等静压+直接老化样品显示出最长的高循环疲劳寿命为5.16×10个循环。在裂纹萌生区观察到Laves相和碳化物夹杂物,并且裂纹在镍基718高温合金中沿针状δ相扩展。热等静压+直接时效样品的基体中细的γ''相的析出和晶界中相对粗的γ''相的析出会阻碍位错的运动。

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