Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material

The study presents an analysis of the cracking process of explosive welded layered material AA2519–AA1050–Ti6Al4V (Al–Ti laminate) at ambient (293 K) and reduced (223 and 77 K) temperatures. Fracture toughness tests were conducted for specimens made of base materials and Al–Ti laminate. As a result...

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Main Authors: Dariusz Boroński, Ihor Dzioba, Maciej Kotyk, Aleksandra Krampikowska, Robert Pała
Format: Article
Language:English
Published: MDPI AG 2020-05-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/13/10/2226
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spelling doaj-ed7878d0f1474040a8eab3f5dfbed4b22020-11-25T02:20:45ZengMDPI AGMaterials1996-19442020-05-01132226222610.3390/ma13102226Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered MaterialDariusz Boroński0Ihor Dzioba1Maciej Kotyk2Aleksandra Krampikowska3Robert Pała4Faculty of Mechanical Engineering, UTP University of Science and Technology, 85-796 Bydgoszcz, PolandFaculty of Mechatronics and Mechanical Engineering, Kielce University of Technology, 25-314 Kielce, PolandFaculty of Mechanical Engineering, UTP University of Science and Technology, 85-796 Bydgoszcz, PolandFaculty of Civil Engineering and Architecture, Kielce University of Technology, 25-314 Kielce, PolandFaculty of Mechatronics and Mechanical Engineering, Kielce University of Technology, 25-314 Kielce, PolandThe study presents an analysis of the cracking process of explosive welded layered material AA2519–AA1050–Ti6Al4V (Al–Ti laminate) at ambient (293 K) and reduced (223 and 77 K) temperatures. Fracture toughness tests were conducted for specimens made of base materials and Al–Ti laminate. As a result of loading, delamination cracking occurred in the bonding layer of specimens made from Al–Ti laminate. To define the crack mechanisms that occur at the tested temperatures, a fracture analysis was made using a scanning electron microscope. Moreover, acoustic emission (AE) signals were recorded while loading. AE signals were segregated to link their groups with respective cracking process mechanisms. Numerical models of the tested specimens were developed, taking into account the complexity of the laminate structure and the ambiguity of the cracking process. A load simulation using the finite element method FEM allowed calculating stress distributions in the local area in the crack tip of the Al–Ti laminate specimens, which enabled the explanation of significant material cracking process development aspects. Results analysis showed an influence of interlayer delamination crack growth on the process of the Al–Ti laminate specimen cracking and the level of K<sub>Q</sub> characteristics at different temperatures.https://www.mdpi.com/1996-1944/13/10/2226layered materialfracture processexperimental analysisdelaminationreduced temperatures
collection DOAJ
language English
format Article
sources DOAJ
author Dariusz Boroński
Ihor Dzioba
Maciej Kotyk
Aleksandra Krampikowska
Robert Pała
spellingShingle Dariusz Boroński
Ihor Dzioba
Maciej Kotyk
Aleksandra Krampikowska
Robert Pała
Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
Materials
layered material
fracture process
experimental analysis
delamination
reduced temperatures
author_facet Dariusz Boroński
Ihor Dzioba
Maciej Kotyk
Aleksandra Krampikowska
Robert Pała
author_sort Dariusz Boroński
title Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
title_short Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
title_full Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
title_fullStr Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
title_full_unstemmed Investigation of the Fracture Process of Explosively Welded AA2519–AA1050–Ti6Al4V Layered Material
title_sort investigation of the fracture process of explosively welded aa2519–aa1050–ti6al4v layered material
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2020-05-01
description The study presents an analysis of the cracking process of explosive welded layered material AA2519–AA1050–Ti6Al4V (Al–Ti laminate) at ambient (293 K) and reduced (223 and 77 K) temperatures. Fracture toughness tests were conducted for specimens made of base materials and Al–Ti laminate. As a result of loading, delamination cracking occurred in the bonding layer of specimens made from Al–Ti laminate. To define the crack mechanisms that occur at the tested temperatures, a fracture analysis was made using a scanning electron microscope. Moreover, acoustic emission (AE) signals were recorded while loading. AE signals were segregated to link their groups with respective cracking process mechanisms. Numerical models of the tested specimens were developed, taking into account the complexity of the laminate structure and the ambiguity of the cracking process. A load simulation using the finite element method FEM allowed calculating stress distributions in the local area in the crack tip of the Al–Ti laminate specimens, which enabled the explanation of significant material cracking process development aspects. Results analysis showed an influence of interlayer delamination crack growth on the process of the Al–Ti laminate specimen cracking and the level of K<sub>Q</sub> characteristics at different temperatures.
topic layered material
fracture process
experimental analysis
delamination
reduced temperatures
url https://www.mdpi.com/1996-1944/13/10/2226
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