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Creep and Thermomechanical Fatigue of Functionally Graded Inconel 718 Produced by Additive Manufacturing

机译:通过增材制造生产的功能梯度Inconel 718的蠕变和热机械疲劳

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Inconel 718 is a nickel-based superalloy commonly used in aircraft engine and nuclear applications, where components experience severe mechanical stresses. Due to the typical high temperature applications, Thermo-Mechanical Fatigue (TMF) and creep tests are common benchmarks for such applications. Additive manufacturing offers a unique way of manufacturing Inconel 718 with high degree of design freedom. However, limited knowledge exists regarding the resulting high temperature properties. The objective of this work is to evaluate creep and TMF behaviour of Inconel 718, produced by selective laser melting (SLM). A novel microstructural design, allowing for grain size control was employed in this study. The obtained functionally graded Inconel 718, exhibiting core with coarse and outside shell with fine grained microstructure, allowed for the best trade-off between creep and fatigue performance. The post heat-treatment regimens and resulting microstructures are also evaluated and its influence on creep and TMF is discussed.
机译:Inconel 718是一种镍基高温合金,通常用于飞机发动机和核能应用中,在这些应用中组件会承受严重的机械应力。由于典型的高温应用,热机械疲劳(TMF)和蠕变测试是此类应用的常见基准。增材制造提供了具有高度设计自由度的独特制造Inconel 718的方式。但是,关于所得的高温特性的知识有限。这项工作的目的是评估通过选择性激光熔化(SLM)生产的Inconel 718的蠕变和TMF行为。在这项研究中采用了一种新颖的微观结构设计,可以控制晶粒尺寸。所获得的功能梯度Inconel 718的芯部具有粗糙的外壳,外壳具有精细的微观结构,因此可以在蠕变和疲劳性能之间取得最佳平衡。还评估了后热处理方案和所得的微结构,并讨论了其对蠕变和TMF的影响。

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