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热处理对选区激光熔化成形Ti2AlC/Inconel 718复合材料组织和力学性能的影响

Effect of heat treatment on the microstructure and mechanical properties of Ti2AlC/Inconel 718 composite materials formed by selective laser melting

  • 摘要: 采用选区激光熔化工艺制备了Ti2AlC/Inconel 718复合材料试样,分别对复合材料试样进行了直接双时效、固溶双时效、均匀化+固溶双时效3种热处理,研究了不同热处理工艺对复合材料微观组织及力学性能的影响。结果表明:经过直接双时效热处理后,试样的组织中含有大量白色Laves相析出物;经过固溶双时效处理后,在试样晶界处析出大量针状的白色δ相析出物,同时在晶内析出γ′相与γ″相,形状为球状与圆盘状;相较于直接双时效与固溶双时效,经过均匀化+固溶双时效处理的Ti2AlC/Inconel 718复合材料组织中的Laves相明显减少,但是碳化物的析出增多,并且大多沿晶界分布。由于γ′相与γ″相的析出,直接双时效处理试样显微硬度和拉伸强度明显提升,但由于强度的提升及沉积态Laves相未被充分溶解,导致断后延伸率及收缩率下降。固溶双时效处理和均匀化+固溶时效处理后的材料组织均发生了再结晶,抵消了选区激光熔化成形工艺获得的快速凝固组织,同时由于在晶界处析出了针状δ相,消耗了强化元素Nb,降低了γ″相与γ′相的析出,导致强度相对于直接双时效处理试样明显下降,塑性提升,达到了10.5%,满足了该材料的使用标准。

     

    Abstract: Ti2AlC/Inconel 718 composites were prepared by selective laser melting (SLM) process. Three types of heat treatments were carried out on the composites, respectively: direct double aging (DA), solution double aging (SA), and homogenization+solution double aging (HSA). The effects of heat treatments on the microstructure and mechanical properties of the composites were studied. The results show that after the direct double aging heat treatment, the microstructure of the samples contains a large amount of white Laves phase precipitates. After the solution double aging treatment, a large number of needle-shaped white δ-phase precipitates are formed at the grain boundaries. Meanwhile, γ′ phases and γ″ phases are precipitated within the grains, with shapes being spherical and disc-shaped. The Laves phases in the Ti2AlC/Inconel 718 composites after the homogenization+solution double aging treatment are significantly less than those in the samples treated with direct double aging or solution double aging. However, the precipitation of carbides increases, and most of them are distributed along the grain boundaries. After the direct double aging treatment, due to the precipitation of γ′ phases and γ″ phases, the microhardness and tensile strength are significantly improved. However, due to the increase in strength and the insufficient dissolution of the deposited Laves phases, the elongation after fracture and the contraction rate are decreased. After the solution double aging treatment and the homogenization+solution double aging treatment, the Ti2AlC/Inconel 718 composites undergo recrystallization, which counteracts the rapid solidification microstructure obtained by SLM. Meanwhile, compared to the samples treated with direct double aging, due to the precipitation of needle-shaped δ phases at the grain boundaries, the strengthening element Nb is consumed, and the precipitation of γ″ and γ′ phases is reduced, resulting in a significant decrease in strength. The plasticity increases by 10.5%, meeting the usage standards of this material.

     

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