Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy

According to the actual size parameters, the finite element model (FEM) of friction stir welding (FSW) was established, and the FEM was updated by experiments. The FSW of the 2A14-T6 high-strength aluminum alloy was simulated under a reasonable welding process parameter range, and the welding proces...

Full description

Bibliographic Details
Main Authors: Haitao Luo, Tingke Wu, Jia Fu, Wei Wang, Ning Chen, Haonan Wang
Format: Article
Language:English
Published: MDPI AG 2019-02-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/12/3/480
id doaj-2e5e03a415fa498c84dcda8be3d1fa46
record_format Article
spelling doaj-2e5e03a415fa498c84dcda8be3d1fa462020-11-25T01:13:40ZengMDPI AGMaterials1996-19442019-02-0112348010.3390/ma12030480ma12030480Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum AlloyHaitao Luo0Tingke Wu1Jia Fu2Wei Wang3Ning Chen4Haonan Wang5Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaShenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaShenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaShenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaShenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaShenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, ChinaAccording to the actual size parameters, the finite element model (FEM) of friction stir welding (FSW) was established, and the FEM was updated by experiments. The FSW of the 2A14-T6 high-strength aluminum alloy was simulated under a reasonable welding process parameter range, and the welding process parameters with good simulation effect were determined. The test was carried out under the same parameters, and the axial force of the FSW tool and temperature of the workpiece measuring point were collected. The comparison between the simulated data and the experimental data is reasonable, indicating the correctness of the FEM. The microstructure analysis of the welded joint shows that the grain size in the upper part of the weld nugget was smaller than that in the middle and lower parts, and there are obvious boundaries of grain size in each region of the joint. The hardness of the joint in the upper layer is higher than that in the middle and lower layers, and the minimum Vickers hardness value of the joint appears near the interface between the thermo-mechanically affected zone and the heat-affected zone on both sides of the weld. Tensile testing shows that the strength coefficient of the joint reaches 82.5% under this process parameter, and the sample breaks at the intersection of the material flow during stretching. After analyzing the final mechanical properties of the joint, we found that a degree of aerospace application can be achieved. Under this parameter, the welding test was carried out on the top cover of the rocket fuel tank. Firstly, melon valve welding, which is relatively difficult in welding conditions, was carried out, and a high-quality joint with good surface and no defects was obtained.https://www.mdpi.com/1996-1944/12/3/480friction stir welding (FSW)finite element model (FEM)microstructuremechanical propertiesaerospace application
collection DOAJ
language English
format Article
sources DOAJ
author Haitao Luo
Tingke Wu
Jia Fu
Wei Wang
Ning Chen
Haonan Wang
spellingShingle Haitao Luo
Tingke Wu
Jia Fu
Wei Wang
Ning Chen
Haonan Wang
Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
Materials
friction stir welding (FSW)
finite element model (FEM)
microstructure
mechanical properties
aerospace application
author_facet Haitao Luo
Tingke Wu
Jia Fu
Wei Wang
Ning Chen
Haonan Wang
author_sort Haitao Luo
title Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
title_short Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
title_full Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
title_fullStr Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
title_full_unstemmed Welding Characteristics Analysis and Application on Spacecraft of Friction Stir Welded 2A14-T6 Aluminum Alloy
title_sort welding characteristics analysis and application on spacecraft of friction stir welded 2a14-t6 aluminum alloy
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2019-02-01
description According to the actual size parameters, the finite element model (FEM) of friction stir welding (FSW) was established, and the FEM was updated by experiments. The FSW of the 2A14-T6 high-strength aluminum alloy was simulated under a reasonable welding process parameter range, and the welding process parameters with good simulation effect were determined. The test was carried out under the same parameters, and the axial force of the FSW tool and temperature of the workpiece measuring point were collected. The comparison between the simulated data and the experimental data is reasonable, indicating the correctness of the FEM. The microstructure analysis of the welded joint shows that the grain size in the upper part of the weld nugget was smaller than that in the middle and lower parts, and there are obvious boundaries of grain size in each region of the joint. The hardness of the joint in the upper layer is higher than that in the middle and lower layers, and the minimum Vickers hardness value of the joint appears near the interface between the thermo-mechanically affected zone and the heat-affected zone on both sides of the weld. Tensile testing shows that the strength coefficient of the joint reaches 82.5% under this process parameter, and the sample breaks at the intersection of the material flow during stretching. After analyzing the final mechanical properties of the joint, we found that a degree of aerospace application can be achieved. Under this parameter, the welding test was carried out on the top cover of the rocket fuel tank. Firstly, melon valve welding, which is relatively difficult in welding conditions, was carried out, and a high-quality joint with good surface and no defects was obtained.
topic friction stir welding (FSW)
finite element model (FEM)
microstructure
mechanical properties
aerospace application
url https://www.mdpi.com/1996-1944/12/3/480
work_keys_str_mv AT haitaoluo weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
AT tingkewu weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
AT jiafu weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
AT weiwang weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
AT ningchen weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
AT haonanwang weldingcharacteristicsanalysisandapplicationonspacecraftoffrictionstirwelded2a14t6aluminumalloy
_version_ 1725160732915400704