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Open Access

Improvement of rotating laser Al/steel lap welded joints via Cu interlayer: Microstructure and mechanical properties

Jiang YUaTao YANGa( )Bo LIa,bYuan ZHUANGbLin LIaYuan WANGb
Ningbo Institute of Materials Technology and Engineering, Chinese Academy of Sciences, Ningbo 315201, China
Key Laboratory of Advanced Technologies of Materials, Ministry of Education, Southwest Jiaotong University, Chengdu 610031, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The joining of Al/steel dissimilar metals has emerged as a critical challenge in automotive lightweight design. The sound Al/steel lap configuration joints were achieved via the new welding technology, i.e., the rotating laser welding method, with the inserted Cu foil interlayer. The interfacial temperature fields of the obtained joints were accurately predicted by finite element simulation. The results indicate that the heat concentration effect at the interface was generated via the rotating laser, and the temperature difference of the laser direct irradiation area, the middle area, and the welding toe region was controlled to 100 °C. Besides, the inserted Cu interlayer significantly optimized interfacial metallurgical reactions, resulting in the formation of a uniform composite interface layer consisting of θ-(Fe, Cu)4Al13, α-Al, and Al2Cu. The thermodynamic calculations elucidated the sequential phase evolution: the Al-Fe binary system was generated first, and then followed by the Al-Cu binary system in the welding process. The final joint line load was enhanced with the inserted rotating laser. When the rotating diameter was 1 mm and the thickness of Cu interlayer was 10 μm, the joint line load reached the maximum value of 297 N/mm.

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Chinese Journal of Aeronautics

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Cite this article:
YU J, YANG T, LI B, et al. Improvement of rotating laser Al/steel lap welded joints via Cu interlayer: Microstructure and mechanical properties. Chinese Journal of Aeronautics, 2025, 38(12). https://doi.org/10.1016/j.cja.2025.103834

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Received: 26 April 2025
Revised: 20 June 2025
Accepted: 27 July 2025
Published: 18 September 2025
© 2025 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).