Effects of laser shock peening on the ultra-high cycle fatigue performance of additively manufactured Ti6Al4V alloy

被引:61
作者
Jiang, Qinghong [1 ,2 ]
Li, Shuai [1 ,3 ]
Zhou, Cong [1 ]
Zhang, Bi [1 ]
Zhang, Yongkang [4 ]
机构
[1] Southern Univ Sci & Technol, Dept Mech & Energy Engn, Shenzhen 518055, Peoples R China
[2] Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong, Peoples R China
[3] Harbin Inst Technol, Sch Mechatron Engn, Harbin 150001, Peoples R China
[4] Guangdong Univ Technol, Sch Mech & Elect Engn, Guangzhou 510006, Guangdong, Peoples R China
基金
中国国家自然科学基金;
关键词
Metal additive manufacturing; Selective laser melting; Laser shock peening; Ultra-high cycle fatigue; Ti6Al4V titanium alloy;
D O I
10.1016/j.optlastec.2021.107391
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Although additive manufacturing (AM) allows to fabricate metallic parts with a high static strength comparable to their forged counterparts, the fatigue strength of an AM-ed part is generally inferior, restricting AM from many critical applications. In this study, laser shock peening (LSP) was applied to modify the surface properties of selective laser melting fabricated (SLM-ed) Ti6Al4V titanium alloy. This study performs systematic tests and analyses on the fabricated alloy specimens to characterize their microstructures and mechanical properties including residual stress, tensile strength, ultra-high cycle fatigue (UHCF) strength. The results reveal that LSP can refine microstructure, suppress residual stresses, and delay crack propagation in the affected area. However, the inherent defects in an SLM-ed part, such as unmelted powders, lack of fusion and clusters of alpha phase, dominate the fatigue failure of the specimens especially in the UHCF regime, resulting in their poor fatigue performance. Meanwhile, The LSP processed specimens showed a lower S-N curve than that of specimens without LSP processing especially in the UHCF regime, which not only results from the inherent defects, but also the increased surface roughness and non-uniform residual stresses.
引用
收藏
页数:11
相关论文
共 92 条
[1]  
Aboulkhair N. T., 2014, ADDIT MANUF, V1-4, P77, DOI [DOI 10.1016/J.ADDMA.2014.08.001, 10.1016/j.addma.2014.08.001]
[2]   Defect-dominated fatigue behavior in type 630 stainless steel fabricated by selective laser melting [J].
Akita, Masayuki ;
Uematsu, Yoshihiko ;
Kakiuchi, Toshifumi ;
Nakajima, Masaki ;
Kawaguchi, Ryosei .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2016, 666 :19-26
[3]   Effect of build geometry on the β-grain structure and texture in additive manufacture of Ti-6Al-4V by selective electron beam melting [J].
Antonysamy, A. A. ;
Meyer, J. ;
Prangnell, P. B. .
MATERIALS CHARACTERIZATION, 2013, 84 :153-168
[4]   Influence of cryogenic cooling on tool wear and chip formation in turning of titanium alloy [J].
Aramcharoen, Ampara .
7TH HPC 2016 - CIRP CONFERENCE ON HIGH PERFORMANCE CUTTING, 2016, 46 :83-86
[5]   An overview of residual stresses in metal powder bed fusion [J].
Bartlett, Jamison L. ;
Li, Xiaodong .
ADDITIVE MANUFACTURING, 2019, 27 :131-149
[6]   Low- and high-cycle fatigue resistance of Ti-6Al-4V ELI additively manufactured via selective laser melting: Mean stress and defect sensitivity [J].
Benedetti, M. ;
Fontanari, V. ;
Bandini, M. ;
Zanini, F. ;
Carmignato, S. .
INTERNATIONAL JOURNAL OF FATIGUE, 2018, 107 :96-109
[7]  
[薛红前 Xue Hongqian], 2004, [航空学报, Acta Aeronautica et Astronautica Sinica], V25, P425
[8]   Investigation of the accuracy and roughness in the laser powder bed fusion process [J].
Calignano, F. .
VIRTUAL AND PHYSICAL PROTOTYPING, 2018, 13 (02) :97-104
[9]   Defect, Microstructure, and Mechanical Property of Ti-6Al-4V Alloy Fabricated by High-Power Selective Laser Melting [J].
Cao, Sheng ;
Chen, Zhuoer ;
Lim, Chao Voon Samuel ;
Yang, Kun ;
Jia, Qingbo ;
Jarvis, Tom ;
Tomus, Dacian ;
Wu, Xinhua .
JOM, 2017, 69 (12) :2684-2692
[10]   The effect of residual stresses arising from laser shock peening on fatigue crack growth [J].
Chahardehi, A. ;
Brennan, F. P. ;
Steuwer, A. .
ENGINEERING FRACTURE MECHANICS, 2010, 77 (11) :2033-2039