Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening

In order to improve fatigue life of GH3039 superalloy, GH3039 superalloy sheets were treated by laser shock peening (LSP). The microstructure of GH3039 superalloy before and after LSP was characterized using an optical microscope, transmission electron microscope (TEM), and X-ray diffractometer. The...

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Main Authors: Yang Tang, MaoZhong Ge, Yongkang Zhang, Taiming Wang, Wen Zhou
Format: Article
Language:English
Published: MDPI AG 2020-08-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/13/17/3849
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spelling doaj-73f9047c261b43ed926a66fc5adc100d2020-11-25T03:53:41ZengMDPI AGMaterials1996-19442020-08-01133849384910.3390/ma13173849Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock PeeningYang Tang0MaoZhong Ge1Yongkang Zhang2Taiming Wang3Wen Zhou4School of Materials Engineering, Jiangsu University of Technology, Changzhou 213001, ChinaSchool of Materials Engineering, Jiangsu University of Technology, Changzhou 213001, ChinaSchool of Electromechanical Engineering, Guangdong University of Technology, Guangzhou 510006, ChinaDevelopment department, China Aero Engine Group Changzhou Lanxiang Machinery Co., Ltd., Changzhou 213021, ChinaSchool of Materials Engineering, Jiangsu University of Technology, Changzhou 213001, ChinaIn order to improve fatigue life of GH3039 superalloy, GH3039 superalloy sheets were treated by laser shock peening (LSP). The microstructure of GH3039 superalloy before and after LSP was characterized using an optical microscope, transmission electron microscope (TEM), and X-ray diffractometer. The fatigue life of the samples with and without LSP was investigated by fatigue experiments. Moreover, surface profile and residual stress were also examined. Experimental results indicated that the grains in the surface layer of the LSP sample were remarkably refined and reached the nanometer scale. The average surface roughness increased from 0.024 μm to 0.19 μm after LSP. The average fatigue life of the laser treated samples was 2.01 times larger than that of the untreated specimens. Additionally, mathematical statistical analysis confirms that LSP has a significant influence on the fatigue life of GH3039 superalloy. The improvement of fatigue life for the laser processed GH3039 superalloy was mainly attributed to compressive residual stress and grain refinement generated by LSP.https://www.mdpi.com/1996-1944/13/17/3849laser shock peeningGH3039 superalloymicrostructurefatigue life
collection DOAJ
language English
format Article
sources DOAJ
author Yang Tang
MaoZhong Ge
Yongkang Zhang
Taiming Wang
Wen Zhou
spellingShingle Yang Tang
MaoZhong Ge
Yongkang Zhang
Taiming Wang
Wen Zhou
Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
Materials
laser shock peening
GH3039 superalloy
microstructure
fatigue life
author_facet Yang Tang
MaoZhong Ge
Yongkang Zhang
Taiming Wang
Wen Zhou
author_sort Yang Tang
title Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
title_short Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
title_full Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
title_fullStr Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
title_full_unstemmed Improvement of Fatigue Life of GH3039 Superalloy by Laser Shock Peening
title_sort improvement of fatigue life of gh3039 superalloy by laser shock peening
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2020-08-01
description In order to improve fatigue life of GH3039 superalloy, GH3039 superalloy sheets were treated by laser shock peening (LSP). The microstructure of GH3039 superalloy before and after LSP was characterized using an optical microscope, transmission electron microscope (TEM), and X-ray diffractometer. The fatigue life of the samples with and without LSP was investigated by fatigue experiments. Moreover, surface profile and residual stress were also examined. Experimental results indicated that the grains in the surface layer of the LSP sample were remarkably refined and reached the nanometer scale. The average surface roughness increased from 0.024 μm to 0.19 μm after LSP. The average fatigue life of the laser treated samples was 2.01 times larger than that of the untreated specimens. Additionally, mathematical statistical analysis confirms that LSP has a significant influence on the fatigue life of GH3039 superalloy. The improvement of fatigue life for the laser processed GH3039 superalloy was mainly attributed to compressive residual stress and grain refinement generated by LSP.
topic laser shock peening
GH3039 superalloy
microstructure
fatigue life
url https://www.mdpi.com/1996-1944/13/17/3849
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AT maozhongge improvementoffatiguelifeofgh3039superalloybylasershockpeening
AT yongkangzhang improvementoffatiguelifeofgh3039superalloybylasershockpeening
AT taimingwang improvementoffatiguelifeofgh3039superalloybylasershockpeening
AT wenzhou improvementoffatiguelifeofgh3039superalloybylasershockpeening
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