Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate
Explosively welded layered materials made of (a) an AA2519 aluminum alloy (AlCuMgMn + ZrSc), (b) titanium alloy Ti6Al4V and (c) an intermediate layer composed of a thin aluminum alloyed AA1050 layer are considered herein. This study presents test results connected to measurement science including mi...
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| Format: | Article |
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MDPI AG
2020-09-01
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| Series: | Materials |
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| Online Access: | https://www.mdpi.com/1996-1944/13/19/4348 |
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| author | Ireneusz Szachogluchowicz Lucjan Sniezek Tomasz Slezak Janusz Kluczyński Krzysztof Grzelak Janusz Torzewski Teresa Fras |
| author_facet | Ireneusz Szachogluchowicz Lucjan Sniezek Tomasz Slezak Janusz Kluczyński Krzysztof Grzelak Janusz Torzewski Teresa Fras |
| author_sort | Ireneusz Szachogluchowicz |
| collection | DOAJ |
| description | Explosively welded layered materials made of (a) an AA2519 aluminum alloy (AlCuMgMn + ZrSc), (b) titanium alloy Ti6Al4V and (c) an intermediate layer composed of a thin aluminum alloyed AA1050 layer are considered herein. This study presents test results connected to measurement science including microstructural observations of the material combined with the explosive method, and a basic analysis of the strength properties based on microhardness and tensile tests. Owing to the joint’s special manufacturing conditions, the laminate was subjected to deformation measurements with the digital image correlation (DIC) method. The research was supplemented by the residual stress measurements with the sin2ψ X-ray method based on the diffraction–reflection analysis that was verified by the bore trepanation method. |
| first_indexed | 2024-03-10T15:56:56Z |
| format | Article |
| id | doaj.art-8bbd829c071f42b9a97e603ae76430c1 |
| institution | Directory Open Access Journal |
| issn | 1996-1944 |
| language | English |
| last_indexed | 2024-03-10T15:56:56Z |
| publishDate | 2020-09-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Materials |
| spelling | doaj.art-8bbd829c071f42b9a97e603ae76430c12023-11-20T15:37:03ZengMDPI AGMaterials1996-19442020-09-011319434810.3390/ma13194348Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded LaminateIreneusz Szachogluchowicz0Lucjan Sniezek1Tomasz Slezak2Janusz Kluczyński3Krzysztof Grzelak4Janusz Torzewski5Teresa Fras6Institute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandInstitute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandInstitute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandInstitute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandInstitute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandInstitute of Robots & Machine Design, Faculty of Mechanical Engineering, Military University of Technology, 2 Gen. S. Kaliskiego St., 00-908 Warsaw 46, PolandFrench-German Research Institute of Saint-Louis (ISL), 5 rue du Général Cassagnou, 68301 Saint-Louis, FranceExplosively welded layered materials made of (a) an AA2519 aluminum alloy (AlCuMgMn + ZrSc), (b) titanium alloy Ti6Al4V and (c) an intermediate layer composed of a thin aluminum alloyed AA1050 layer are considered herein. This study presents test results connected to measurement science including microstructural observations of the material combined with the explosive method, and a basic analysis of the strength properties based on microhardness and tensile tests. Owing to the joint’s special manufacturing conditions, the laminate was subjected to deformation measurements with the digital image correlation (DIC) method. The research was supplemented by the residual stress measurements with the sin2ψ X-ray method based on the diffraction–reflection analysis that was verified by the bore trepanation method.https://www.mdpi.com/1996-1944/13/19/4348deformation analysisresidual stresses measurementAA2519Ti6Al4Vexplosive weldinglayered laminate |
| spellingShingle | Ireneusz Szachogluchowicz Lucjan Sniezek Tomasz Slezak Janusz Kluczyński Krzysztof Grzelak Janusz Torzewski Teresa Fras Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate Materials deformation analysis residual stresses measurement AA2519 Ti6Al4V explosive welding layered laminate |
| title | Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate |
| title_full | Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate |
| title_fullStr | Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate |
| title_full_unstemmed | Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate |
| title_short | Mechanical Properties Analysis of the AA2519-AA1050-Ti6Al4V Explosive Welded Laminate |
| title_sort | mechanical properties analysis of the aa2519 aa1050 ti6al4v explosive welded laminate |
| topic | deformation analysis residual stresses measurement AA2519 Ti6Al4V explosive welding layered laminate |
| url | https://www.mdpi.com/1996-1944/13/19/4348 |
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