Singla Anil Kumar, Singh Jagtar, Sharma Vishal S, Gupta Munish Kumar, Song Qinghua, Rozumek Dariusz, Krolczyk Grzegorz M
Department of Mechanical Engineering, Sant Longowal Institute of Engineering and Technology, Longowal-148106, Punjab, India.
Department of Industrial and Production Engineering, Dr B R Ambedkar National Institute of Technology, Jalandhar-144011, Punjab, India.
Materials (Basel). 2020 Jan 21;13(3):500. doi: 10.3390/ma13030500.
The poor fatigue strength of Ti-6Al-4V ELI is a main cause of failure in structural implants. In this work, Ti-6Al-4V ELI was subjected to β-solution treatment to obtain martensite microstructure and further subjected to -196 °C for 24 h. Significant improvement in high cycle fatigue performance of martensite Ti-6Al-4V ELI was observed on exposure to cryogenic cycle. Resistance to fatigue crack growth of alloy was augmented in martensite structure as compared with mill annealed sample and the same was retained even after exposure to cryogenic treatment. The variation observed in fatigue behavior due to cryogenic treatment was correlated with fractography and metallurgical investigations. Improvement in high cycle fatigue performance can be attributed to a combined effect of a decrease in the size of prior β grain, formation of massive α patch and its subsequent transformation into ultra-fine α and β during the soaking period at -196 °C.
Ti-6Al-4V ELI疲劳强度较差是结构植入物失效的主要原因。在本研究中,对Ti-6Al-4V ELI进行β固溶处理以获得马氏体微观结构,并进一步在-196°C下处理24小时。观察到马氏体Ti-6Al-4V ELI在经历低温循环后,其高周疲劳性能有显著改善。与轧态退火样品相比,合金在马氏体结构中的疲劳裂纹扩展阻力有所增强,并且即使在经过低温处理后仍保持这一特性。通过断口分析和金相研究,揭示了低温处理导致的疲劳行为变化。高周疲劳性能的改善可归因于以下综合效应:原始β晶粒尺寸减小、块状α相的形成以及在-196°C保温期间其随后转变为超细α相和β相。