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Hydrogen's Absorption/Desorption Behavior in Gaseous-Phase Charged Duplex-Annealed Ti-6AI-4V Alloy

机译:气相带电双相退火Ti-6AI-4V合金中氢的吸收/解吸行为

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Ti-6Al-4V alloy has proven to be technically superior and cost-effective materials for a wide variety of aerospace, industrial, marine and commercial applications. The mechanical properties of Ti-6Al-4V are very sensitive to the microstructure obtained after the thermo-mechanical treatment. The duplex structures provide good tensile ductility, fatigue strength, resistance to microcrack growth and crack initiation, and are often used in demanding fatigue critical tasks. However, although Ti-6A-4V is considered to be reasonably resistance to chemical attack, severe problems can arise when it comes in contact with hydrogen-containing environments due to its susceptibility to hydrogen embrittlement. The objective of this paper is to investigate the absorption and desorption behavior of external hydrogen on a duplex-annealed Ti-6Al-4V alloy. While investigating the desorption profile, we seek to better understand the thermodynamics and the kinetic nature of the interaction between traps and hydrogen atoms, with specific emphasis on the investigation of the impact of these interactions on the microstructure of the studied aerospace applicative titanium alloy. In order to achieve these goals, thermal desorption spectroscopy (TDS) was applied and the data obtained from this analysis was supported by a variety of other experimental techniques, such as LECO hydrogen determinator, XRD and microstructure investigations by means of optic and electronic microscopy. Hydrogen was found to influence significantly the microstructure of the alloy. The process of hydrogen evolution was found to be a very complex process, being affected mainly by the phase transformations that may occur during the thermal analysis.
机译:Ti-6Al-4V合金已被证明是技术卓越且具有成本效益的材料,可广泛用于航空航天,工业,船舶和商业应用。 Ti-6Al-4V的机械性能对热机械处理后获得的微观结构非常敏感。双相结构提供良好的拉伸延展性,疲劳强度,抗微裂纹增长和裂纹萌生的能力,通常用于要求苛刻的疲劳任务。然而,尽管认为Ti-6A-4V具有一定的耐化学腐蚀性能,但由于其易受氢脆性的影响,当与含氢环境接触时,仍可能出现严重的问题。本文的目的是研究双退火Ti-6Al-4V合金上外部氢的吸收和解吸行为。在研究解吸曲线时,我们试图更好地理解陷阱与氢原子之间相互作用的热力学和动力学性质,特别着重于研究这些相互作用对所研究的航空航天应用钛合金的微观结构的影响。为了实现这些目标,应用了热脱附光谱法(TDS),并通过各种其他实验技术(例如LECO氢测定仪,XRD和通过光学和电子显微镜进行的显微结构研究)来支持从该分析中获得的数据。发现氢显着影响合金的微观结构。发现氢的释放过程是一个非常复杂的过程,主要受热分析过程中可能发生的相变影响。

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