Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy

The service life of single crystal turbine blades,which serve as pivotal components in aero-engines,is intricately tied to their surface integrity. To fulfill performance standards, these blades typically undergo shot peening to meet for reinforcement. This study meticulously examines the impact of...

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Main Authors: GAI Pengtao, WU Yunhua, CAO Ziwen, WEI Dasheng, FU Xuesong
Format: Article
Language:zho
Published: Journal of Aeronautical Materials 2025-02-01
Series:Journal of Aeronautical Materials
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Online Access:http://jam.biam.ac.cn/article/doi/10.11868/j.issn.1005-5053.2024.000086
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author GAI Pengtao
WU Yunhua
CAO Ziwen
WEI Dasheng
FU Xuesong
author_facet GAI Pengtao
WU Yunhua
CAO Ziwen
WEI Dasheng
FU Xuesong
author_sort GAI Pengtao
collection DOAJ
description The service life of single crystal turbine blades,which serve as pivotal components in aero-engines,is intricately tied to their surface integrity. To fulfill performance standards, these blades typically undergo shot peening to meet for reinforcement. This study meticulously examines the impact of surface morphology and various surface integrity indicators—including roughness,near-surface microstructure, hardness, and residual stress—on DD6 single-crystal superalloy before and after undergoing shot peening treatments of varying intensities (0.15,0.2 mmA,and 0.25 mmA). Utilizing a surface profilometer,scanning electron microscope,microhardness tester,and stress tester, we comprehensively analyze these factors. The results show that shot peening diminishes the original machining marks on the DD6 superalloy’s surface,with surface roughness escalating from 0.507 μm at 0.15 mmA to 0.883 μm at 0.25 mmA. A gradient plastic severe deformation layer emerges near the surface,its depth progressively increasing from 45 μm at 0.15 mmA to 98 μm at 0.25 mmA. Furthermore,the surface hardness value rises steadily, from 490HV in the original specimen to 738HV at 0.25 mmA,with the hardened layer’s depth also augmenting,from 50 μm initially to 260 μm at 0.25 mmA. Notably,the alloy attains its peak residual compressive stress of approximately –821.2 MPa on the surface when subjected to a blasting intensity of 0.2 mmA.
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spelling doaj-art-de607b9dde224393a645b0cd1b1412522025-02-12T09:22:41ZzhoJournal of Aeronautical MaterialsJournal of Aeronautical Materials1005-50532025-02-01451536110.11868/j.issn.1005-5053.2024.000086a2024-0086Effect of shot peening intensities on surface integrity of DD6 single crystal superalloyGAI Pengtao0WU Yunhua1CAO Ziwen2WEI Dasheng3FU Xuesong4AVIC Manufacturing Technology Institute,Beijing 100024,ChinaSchool of Materials Science and Engineering,Dalian University of Technology,Dalian 116024,Liaoning,ChinaAVIC Manufacturing Technology Institute,Beijing 100024,ChinaSchool of Energy and Power Engineering,Beihang University,Beijing 100191,ChinaSchool of Materials Science and Engineering,Dalian University of Technology,Dalian 116024,Liaoning,ChinaThe service life of single crystal turbine blades,which serve as pivotal components in aero-engines,is intricately tied to their surface integrity. To fulfill performance standards, these blades typically undergo shot peening to meet for reinforcement. This study meticulously examines the impact of surface morphology and various surface integrity indicators—including roughness,near-surface microstructure, hardness, and residual stress—on DD6 single-crystal superalloy before and after undergoing shot peening treatments of varying intensities (0.15,0.2 mmA,and 0.25 mmA). Utilizing a surface profilometer,scanning electron microscope,microhardness tester,and stress tester, we comprehensively analyze these factors. The results show that shot peening diminishes the original machining marks on the DD6 superalloy’s surface,with surface roughness escalating from 0.507 μm at 0.15 mmA to 0.883 μm at 0.25 mmA. A gradient plastic severe deformation layer emerges near the surface,its depth progressively increasing from 45 μm at 0.15 mmA to 98 μm at 0.25 mmA. Furthermore,the surface hardness value rises steadily, from 490HV in the original specimen to 738HV at 0.25 mmA,with the hardened layer’s depth also augmenting,from 50 μm initially to 260 μm at 0.25 mmA. Notably,the alloy attains its peak residual compressive stress of approximately –821.2 MPa on the surface when subjected to a blasting intensity of 0.2 mmA.http://jam.biam.ac.cn/article/doi/10.11868/j.issn.1005-5053.2024.000086dd6single crystal superalloyshot peeningsurface integrityresidual stressplastic deformation
spellingShingle GAI Pengtao
WU Yunhua
CAO Ziwen
WEI Dasheng
FU Xuesong
Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
Journal of Aeronautical Materials
dd6single crystal superalloy
shot peening
surface integrity
residual stress
plastic deformation
title Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
title_full Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
title_fullStr Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
title_full_unstemmed Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
title_short Effect of shot peening intensities on surface integrity of DD6 single crystal superalloy
title_sort effect of shot peening intensities on surface integrity of dd6 single crystal superalloy
topic dd6single crystal superalloy
shot peening
surface integrity
residual stress
plastic deformation
url http://jam.biam.ac.cn/article/doi/10.11868/j.issn.1005-5053.2024.000086
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AT wuyunhua effectofshotpeeningintensitiesonsurfaceintegrityofdd6singlecrystalsuperalloy
AT caoziwen effectofshotpeeningintensitiesonsurfaceintegrityofdd6singlecrystalsuperalloy
AT weidasheng effectofshotpeeningintensitiesonsurfaceintegrityofdd6singlecrystalsuperalloy
AT fuxuesong effectofshotpeeningintensitiesonsurfaceintegrityofdd6singlecrystalsuperalloy