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Comparison of AlSi7Mg0.6 alloy obtained by selective laser melting and investment casting processes: Microstructure and mechanical properties in as-built/as-cast and heat-treated conditions

机译:通过选择性激光熔融和熔模铸造工艺获得的AlSi7Mg0.6合金的比较:竣工/铸造和热处理条件下的显微组织和力学性能

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摘要

AlSi7Mg0.6 alloy is widely used in the automotive and aeronautical industries, and metal additive manufacturing (AM) is a breakthrough technology that motivates foundry companies to explore its potential in these industries; however, there is no deep knowledge of the mechanical properties and their relationship to microstructure in parts obtained by selective laser melting (SLM), as there is for parts obtained by casting. In this work, a comparison of the microstructure and mechanical properties of AlSi7Mg0.6 alloy obtained by SLM and investment casting processes was made. The mechanical properties of tensile specimens processed by both technologies were evaluated by uniaxial tensile tests and microhardness measurements in as-built/as-cast and heat-treated conditions with different build orientations in the case of SLM. An advanced characterization of the microstructure by field emission scanning electron microscopy (FESEM) and x-ray diffraction (XRD) analysis was also performed. After analyzing the microstructure and mechanical properties obtained with different heat treatments, the strengthening mechanisms of the two processes were identified. It is possible to obtain improved mechanical properties with SLM processing, exceeding the typical values required for aeronautical parts obtained in investment casting heat-treated (T6), and the ductility is satisfactory. Direct aging after SLM processing can effectively strengthen the AlSi7Mg0.6 alloy and is the more effective way to improve the as-built mechanical properties.
机译:AlSi7Mg0.6合金广泛用于汽车和航空工业,而金属增材制造(AM)是一项突破性技术,它促使铸造公司发掘其在这些行业中的潜力;但是,对于通过选择性激光熔化(SLM)获得的零件,其机械性能及其与微结构的关系尚无深入了解,对于铸造获得的零件也是如此。在这项工作中,对通过SLM和熔模铸造工艺获得的AlSi7Mg0.6合金的组织和力学性能进行了比较。在SLM的情况下,通过在建造/铸造和热处理条件下以不同构造方向进行的单轴拉伸试验和显微硬度测量,评估了两种技术处理的拉伸试样的机械性能。还通过场发射扫描电子显微镜(FESEM)和X射线衍射(XRD)分析对微观结构进行了高级表征。通过分析不同热处理获得的组织和力学性能,确定了这两个过程的强化机理。可以通过SLM加工获得改进的机械性能,超过在熔模铸造热处理(T6)中获得的航空零件所需的典型值,并且延展性令人满意。 SLM处理后的直接时效可以有效地增强AlSi7Mg0.6合金,并且是改善铸件力学性能的更有效方法。

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