1. 烟台大学精准材料高等研究院,烟台,264005
2. 上海交通大学,上海,200240
3. 北京钢研高纳科技股份有限公司,北京,100081
纸质出版:2024
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张尚洲,李子福,王瑞,孙广宝,刘国浩,于鸿垚. 热处理对选区激光熔化GH4061合金组织和性能的影响[J]. 航空制造技术, 2024, 67(17): 14-19.
ZHANG Shangzhou, LI Zifu, WANG Rui, SUN Guangbao, LIU Guohao, YU Hongyao. Effect of Heat Treatment on Microstructure and Properties of GH4061 Alloy by Selective Laser Melting[J]. Aeronautical Manufacturing Technology, 2024, 67(17): 14-19.
张尚洲,李子福,王瑞,孙广宝,刘国浩,于鸿垚. 热处理对选区激光熔化GH4061合金组织和性能的影响[J]. 航空制造技术, 2024, 67(17): 14-19. DOI: 10.16080/j.issn1671-833x.2024.17.014.
ZHANG Shangzhou, LI Zifu, WANG Rui, SUN Guangbao, LIU Guohao, YU Hongyao. Effect of Heat Treatment on Microstructure and Properties of GH4061 Alloy by Selective Laser Melting[J]. Aeronautical Manufacturing Technology, 2024, 67(17): 14-19. DOI: 10.16080/j.issn1671-833x.2024.17.014.
采用激光选区熔化成形技术制备了GH4061合金,研究了不同热处理工艺对合金组织和性能的影响。结果表明,沉积态合金的柱状晶穿过多个熔池外延生长,晶内由胞状亚晶结构组成。随着固溶温度的升高,晶粒取向逐渐偏向(101)和(111),晶粒长大;Laves相由长链状转变为颗粒状,1060 ℃固溶温度时基本溶解;δ相在晶界析出,由粗大块状转变为盘状,然后再转变为短棒状,1100 ℃热处理时无δ 相析出; 980 ℃、1020 ℃、1060 ℃、1100 ℃固溶温度时γ′和γ″相平均尺寸分别为23.53 nm、24.43 nm、25.34 nm 和25.66 nm。热处理后合金的室温和650 ℃力学性能显著提高,其中980 ℃固溶时效热处理试样的室温和650 ℃抗拉强度分别达到1342 MPa 和1120 MPa,随着固溶温度的升高,1020 ℃、1060 ℃、1100 ℃固溶温度时试样室温抗拉强度分别下降约6.4%、8.3% 和10%,650 ℃抗拉强度分别下降约7.9%、8.8% 和11%,塑性有所提高。
The study investigated the impact of heat treatment on the microstructure and tensile properties of GH4061 alloys fabricated by selective laser melting. Findings demonstrated that the as-built columnar grains experienced epitaxial growth spanning multiple molten pools
resulting in the formation of cellular substructures. Following heat treatment
as the solid solution temperature increased
there was a gradual shift in grain orientation towards the (101) and (111) crystal planes. The Laves phase transitioned from elongated chains to granular forms and dissolved at approximately 1060 ℃. The δ phases that precipitated at grain boundaries transformed from coarse bulk structures to disc-shaped
and eventually to short rod-shaped configurations. The average sizes of γ′ and γ″ phases are 23.53 nm
24.43 nm
25.34 nm and 25.66 nm at solution temperature of 980 ℃
1020 ℃
1060 ℃
1100 ℃
respectively. The mechanical properties of the alloys after heat treatment show significant improvement at both room temperature and 650 ℃. Specifically
the tensile strengths at room temperature and 650 ℃ for the sample subjected to the 980 ℃ solid solution aging heat treatment are 1342 MPa and 1120 MPa
respectively. As the solid solution temperature increases
the room temperature tensile strength at 1020 ℃
1060 ℃ and 1100 ℃ decreases by approximately 6.4%
8.3%
and 10% than that at 980 ℃
respectively. At 650 ℃
the tensile strength at 1020 ℃
1060 ℃ and 1100 ℃ decreases by approximately 7.9%
8.8%
and 11% than that at 980 ℃
respectively
while the plasticity increases.
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