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Microstructure and fatigue performance of SLM-fabricated Ti6Al4V alloy after different stress-relief heat treatments

机译:SLM制造的Ti6Al4V合金在不同应力释放热处理后的组织和疲劳性能

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The main interest in Additive Manufacturing (AM) technology relates to its ability to produce complex components with relatively reduced weight that are difficult to produce or cannot be produced by other conventional technologies. Selective laser melting (SLM) is extensively used, as one of the AM technologies to fabricate metallic parts. This advanced method allows to produce various parts with complex geometries with high three-dimensional (3D) accuracy from fusion powders in a layer-by-layer style.Ti6Al4V alloy is a widely used material for structural applications in aerospace and biomedical due to high specific fatigue strength. SLM processing makes this alloy attractive when weight reduction is a design objective. The SLM Ti6Al4V microstructure is influenced by process parameters and build orientation. The localized high energy input during very short interaction times leads to the formation of very fine structures and to the generation of internal stresses. Therefore, the SLM parts are heat treated to decrease or completely remove residual stresses.The present study aims at evaluating the effect of stress-relief heat treatments on the microstructure, the mechanical properties and the fatigue performance of SLM Ti6Al4V alloy. Ti6Al4V alloy specimens were manufactured according to the SLM process with an EOS M290 system. Post fabrications heat treatments at different temperatures (i.e. 740?C vs. 900?C) resulted in different structure and mechanical properties that were identified and measured. Fatigue testing of specimens with as-built surfaces was performed at room temperature on modified Schenk-type fatigue testing machine applying a pulsating plane bending (load cycle ratio R = 0) to the specimens at a frequency f = 15 Hz.
机译:增材制造(AM)技术的主要兴趣在于其能够生产重量相对减轻的复杂组件的能力,这些组件难以生产或无法通过其他常规技术生产。选择性激光熔化(SLM)被广泛用作制造金属零件的增材制造技术之一。 Ti6Al4V合金是一种先进的方法,可以以逐层的方式用熔融粉末生产具有高三维(3D)精度的复杂几何形状的各种零件。疲劳强度。当减轻重量成为设计目标时,SLM处理使这种合金具有吸引力。 SLM Ti6Al4V的微观结构受工艺参数和构建方向的影响。在非常短的相互作用时间内输入的局部高能量会导致形成非常精细的结构并产生内应力。因此,对SLM零件进行热处理以减少或完全消除残余应力。本研究旨在评估应力消除热处理对SLM Ti6Al4V合金的组织,力学性能和疲劳性能的影响。 Ti6Al4V合金试样是根据SLM工艺和EOS M290系统制造的。在不同温度(即740°C与900°C)下进行的后期加工热处理会导致识别和测量不同的结构和机械性能。在室温下,在改良的Schenk型疲劳试验机上对表面成形的试样进行疲劳试验,该试验机以f = 15 Hz的频率对试样施加脉动平面弯曲(载荷循环比R = 0)。

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