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增材制造GH3536合金的高温拉伸及疲劳裂纹扩展性能研究
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中南大学 材料科学与工程学院

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中图分类号:

TG146.1

基金项目:

国家自然科学基金(51901252);湖南省青年自然科学基金(2019JJ50817);国家重点研发计划(2018YFB1106000)


High Temperature Tensile and Fatigue Crack Propagation Properties of GH3536 Alloy Fabricated by Additive Manufacturing
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Affiliation:

中南大学

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国家自然科学基金(51901252);湖南省青年自然科学基金(2019JJ50817);国家重点研发计划(2018YFB1106000)

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    摘要:

    本文采用选区激光融化技术制备了GH3536合金试样,在进行了热等静压和固溶处理后对合金试样的显微组织、高温拉伸性能和不同应力比下的裂纹扩展性能进行了分析。研究结果表明,经热等静压和固溶处理后合金试样内部存在两种不同大小的等轴晶粒,在晶间存在连续片状分布的M23C6和M6C碳化物。合金试样的拉伸性能随着温度的上升而不断下降,断裂方式由室温下的韧性断裂转变为900℃下的脆性断裂。在不同应力比下,合金试样的裂纹扩展方式主要为穿晶扩展,裂纹扩展速率随着应力比的不断上升而提高,在高应力比下合金内部的疲劳裂纹更倾向于在取向差较小的晶粒内部扩展。

    Abstract:

    In this work, GH3536 alloy specimens were fabricated by selective laser melting (SLM). The microstructure, high temperature tensile properties and fatigue crack growth rate of the specimens were investigated after hot isostatic pressing and solution treatment. The results show that there are two kinds of equiaxed grains of different sizes in the alloy samples after hot isostatic pressing and solution treatment, and there are continuous lamellar distribution of M23C6 and M6C carbides between the grains. The tensile properties of the alloy specimens decreased continuously with the increase of temperature, and the fracture mode changed from ductile fracture at room temperature to brittle fracture at 900℃. Under different stress ratios, the crack propagation mode of the specimens is transgranular propagation. The increase of stress ratio will accelerate the crack growth rate, which is caused by the inclination of fatigue crack propagating through these grains with low grain boundary misorientation.

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肖来荣,彭振武,蔡圳阳,赵小军,钟琦,余华丽,王森,谭威.增材制造GH3536合金的高温拉伸及疲劳裂纹扩展性能研究[J].稀有金属材料与工程,2023,52(3):1015~1021.[XiaoLairong, PengZhenwu, CaiZhenyang, ZhaoXiaojun, ZhongQi, YuHuali, WangSen, TanWei. High Temperature Tensile and Fatigue Crack Propagation Properties of GH3536 Alloy Fabricated by Additive Manufacturing[J]. Rare Metal Materials and Engineering,2023,52(3):1015~1021.]
DOI:10.12442/j. issn.1002-185X.20220161

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历史
  • 收稿日期:2022-03-01
  • 最后修改日期:2022-04-18
  • 录用日期:2022-04-26
  • 在线发布日期: 2023-04-07
  • 出版日期: 2023-03-24