L-DED增材制造不同构建取向的铸态和热处理Inconel 625的力学性能

Juliane Ribeiro da Cruz , Henrique Santos Ferreira , Anselmo Thiesen Jr. , Jurandir Marcos Sá de Sousa
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摘要

镍基Inconel 625高温合金的增材制造,作为传统方法的替代方法,是生产近净形状零件的兴趣,由于该合金固有的高耐磨性和较差的可加工性。由于L-DED AM复杂的热历史,通常需要后处理热处理来消除应力和组织均匀化。本文研究了激光定向能沉积(L-DED)制备的Inconel 625试样在预制和热处理(900°C, 2 h)条件下的力学性能。通过光学和扫描电子显微镜以及能量色散光谱表征了显微结构。机械性能通过维氏硬度、拉伸和夏比冲击试验进行评估。讨论了构建取向和热处理的影响,并将结果与文献报道的商用Inconel 625进行了基准比较。结果表明:构建的样品呈柱状枝晶结构,晶粒外延生长,枝晶间存在富含Mo、Nb和si的Laves相;后处理热处理导致部分再结晶,晶界处形成Laves相和碳化物,使夏比能吸收比原状降低约40%。这种行为与观察到的变形Inconel 625相似。在拉伸作用下,晶界脆化降低了总伸长率,但不影响屈服强度和极限抗拉强度,这仍然优于ASTM B446-24所报告的Ni-Cr-Mo-Nb合金的预期。稍微优越的硬度,屈服强度和极限抗拉强度发现水平建造的标本。这一结果与其较高的冷却速率和微观结构的细化有关。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Mechanical performance of as-built and heat-treated Inconel 625 additively manufactured by L-DED with different build orientations

Mechanical performance of as-built and heat-treated Inconel 625 additively manufactured by L-DED with different build orientations
Additive manufacturing of the Ni-based Inconel 625 superalloy, as an alternative to conventional methods, is of interest to produce near-net-shape parts, due to this alloy's intrinsic high abrasiveness and poor machinability. Because of the complex thermal history of L-DED AM, post processing heat-treatments are often required for stress relief and microstructure homogenization. This work investigates the mechanical performance of Inconel 625 specimens manufactured by laser directed energy deposition (L-DED) in the as-built and heat-treated conditions (900 °C for 2 h). Microstructure was characterized by optical and scanning electron microscopy with energy dispersive spectroscopy. Mechanical properties were assessed by Vickers hardness, tensile, and Charpy impact tests. The effects of build orientation and heat-treatment were discussed, and results were benchmarked to those of commercial Inconel 625 reported in the literature. Results show that the as-built samples developed a columnar dendritic microstructure with epitaxial grain growth, and the presence of Mo, Nb, and Si-rich interdendritic Laves phase. The post processing heat-treatment led to partial recrystallization and formation of Laves phase and carbides at grain boundaries, which caused a Charpy energy absorption reduction of about 40 % compared with the as-built condition. This behavior was similar to that observed for the wrought Inconel 625. Under tensile solicitations, the grain boundary embrittlement decreased the total elongation but did not compromise yield strength and ultimate tensile strength, which remained superior to those expected from Ni–Cr–Mo–Nb alloys, as reported by ASTM B446-24. Slightly superior hardness, yield strength, and ultimate tensile strength were found for horizontally built specimens. This outcome is associated with its higher cooling rates and microstructure refinement.
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