Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming
A thermal mechanical coupling numerical model of 7050 aluminium alloy was established using the Hansel-Spittel constitutive model. The stress state of the samples during quenching and cold deformation was analyzed using the finite element simulation technology at first, which is in good accordance w...
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Format: | Article |
Language: | zho |
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Journal of Materials Engineering
2021-08-01
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Series: | Cailiao gongcheng |
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Online Access: | http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2021.000242 |
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author | WANG Hao XIAO Na-min LI Hui-qu WANG Xiao |
author_facet | WANG Hao XIAO Na-min LI Hui-qu WANG Xiao |
author_sort | WANG Hao |
collection | DOAJ |
description | A thermal mechanical coupling numerical model of 7050 aluminium alloy was established using the Hansel-Spittel constitutive model. The stress state of the samples during quenching and cold deformation was analyzed using the finite element simulation technology at first, which is in good accordance with the measured result by ultrasonic test. Then, residual stress evolution rule during heat treatment and cold deformation of an aluminium component with rib structure was studied and ultrasonic residual stress inspection and matching deformation verification were carried out on the structural component. The results show that residual stress after quenching is in the state of external compression and internal tension. The reduction degree of quenching induced residual stress by different cold deformation methods is obviously different. For cold compression, when deformation exceeds 2%, compression on the web obviously improves stress state of the whole web region while compression on the lib has relatively less improvement. For cold stretching, 3% deformation can effectively improve the stress uniformity for both web region and lib region. After cold stretching, the distortion during machining can be obviously improved. |
first_indexed | 2024-04-11T02:55:32Z |
format | Article |
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institution | Directory Open Access Journal |
issn | 1001-4381 1001-4381 |
language | zho |
last_indexed | 2024-04-11T02:55:32Z |
publishDate | 2021-08-01 |
publisher | Journal of Materials Engineering |
record_format | Article |
series | Cailiao gongcheng |
spelling | doaj.art-aa4c6d191f9b48728601ff69921937e12023-01-02T15:24:08ZzhoJournal of Materials EngineeringCailiao gongcheng1001-43811001-43812021-08-01498728010.11868/j.issn.1001-4381.2021.00024220210807Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold formingWANG Hao0XIAO Na-min1LI Hui-qu2WANG Xiao3AECC Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaAECC Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaAECC Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaAECC Beijing Institute of Aeronautical Materials, Beijing 100095, ChinaA thermal mechanical coupling numerical model of 7050 aluminium alloy was established using the Hansel-Spittel constitutive model. The stress state of the samples during quenching and cold deformation was analyzed using the finite element simulation technology at first, which is in good accordance with the measured result by ultrasonic test. Then, residual stress evolution rule during heat treatment and cold deformation of an aluminium component with rib structure was studied and ultrasonic residual stress inspection and matching deformation verification were carried out on the structural component. The results show that residual stress after quenching is in the state of external compression and internal tension. The reduction degree of quenching induced residual stress by different cold deformation methods is obviously different. For cold compression, when deformation exceeds 2%, compression on the web obviously improves stress state of the whole web region while compression on the lib has relatively less improvement. For cold stretching, 3% deformation can effectively improve the stress uniformity for both web region and lib region. After cold stretching, the distortion during machining can be obviously improved.http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2021.0002427050 aluminium alloyresidual stresscold deformationthermal mechanical coupling simulation |
spellingShingle | WANG Hao XIAO Na-min LI Hui-qu WANG Xiao Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming Cailiao gongcheng 7050 aluminium alloy residual stress cold deformation thermal mechanical coupling simulation |
title | Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
title_full | Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
title_fullStr | Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
title_full_unstemmed | Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
title_short | Modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
title_sort | modeling of residual stress evolution of 7050 aluminium alloy component during heat treatment and cold forming |
topic | 7050 aluminium alloy residual stress cold deformation thermal mechanical coupling simulation |
url | http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2021.000242 |
work_keys_str_mv | AT wanghao modelingofresidualstressevolutionof7050aluminiumalloycomponentduringheattreatmentandcoldforming AT xiaonamin modelingofresidualstressevolutionof7050aluminiumalloycomponentduringheattreatmentandcoldforming AT lihuiqu modelingofresidualstressevolutionof7050aluminiumalloycomponentduringheattreatmentandcoldforming AT wangxiao modelingofresidualstressevolutionof7050aluminiumalloycomponentduringheattreatmentandcoldforming |