D.A. Ariza , E. Arrieta , C. Banuelos , B.J. Colón , L.E. Murr , R.B. Wicker , C. Beamer , F. Medina
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Similarly, tensile and hardness testing were implemented to study the mechanical properties, where due to the effects of the HIP treatments, higher ductility but lower hardness values were recorded. Furthermore, fracture morphologies and stress-life (cycles-to-failure) (S–N) curves of the Ti–6Al–4V specimens concerning the fatigue behavior were analyzed. The HIP treatment groups behaved similarly during 4-point bending and uniaxial testing, with the LTHP obtaining a superior fatigue life behavior, followed by the standard and super beta HIP groups. In addition, the efficacy of HIP to reduce pores showed better results in the 4-point bending specimens, leading to few defects as fatigue initiators in contrast to the uniaxial specimens. Fractography results suggested that defects and microstructural features acting as fatigue crack initiators (FCI) govern the fracture behavior of uniaxial specimens. 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引用次数: 0
摘要
本研究调查了热等静压(HIP)在四点弯曲和单轴测试下对激光粉末床融合(L-PBF)Ti-6Al-4V 合金疲劳性能的影响。研究了三种 HIP 循环:标准、低温/高压 (LTHP) 和超级β。此外,还将退火热处理组与 HIP 组进行了比较。在研究过程中,对各种热处理的材料微观结构进行了分析和比较,结果表明存在α′马氏体、α+β维德曼斯泰滕和粗大的等轴晶粒。同样,还进行了拉伸和硬度测试,以研究其机械性能,由于 HIP 处理的影响,记录显示延展性较高,但硬度值较低。此外,还分析了 Ti-6Al-4V 试样有关疲劳行为的断裂形态和应力-寿命(失效循环)(S-N)曲线。在四点弯曲和单轴测试中,HIP 处理组的表现相似,其中 LTHP 组的疲劳寿命表现更优,其次是标准 HIP 组和超贝塔 HIP 组。此外,在 4 点弯曲试样中,HIP 减少孔隙的效果更好,与单轴试样相比,很少有缺陷作为疲劳引发剂。断裂分析结果表明,缺陷和微结构特征可作为疲劳裂纹引发剂(FCI)控制单轴试样的断裂行为。相比之下,只有微结构特征的存在才能控制四点弯曲破坏行为。
Comparison of fatigue life behavior between 4-point and uniaxial loading for L-PBF Ti–6Al–4V after HIP treatments
The present study investigated the effects of Hot Isostatic Pressing (HIP) on the fatigue performance of Laser Powder Bed Fusion (L-PBF) Ti–6Al–4V alloy under both 4-point bending and uniaxial testing. Three HIP-cycles were examined: standard, low temperature/high pressure (LTHP), and super beta. Moreover, an annealed heat treatment group was incorporated to compare against the HIP groups. The material microstructure was analyzed and compared across the heat treatments during the study, which showed the presence of α′ martensites, α+β Widmanstätten, and coarse equiaxed grains. Similarly, tensile and hardness testing were implemented to study the mechanical properties, where due to the effects of the HIP treatments, higher ductility but lower hardness values were recorded. Furthermore, fracture morphologies and stress-life (cycles-to-failure) (S–N) curves of the Ti–6Al–4V specimens concerning the fatigue behavior were analyzed. The HIP treatment groups behaved similarly during 4-point bending and uniaxial testing, with the LTHP obtaining a superior fatigue life behavior, followed by the standard and super beta HIP groups. In addition, the efficacy of HIP to reduce pores showed better results in the 4-point bending specimens, leading to few defects as fatigue initiators in contrast to the uniaxial specimens. Fractography results suggested that defects and microstructural features acting as fatigue crack initiators (FCI) govern the fracture behavior of uniaxial specimens. In contrast, only the presence of microstructural features controls the 4-point bending failure behavior.