High‐Cycle Fatigue Properties at Cryogenic Temperatures in INCONEL 718

Y. Ono, T. Yuri, H. Sumiyoshi, Etsuo Takeuchi, S. Matsuoka, T. Ogata
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引用次数: 7

Abstract

High‐cycle fatigue properties at 4 K, 20 K, 77 K and 293 K were investigated in forged‐INCONEL 718 nickel‐based superalloy with a mean gamma (γ) grain size of 25 μm. In the present material, plate‐like delta phase precipitated at γ grain boundaries and niobium (Nb)‐enriched MC type carbides precipitated coarsely throughout the specimens. The 0.2% proof stress and the tensile strength of this alloy increased with decreasing temperature, without decreasing elongation or reduction of area. High‐cycle fatigue strengths also increased with decreasing temperature although the fatigue limit at each temperature didn’t appear even around 107 cycles. Fatigue cracks initiated near the specimen surface and formed faceted structures around crack initiation sites. Fatigue cracks predominantly initiated from coarse Nb‐enriched carbides and faceted structures mainly corresponded to these carbides. In lower stress amplitude tests, however, facets were formed through transgranular crack initiation and growth. These kinds o...
低温下INCONEL 718的高周疲劳性能
研究了平均γ (γ)晶粒尺寸为25 μm的锻造INCONEL 718镍基高温合金在4 K、20 K、77 K和293 K时的高周疲劳性能。在该材料中,片状三角洲相在γ晶界处析出,富铌(Nb)的MC型碳化物在整个试样中粗析出。随着温度的降低,合金的0.2%抗拉应力和抗拉强度增加,而伸长率和面积不减小。高周疲劳强度也随着温度的降低而增加,尽管在107次循环左右,每个温度下的疲劳极限都没有出现。疲劳裂纹在试样表面附近萌生,在裂纹萌生点周围形成多面结构。疲劳裂纹主要由粗大的富铌碳化物引起,这些碳化物的多面结构主要与这些碳化物相对应。而在较低应力幅值的试验中,通过穿晶裂纹的萌生和扩展形成了切面。这些类型的……
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