2.1 Experimental setup
The fiber laser welding system featured (independently controllable) core and ring beams output by a dual-core optical fiber. Table 1 lists the specifications of laser system and Figure 1 presents the experimental setup and the schematics of beam splits. To optimize laser heat input, the two beams were individually controlled and Figure 2 presents welding specimens and a schematic of the beam delivery system.
Table 1 Specification of laser system
Laser type
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FL8000 - ARM (Fiber laser), Coherent Inc.
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Wavelength
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1.07µm
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Max. power
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Center : 4kW, Ring : 4kW
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Beam modulation
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Max. 5 kHz
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Optical fiber dia.
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Center: 70µm, Ring : 180µm
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Scanner
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300 x 200mm ,Fd : 560mm
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Independent control of the core and ring beams allowed welding to proceed in three stages: pre-heating, keyhole formation, and post-heating. During pre-heating, the surface is heated to below the melting point to increase laser energy absorption; this assists melting stability by removing foreign substances. During keyhole formation, a keyhole and a molten pool are formed by the ring and core beams respectively which yield a deep, narrow weld bead. Finally, post-heating shortens the length of the keyhole and reduces the molten pool; ultimately, both disappear, with maintained weld stability.
We used 0.4 mm thick sheets of the Al (Al6061) and Cu (C1020P) alloys typically employed to fabricate EV battery packs. The Al-Si-Mg-based alloy contained about 0.4 to 0.8% silicon (Si) and about 0.8 to 1.2% magnesium (Mg). We employed an oxygen-free copper C1020P-1/2H alloy. Table 2 lists detailed chemical compositions. The sheets were cut 50 mm in width and the Al plate was placed on top and the Cu for the welding. The materials were overlapped by 45 mm, and 40 mm sections were welded across the width.
Table 2 Chemical composition of Al, Cu alloy (wt. %)
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Mat’l
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Cu
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Si
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Mg
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Zn
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Mn
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Cr
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Fe
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Ti
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Al
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Al6061
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0.4
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0.8
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< 1.2
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< 0.25
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< 0.10
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< 0.35
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< 0.70
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< 0.15
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Bal.
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C1020P
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Cu
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O2
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> 99.56
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< 10 ppm
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To investigate welding characteristics, bead-on-plate (BOP) tests were performed for both Al and Cu. To determine the laser outputs required for the full penetration of the materials, the output was varied with the welding speed and the focal position was held constant.
2.2 BOP and lap joint welding conditions
Because the properties of the two materials differed, it was necessary to optimize welding [19]. The initial welding conditions were established by fixing the focal position and welding speed and then varying the laser output. In general, partial penetration welding is required when welding the tabs and busbars of lithium-ion batteries. Given the high reflectivity of Al and Cu alloys, the laser beam was inclined by 8ºwith respect to the direction of travel, to ensure that the reflected beam did not attain the laser. Lap joint welding was performed in the manner described above, using specimens with dimensions of 100 x 50 x 0.4 mm. The Al specimens were on top and the Cu specimens on the bottom. Welding was performed over a length of about 40 mm. The laser light source was remotely irradiated (using a galvanometer scanner) without a shielding gas supply.
2.3 Computer simulation
To explore the heat distributions when welding Al and Cu, computer simulations were performed with reference to the experimental conditions. Such simulations effectively track weld heat distribution and deformation based on the temperature distribution [8]. When welding dissimilar materials, the optimal heat input can be predicted by simulation to explore how intermetallic compounds (IMCs) with various physical properties affect weld strength and soundness. During typical welding process, keyholes are generated, and heat thus moves not only via conduction but also via convection. We used the heat transfer module of COMSOL Multiphysics (ver. 5.3a) for numerical analysis. The simulations were verified by comparing the simulated and actual temperature distributions (the latter were assessed using a thermocouple and an infrared camera).
In the simulations, the Al and Cu plates were of the same thicknesses as those of the experiments; the simulation domain was 40 mm in width and 100 mm in length to allow adequate thermal diffusion. The governing three-dimensional heat transfer equation for the entire domain can be expressed as Eq. (1), and the natural convection conditions as Eq. (2):
where Eq. (2) deals with conductive or convective heat transfer through surrounding bodies. In Eq. (2), ρ is the density of the polymer, Cp is the specific heat capacity at constant stress, T is the absolute temperature, utrans is the velocity vector of translational motion, k is the thermal conductivity, and q is the heat flux of conduction, qr is the heat flux of radiation, α is the coefficient of thermal expansion, S is the second Piola-Kirchhoff stress tensor, and Q contains the additional laser heat sources of Eq. (3) or (4).
To simulate the core beam, a three-dimensional (3D) Gaussian laser beam was used, as expressed in Eq. (3). The ring beam can be expressed as Eq. (4). The outer and inner diameters of the ring beam were established using the Dirac delta function and the “rectangle function” of COMSOL. Figure 3 presents the 3D models of laser beam intensity distributions for each case.
In Eq. (3), Q0 is the peak power, Rc is the reflectance, σx and σy are the beam waists in the x and y directions, and Ac is the skin depth/absorption layer thickness. As shown in Eq. (3), the irradiating laser beam was assumed to have a two-dimensional ellipsoidal distribution and a skin depth of Ac in the z direction.
Skin depth can be analytically calculated for any metal. The reflectance (Rc) is important, and was experimentally determined by integrating the sphere. To track the temperature distribution, a temperature probe was placed 0.5 mm distant from the weld line, and then moved to the upper, middle, and lower surfaces in the direction of thickness.
2.4 Weld tests
To test weld strengths, we performed cross-sectional analyses and mechanical strength tests to assess surface cracks and voids. For weld analysis, the specimens were cut, polished, etched, and observed under a microscope. The Al etching solution was hydrochloric acid 75 mL + nitric acid 25 mL; the Cu etching solution was nitric acid 30 mL + distilled water 70 mL.
Tensile tests were performed using a 1-tonne-class, small tensile tester (AGS-X; Shimadzu) of grip size about 22 mm. The welding test pieces were cut from the overall test pieces (25–50 mm in width and laser-welded for about 20 mm). Figure 4 presents a photograph of the tensile test system and the specimen specifications.