High-integrity diffusion bonding of laser powder bed fused, forged, and rolled Ti-6Al-4V alloys

被引:0
作者
Jeon, Seoyeon [1 ]
Ha, Hyunjong [2 ]
Lee, Dong Jun [3 ]
Park, Hyeonil [3 ]
Kwon, Yong Nam [3 ]
Choi, Hyunjoo [1 ]
Sung, Hyokyung [1 ]
机构
[1] Kookmin Univ, Sch Mat Sci & Engn, Seoul 02707, South Korea
[2] Rebiality, Pyeongtaek 17926, Gyeonggi, South Korea
[3] Korea Inst Mat Sci, Mat Deformat Dept, Changwon Si 51508, Gyeongnam, South Korea
来源
JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T | 2025年 / 35卷
基金
新加坡国家研究基金会;
关键词
Ti-6Al-4V; Diffusion bonding; Laser powder bed fusion; Microstructure; Mechanical properties; TITANIUM; MICROSTRUCTURE;
D O I
10.1016/j.jmrt.2025.01.175
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Diffusion bonding of additively manufactured Ti-6Al-4V components with complex geometries to conventionally processed frames is a cost-effective approach for reducing the buy-to-fly ratio while minimizing deformation. This is the first study to investigate the diffusion bonding between laser powder bed fusion (LPBF)-manufactured and conventionally processed Ti-6Al-4V alloys at various temperatures, durations, and pressures. Herein, the diffusion bonding of forged, rolled, and LPBF-manufactured Ti-6Al-4V alloys were examined under specific bonding conditions: 900 degrees C for bonding durations of 1 and 2 h and pressures of 2 and 4 MPa. Extended bonding durations led to beta phase coarsening and thickened, elongated alpha ' laths in LPBFed materials, negatively impacting their mechanical properties. Optimal bonding was achieved at 900 degrees C for 2 h under 4 MPa, with bonding ratios exceeding 97%. Although LPBFed materials exhibited higher porosity than conventional alloys, which slightly reduced the bonding strength, microhardness and tensile testing revealed comparable bonding strengths. However, the LPBFed samples exhibited smaller elongation owing to the surface porosity. These findings suggest that diffusion bonding between LPBFed and conventional Ti-6Al-4V alloys can maintain mechanical integrity while reducing material waste, which presents a viable solution for aerospace component manufacturing.
引用
收藏
页码:2108 / 2118
页数:11
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