TY - JOUR
T1 - Study on the interfacial bonding behavior of dissimilar aluminum alloys via additive friction stir deposition
AU - Zhang, Mingtao
AU - Jiang, Tao
AU - Su, Yu
AU - Sun, Zhonggang
AU - Xu, Yaxin
AU - Li, Wenya
N1 - Publisher Copyright:
© 2025 Chinese Materials Research Society
PY - 2025
Y1 - 2025
N2 - Conventional fusion-based additive manufacturing methods for dissimilar aluminum alloys often face low efficiency and weak interfacial bonding. The rod-feeding-based additive friction stir deposition (R-AFSD) process improves this by achieving metallurgical bonding through recrystallization without melting the material. This work fills a study gap in multilayer deposition of dissimilar aluminum alloys, focusing on bonding mechanisms and optimizing interfacial properties critical for high-performance dissimilar aluminum alloys structures in aerospace applications. This work fabricated a three-layer deposition of 6061-T6, 2024-T6, and 7075-T6 alloys, characterizing material flow and interfacial microstructure using scanning electron microscopy (SEM) and electron backscattered diffraction (EBSD). Zn enrichment at the 7075/2024 interface resulted in an average grain size of 0.8 μm, enhancing interfacial strength. Shear tests showed that the 7075/2024 interface had the highest shear strength of 232 MPa, while the 6061/2024 interface exhibited a maximum shear strength of 155 MPa with greater plasticity. The multilayer structure of dissimilar aluminum alloys demonstrates superior performance by integrating the strengths of each alloy. The strategic placement of 6061 in the bottom layer provides corrosion resistance, while 2024 enhances fatigue resistance, and 7075 withstands high loads. This study offers novel insights into R-AFSD for dissimilar aluminum alloy deposition, with significant implications for aerospace applications.
AB - Conventional fusion-based additive manufacturing methods for dissimilar aluminum alloys often face low efficiency and weak interfacial bonding. The rod-feeding-based additive friction stir deposition (R-AFSD) process improves this by achieving metallurgical bonding through recrystallization without melting the material. This work fills a study gap in multilayer deposition of dissimilar aluminum alloys, focusing on bonding mechanisms and optimizing interfacial properties critical for high-performance dissimilar aluminum alloys structures in aerospace applications. This work fabricated a three-layer deposition of 6061-T6, 2024-T6, and 7075-T6 alloys, characterizing material flow and interfacial microstructure using scanning electron microscopy (SEM) and electron backscattered diffraction (EBSD). Zn enrichment at the 7075/2024 interface resulted in an average grain size of 0.8 μm, enhancing interfacial strength. Shear tests showed that the 7075/2024 interface had the highest shear strength of 232 MPa, while the 6061/2024 interface exhibited a maximum shear strength of 155 MPa with greater plasticity. The multilayer structure of dissimilar aluminum alloys demonstrates superior performance by integrating the strengths of each alloy. The strategic placement of 6061 in the bottom layer provides corrosion resistance, while 2024 enhances fatigue resistance, and 7075 withstands high loads. This study offers novel insights into R-AFSD for dissimilar aluminum alloy deposition, with significant implications for aerospace applications.
KW - Dissimilar aluminum alloy deposition
KW - Interface bonding strength
KW - Microstructure evolution
KW - Rod-feeding-based additive friction stir deposition
UR - http://www.scopus.com/inward/record.url?scp=86000529380&partnerID=8YFLogxK
U2 - 10.1016/j.pnsc.2025.02.008
DO - 10.1016/j.pnsc.2025.02.008
M3 - 文章
AN - SCOPUS:86000529380
SN - 1002-0071
JO - Progress in Natural Science: Materials International
JF - Progress in Natural Science: Materials International
ER -