热处理对选择性激光熔炼Co-Cr合金组织、残余应力和力学性能的影响。

Kyung-Ho Ko, Hyeon-Goo Kang, Yoon-Hyuk Huh, Chan-Jin Park, L. Cho
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引用次数: 14

摘要

钴铬钼(CCM)牙科合金的力学性能和残余应力取决于其制造和后处理方法,这影响着义齿的预后。比较了两种采用铸造和选择性激光熔炼(SLM)制备的CCM合金,并评价了热处理温度对SLM制备CCM合金的影响。通过铸造(Cast-Co-Cr)和SLM(SLM-Co-Cr)制备试样。SLM-Co-Cr试样在750、950和1150°C下进行热处理,以比较其性能。通过扫描电子显微镜(SEM)、能量色散X射线光谱(EDS)和电子背散射衍射(EBSD)分析微观结构,并通过X射线衍射(XRD)测量残余应力。通过维氏硬度测试和拉伸测试来评估机械性能;之后进行了分形学检查。与铸造Co-Cr相比,SLM-Co-Cr组表现出孔隙率降低、晶粒尺寸减小、固溶极限增加和高残余应力;极限抗拉强度、屈服强度和硬度也较高。显微组织、残余应力和机械性能随热处理的不同而有显著差异,强度和硬度表现出与伸长率相反的趋势。在750°C热处理后,I型残余应力大部分降低,但即使在1150°C热处置后,II型和III型残余应力仍保持不变。SLM呈现出优于铸件的机械性能。考虑到拉伸残余应力的降低和延展性的提高,CCM合金应在950°C或更高的温度下进行热处理。
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Effects of heat treatment on the microstructure, residual stress, and mechanical properties of Co-Cr alloy fabricated by selective laser melting.
The mechanical properties and residual stress of dental Co-Cr-Mo (CCM) alloy depend on the manufacturing and post-processing methods, which affect the prognosis of dental prostheses. Two CCM alloys manufactured by casting and selective laser melting (SLM) were compared, and the effect of heat treatment temperature for CCM alloys manufactured by SLM method was evaluated. Specimens were fabricated by casting (Cast Co-Cr) and SLM (SLM Co-Cr). SLM Co-Cr specimens were heat treated at 750, 950, and 1150 °C to compare their properties. Microstructures were analyzed via scanning electron microscopy (SEM), energy dispersive X-ray spectroscopy (EDS), and electron backscattered diffraction (EBSD), and the residual stress was measured via x-ray diffraction (XRD). Mechanical properties were evaluated by a Vickers hardness test and a tensile test; fractography was performed after this. The SLM Co-Cr group exhibited a decrease in porosity, grain size, increase in solid solution limit, and high residual stress compared to Cast Co-Cr; the ultimate tensile strength, yield strength, and hardness were also higher. The microstructures, residual stresses, and mechanical properties differed significantly depending on the heat treatment, and the strength and hardness showed a tendency inverse to that of the elongation. Type I residual stresses mostly decreased after 750 °C heat treatment, however type II and III residual stresses remained even after 1150 °C heat treatment. SLM presented superior mechanical properties to casting. Considering the reduction of tensile residual stress and increased ductility, CCM alloys should be heat treated at a temperature of 950 °C or higher.
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