One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets

A one-step hybrid bending/diffusion bonding process (HB/DBP) was developed for application to Ti-6Al-4V sheets to effectively improve buy-to-fly (BTF) ratio of aircraft parts, integrating sequential diffusion bonding followed by a bending process. The resulting bonding characteristics of these titan...

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Main Authors: Kang Hyun Kim, Hyeonil Park, Dong Jun Lee, Yong Nam Kwon, Namhyun Kang, Jong-Hwa Hong
Format: Article
Language:English
Published: MDPI AG 2023-06-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/16/13/4516
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author Kang Hyun Kim
Hyeonil Park
Dong Jun Lee
Yong Nam Kwon
Namhyun Kang
Jong-Hwa Hong
author_facet Kang Hyun Kim
Hyeonil Park
Dong Jun Lee
Yong Nam Kwon
Namhyun Kang
Jong-Hwa Hong
author_sort Kang Hyun Kim
collection DOAJ
description A one-step hybrid bending/diffusion bonding process (HB/DBP) was developed for application to Ti-6Al-4V sheets to effectively improve buy-to-fly (BTF) ratio of aircraft parts, integrating sequential diffusion bonding followed by a bending process. The resulting bonding characteristics of these titanium alloy sheets were analyzed. Microstructural analysis and mechanical lap shear tests were performed to estimate the bonding quality. Additionally, bonding ratio, thickness strain, and shear strength were evaluated in relation to pressure under increasing temperature. When the applied pressure was lower than 0.5 MPa, early failure occurred at the joint of the specimens. However, when high pressure was applied, early failure occurred near the joint. To discuss the phenomenon, time-dependent viscoplastic material properties were characterized, and a numerical simulation analysis was performed. Viscoplastic deformation was observed around the bending area, which caused weakness around the bond under high-pressure conditions. A prototype of a Y-shaped heat shield was manufactured and the buy-to-fly ratio was effectively improved using the newly developed process. This study demonstrates the potential of applying the developed process for producing aircraft parts and the importance of viscoplastic behavior for the analysis of final product reliability.
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spelling doaj.art-74f91b5a7a9a42afbe4e5a268cbef9e32023-11-18T16:55:52ZengMDPI AGMaterials1996-19442023-06-011613451610.3390/ma16134516One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy SheetsKang Hyun Kim0Hyeonil Park1Dong Jun Lee2Yong Nam Kwon3Namhyun Kang4Jong-Hwa Hong5Aerospace Materials Center, Korea Institute of Materials Science, 797 Changwon-daero, Changwon 51508, Republic of KoreaAerospace Materials Center, Korea Institute of Materials Science, 797 Changwon-daero, Changwon 51508, Republic of KoreaAerospace Materials Center, Korea Institute of Materials Science, 797 Changwon-daero, Changwon 51508, Republic of KoreaAerospace Materials Center, Korea Institute of Materials Science, 797 Changwon-daero, Changwon 51508, Republic of KoreaDepartment of Materials Science and Engineering, Pusan National University, 2 Busandaehak-ro 63beon-gil, Busan 46241, Republic of KoreaAerospace Materials Center, Korea Institute of Materials Science, 797 Changwon-daero, Changwon 51508, Republic of KoreaA one-step hybrid bending/diffusion bonding process (HB/DBP) was developed for application to Ti-6Al-4V sheets to effectively improve buy-to-fly (BTF) ratio of aircraft parts, integrating sequential diffusion bonding followed by a bending process. The resulting bonding characteristics of these titanium alloy sheets were analyzed. Microstructural analysis and mechanical lap shear tests were performed to estimate the bonding quality. Additionally, bonding ratio, thickness strain, and shear strength were evaluated in relation to pressure under increasing temperature. When the applied pressure was lower than 0.5 MPa, early failure occurred at the joint of the specimens. However, when high pressure was applied, early failure occurred near the joint. To discuss the phenomenon, time-dependent viscoplastic material properties were characterized, and a numerical simulation analysis was performed. Viscoplastic deformation was observed around the bending area, which caused weakness around the bond under high-pressure conditions. A prototype of a Y-shaped heat shield was manufactured and the buy-to-fly ratio was effectively improved using the newly developed process. This study demonstrates the potential of applying the developed process for producing aircraft parts and the importance of viscoplastic behavior for the analysis of final product reliability.https://www.mdpi.com/1996-1944/16/13/4516one-step hybrid bending/diffusion bonding processtitanium alloy sheetsnumerical simulationviscoplasticityaircraft parts
spellingShingle Kang Hyun Kim
Hyeonil Park
Dong Jun Lee
Yong Nam Kwon
Namhyun Kang
Jong-Hwa Hong
One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
Materials
one-step hybrid bending/diffusion bonding process
titanium alloy sheets
numerical simulation
viscoplasticity
aircraft parts
title One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
title_full One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
title_fullStr One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
title_full_unstemmed One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
title_short One-Step Hybrid Bending/Diffusion Bonding Process and Analysis of the Bonding Characteristics of Titanium Alloy Sheets
title_sort one step hybrid bending diffusion bonding process and analysis of the bonding characteristics of titanium alloy sheets
topic one-step hybrid bending/diffusion bonding process
titanium alloy sheets
numerical simulation
viscoplasticity
aircraft parts
url https://www.mdpi.com/1996-1944/16/13/4516
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