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高温下选择性激光熔化制备的Inconel 718合金的超高周疲劳行为

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

作者信息

Song Zongxian, Gao Wenbin, Wang Dongpo, Wu Zhisheng, Yan Meifang, Huang Liye, Zhang Xueli

机构信息

School of Materials Science and Engineering, Taiyuan University of Science and Technology, Taiyuan 030024, China.

School of Aeronautics and Astronautics, Tianjin Sino-German University of Applied Sciences, Tianjin 300350, China.

出版信息

Materials (Basel). 2021 Feb 20;14(4):1001. doi: 10.3390/ma14041001.

Abstract

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 10 cycles for the SLM alloy but significantly reduced the fatigue strength in the VHCF regime above 10 cycles. Both the SLM and wrought specimens exhibited similar fatigue resistance in the fatigue life regime of fewer than 10-10 cycles at elevated temperature, and the surface initiation mechanism was dominant in both alloys. In a VHCF regime above 10-10 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.

摘要

本研究调查了通过选择性激光熔化(SLM)制造的Inconel 718合金在高温(650°C)下的超高周疲劳(VHCF)行为。并将结果与锻造合金的结果进行了比较。SLM合金呈现出大的柱状晶粒,晶粒内部具有胞状组织,沿晶界析出Laves/δ相,而锻造合金中存在细小的等轴晶粒。在低于10次循环的范围内,高温对SLM合金的抗疲劳性能影响较小,但在高于10次循环的VHCF范围内显著降低了疲劳强度。在高温下少于10^10次循环的疲劳寿命范围内,SLM和锻造试样均表现出相似的抗疲劳性能,且两种合金均以表面萌生机制为主导。在高温下高于10^10次循环的VHCF范围内,锻造材料的抗疲劳性能略优于SLM合金。所有疲劳裂纹均从内部缺陷或微观结构不连续处萌生。在高温疲劳试验后检查了Laves和δ相的析出情况,并讨论了微观结构对微观结构小裂纹形成和扩展的影响。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9a27/7924031/1e4b2f9f54ba/materials-14-01001-g001.jpg

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