The effect of laser shock peening, shot peening and their combination on the microstructure and fatigue properties of Ti-6Al-4V titanium alloy

[Display omitted] •The fatigue life can be significantly improved (up to 9.3 times) by (LSP+SP).•Gradient microstructure with dislocations and novel CRS distribution can be induced.•Fatigue crack initiation can be hindered by the high-density dislocation layer.•Fatigue crack growth rate can be retar...

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Veröffentlicht in:	International journal of fatigue Jg. 153; S. 106465
Hauptverfasser:	Luo, Xuekun, Dang, Ning, Wang, Xin
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Kidlington Elsevier Ltd 01.12.2021 Elsevier BV
Schlagworte:	Compressive properties Crack initiation Crack propagation Dislocation density Fatigue failure Fatigue life Fractography Fracture mechanics Laser shock processing Materials fatigue Metal fatigue Microstructure Microstructures Residual stress Residual stresses Shot peening Surface treatments Titanium alloys Titanium base alloys Surface treatments Shot peening Microstructures Residual stresses Fractography
ISSN:	0142-1123, 1879-3452
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Abstract	[Display omitted] •The fatigue life can be significantly improved (up to 9.3 times) by (LSP+SP).•Gradient microstructure with dislocations and novel CRS distribution can be induced.•Fatigue crack initiation can be hindered by the high-density dislocation layer.•Fatigue crack growth rate can be retarded by the dislocation proliferation layer. In this work, the effect of a novel post process integrating laser shock peening (LSP) with shot peening (SP) on the fatigue property of Ti-6Al-4V titanium alloy is investigated. The fatigue life can be improved (up to 9.3 times) by this post-process. The compressive residual stress (CRS) distribution and dislocation-gradient microstructure obtained were found to be responsible for the improvement. The fatigue crack initiation was hindered by the high-density dislocation layer with high CRS value on the surface and maximum CRS in the sub-surface, while the crack propagation was retarded by the dislocation proliferation layer with large CRS gradient.
AbstractList	In this work, the effect of a novel post process integrating laser shock peening (LSP) with shot peening (SP) on the fatigue property of Ti-6Al-4V titanium alloy is investigated. The fatigue life can be improved (up to 9.3 times) by this post-process. The compressive residual stress (CRS) distribution and dislocation-gradient microstructure obtained were found to be responsible for the improvement. The fatigue crack initiation was hindered by the high-density dislocation layer with high CRS value on the surface and maximum CRS in the sub-surface, while the crack propagation was retarded by the dislocation proliferation layer with large CRS gradient. [Display omitted] •The fatigue life can be significantly improved (up to 9.3 times) by (LSP+SP).•Gradient microstructure with dislocations and novel CRS distribution can be induced.•Fatigue crack initiation can be hindered by the high-density dislocation layer.•Fatigue crack growth rate can be retarded by the dislocation proliferation layer. In this work, the effect of a novel post process integrating laser shock peening (LSP) with shot peening (SP) on the fatigue property of Ti-6Al-4V titanium alloy is investigated. The fatigue life can be improved (up to 9.3 times) by this post-process. The compressive residual stress (CRS) distribution and dislocation-gradient microstructure obtained were found to be responsible for the improvement. The fatigue crack initiation was hindered by the high-density dislocation layer with high CRS value on the surface and maximum CRS in the sub-surface, while the crack propagation was retarded by the dislocation proliferation layer with large CRS gradient.
ArticleNumber	106465
Author	Luo, Xuekun Wang, Xin Dang, Ning
Author_xml	– sequence: 1 givenname: Xuekun surname: Luo fullname: Luo, Xuekun email: luoxuekun1987@163.com organization: AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China – sequence: 2 givenname: Ning surname: Dang fullname: Dang, Ning organization: School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China – sequence: 3 givenname: Xin surname: Wang fullname: Wang, Xin organization: AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
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Snippet	[Display omitted] •The fatigue life can be significantly improved (up to 9.3 times) by (LSP+SP).•Gradient microstructure with dislocations and novel CRS... In this work, the effect of a novel post process integrating laser shock peening (LSP) with shot peening (SP) on the fatigue property of Ti-6Al-4V titanium...
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SubjectTerms	Compressive properties Crack initiation Crack propagation Dislocation density Fatigue failure Fatigue life Fractography Fracture mechanics Laser shock processing Materials fatigue Metal fatigue Microstructure Microstructures Residual stress Residual stresses Shot peening Surface treatments Titanium alloys Titanium base alloys
Title	The effect of laser shock peening, shot peening and their combination on the microstructure and fatigue properties of Ti-6Al-4V titanium alloy
URI	https://dx.doi.org/10.1016/j.ijfatigue.2021.106465 https://www.proquest.com/docview/2584777873
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