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Very-High-Cycle Fatigue Behavior of Inconel 718 Alloy Fabricated by Selective Laser Melting at Elevated Temperature

机译:通过选择性激光熔化在升高的温度下通过选择性激光熔化制造的Inconel 718合金的非常高循环疲劳行为

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摘要

This study investigates the very-high-cycle fatigue (VHCF) behavior at elevated temperature (650 °C) of the Inconel 718 alloy fabricated by selective laser melting (SLM). The results are compared with those of the wrought alloy. Large columnar grain with a cellular structure in the grain interior and Laves/δ phases precipitated along the grain boundaries were exhibited in the SLM alloy, while fine equiaxed grains were present in the wrought alloy. The elevated temperature had a minor effect on the fatigue resistance in the regime below 108 cycles for the SLM alloy but significantly reduced the fatigue strength in the VHCF regime above 108 cycles. Both the SLM and wrought specimens exhibited similar fatigue resistance in the fatigue life regime of fewer than 107–108 cycles at elevated temperature, and the surface initiation mechanism was dominant in both alloys. In a VHCF regime above 107–108 cycles at elevated temperature, the wrought material exhibited slightly better fatigue resistance than the SLM alloy. All fatigue cracks are initiated from the internal defects or the microstructure discontinuities. The precipitation of Laves and δ phases is examined after fatigue tests at high temperatures, and the effect of microstructure on the formation and the propagation of the microstructural small cracks is also discussed.
机译:本研究研究了通过选择性激光熔化(SLM)制造的Inconel 718合金的升高温度(650℃)的非常高循环疲劳(VHCF)行为。结果与锻造合金的结果进行了比较。在SLM合金中表现出谷物内部中具有蜂窝结构的大柱状颗粒和沿着晶界沉淀的Laves /Δ相,在锻造合金中存在精细等轴晶粒。升高的温度对SLM合金108次循环的疲劳电阻进行了微小的影响,但显着降低了高于108次循环的VHCF制度中的疲劳强度。 SLM和锻造试样均在升高的温度下疲劳寿命制度表现出类似的疲劳性,并且表面引发机理在两种合金中占主导地位。在高温下循环高于107-108周期的VHCF制度中,锻造材料表现出比SLM合金略高的疲劳性。所有疲劳裂缝都从内部缺陷或微观结构不连续引发。在高温下疲劳试验后,检查Laves和δ相的沉淀,还讨论了微观结构对形成和微观结构小裂缝的繁殖的影响。

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