Review on Anti-Fatigue Performance of Gradient Microstructures in Metallic Components by Laser Shock Peening

Author:

Yang Fei1,Liu Ping2,Zhou Liucheng1,He Weifeng1ORCID,Pan Xinlei1,An Zhibin1

Affiliation:

1. National Key Lab of Aerospace Power System Safety and Plasma Technology, Air Force Engineering University, Xi’an 710038, China

2. Institute of Aviation, Chongqing Jiaotong University, Chongqing 400074, China

Abstract

Laser-shock-peening technology is an international research hotspot in the surface-strengthening field, which utilizes the mechanical effects of laser-induced plasma shock waves to effectively improve the fatigue performance of metallic components by introducing the gradient microstructures and compressive residual stress into the surface layer of processed materials. The fatigue failure caused by high-frequency vibrations in aeroengines during service is the most important threat to flight safety, and this case is more prominent for military aeroengines because their service situation is harsher. The present paper focuses on components such as high-temperature components, fan/compressor blade, and thin-walled weldments, and it systematically introduces the researching findings about surface nanocrystallization and compressive residual stress formation mechanism in typical aeronautical metallic materials treated by laser shock peening. The contents mainly involve the characteristics, formation process, fatigue resistance mechanism, thermal stability of residual compressive stress, and nanocrystallization generated by laser shock peening.

Funder

Chongqing Natural Science Foundation

National Major Science and Technology Project of China

Publisher

MDPI AG

Subject

General Materials Science,Metals and Alloys

Reference79 articles.

1. Research progress and prospect of fatigue and structural integrity in aviation industry in China;Wang;Aeronaut. J.,2021

2. Laser Peening of Turbine Engine Integrally Blade Rotor;Zou;Chin. J. Lasers,2011

3. Machining the Integral Impeller and Blisk of Aero-Engines: A Review of Surface Finishing and Strengthening Technologies;Fu;Chin. J. Mech. Eng.,2017

4. Research progress and prospect of laser shock intensification for aeroengine components;Nie;J. Mech. Eng.,2021

5. Influence of high-speed milling parameter on 3D surface topography and fatigue behavior of TB6 titanium alloy;Yao;Trans. Nonferrous Met. Soc. China,2013

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