4.5 Article

Prediction of the Interface Deformation of Ultrasonic Spot Welding of Multilayer Metal Foils Considering Energy Gradient

Publisher

ASME
DOI: 10.1115/1.4053924

Keywords

ultrasonic spot welding; multilayer; finite element model; energy gradient; computer aided design; CAM; CAE; modeling and simulation; welding and joining

Funding

  1. National Natural Science Foundation of China [51875352]

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In this study, an efficient and accurate finite element model was proposed to simulate the ultrasonic spot welding process of multi-layer Cu or Al tabs. By introducing the interface heat flux, the heat generation caused by friction was effectively equivalent. The validated model was then applied to simulate the welding process of different layers of copper and aluminum foils, revealing that the heat generation concentrated in the middle interfaces and was related to welding parameters, tip size, and specimen structure.
The ultrasonic spot welding (USW) is widely used in the joining of multilayer Cu or Al tabs in the lithium-ion battery. Due to the high-frequency vibration of the sonotrode and various deformation in each interface, the friction behavior is complex which makes it difficult to simulate the welding process of multilayer specimens. In this paper, an efficient and accurate finite element model (FEM) was proposed via introducing the interface heat flux to equivalent the heat generation by the friction. The total heat flux was determined by the heat transfer analysis and the proportion of each interface was determined based on the analysis of the friction behavior. Then, the FEM was validated by comparing the simulated temperature and deformation with experimental results. Finally, the FEM was applied to simulate the USW process of four, five, and ten layers of copper and aluminum foils in order to characterize the gradient of the ultrasonic energy. It was found that the heat generation concentrated in middle interfaces was 65% of the total in the welding of four-layer copper foils. The heat generation was mainly related to the welding parameters and the proportion was related to the size of tips and the structure of specimens. The plastic strain varied in specimens because of the gradient of the input energy. It was most obvious in the welding of 10-layer aluminum foils that the maximum equivalent plastic strain (PEEQ) in the fifth interface was 92.9% smaller than the top interface.

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