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Engineering Science in
            Additive Manufacturing                                             EST manipulates structure of Ti-6Al-4V/Cu



            strength of copper-based composites without causing a   However, no systematic studies have been reported
            significant decrease in electrical conductivity. 13-15  on the microstructural evolution and texture effects of
              LMD enhances interfacial bond strength by promoting   Ti-6Al-4V/Cu-Cr-Zr interfaces fabricated by LMD using
            mixed diffusion of copper and coating material, while   EST. Therefore, in this study, we prepared Ti-6Al-4V/
            leading to significant amounts of copper entering the   Cu-Cr-Zr by using LMD technology and investigated
            coating. As a result, there are limitations in terms of   changes in microstructure and mechanical properties
            compatibility between the metal substrate and the cladding   under high-energy-density current conditions. This
            material. Other scholars have also conducted extensive   research provides theoretical guidance and experimental
            research in this area. For instance, Li  et al.  deposited   support for enhancing the performance of copper-based
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            AlCrFeNiMnx high-entropy  alloy on  a copper  substrate   composites.
            and found that an increase in  Mn improved the  copper   2. Materials and methods
            diffusion coefficient, facilitating diffusion of copper into
            the cladding layer and thus reducing the hardness of the   2.1. Materials preparation
            cladding layer. By depositing CoCrNiFeTix high-entropy   In this work, a Cu-Cr-Zr alloy was used as the substrate,
            alloy on the copper alloy surface, Jia et al.  demonstrated   with its main composition shown in Table 1. The substrate
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            that the hardness of the cladding layer increased with the   sample dimensions were 43 mm × 32 mm × 7 mm. Five
            addition of Ti content. CoCrW-xCu coatings with good   pieces  of Cu-Cr-Zr material were prepared for LMD.
            metallurgical bonding  were prepared by laser cladding   Before the LMD experiments, the substrate underwent
            by Dong et al.  Zhou et al.  achieved laser cladding of a   pre-treatment: First, surface oxide layers were removed by
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            gradient molybdenum coating on copper alloy surfaces.   grinding with 600#  and 1200#  sandpaper.  Subsequently,
            By  adjusting process parameters,  they  obtained well-  the  Cu-Cr-Zr  substrate  surface  underwent  shot peening
            bonded, defect-free, and dense strengthening layers. Shear   to reduce surface gloss and enhance surface roughness. In
            tests evaluated the bond strength, with maximum values   preliminary work, we thoroughly investigated the influence
            reaching 240 MPa. The above-mentioned studies have all   of surface roughness on the LMD coating properties under
            achieved effective strengthening of copper alloy surfaces,   various shot peening parameters. Detailed comparisons
            thereby enhancing their surface properties.        of interface forming performance across six distinct
              As a rapid post-processing technology, electroshock   Ra values revealed that a coating with optimal forming
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            treatment (EST) optimizes the organizational structure of   characteristics was achieved at Ra = 3.9 μm.  Consequently,
            the material through the action of high current, offering   all subsequent LMD experiments were conducted with a
            a  novel  approach  to  enhancing  material  properties.    surface Ra maintained at 3.9 μm. Finally, acetone cleaning
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            EST provides favorable conditions for analyzing the   was performed to remove oil contamination from the
            microstructure evolution of the bonding zone of the   substrate  surface, followed by  ultrasonic  cleaning  with
            composite layer under high current density. 21-23  Fan   anhydrous ethanol to eliminate adhering contaminants
            et al.   investigated  the effect of  electrical  pulse  on the   and particulates. The substrate was dried and set aside
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            microstructure of spot  welded joints  of AA2198-T8   for  later  use.  Ti-6Al-4V  powder  with  a  particle  size  of
            aluminum alloy. The interfacial defects of the welded   45–150 μm was selected as the coating material, with its
            joints were gradually reduced with the increase of the   main composition shown in Table 1. The powder exhibits a
            electrical pulse time. Liu  et al.  explored the defect   spherical morphology with excellent sphericity, with 80%
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                                                                                                            13
            healing mechanism of 6061-T6 aluminum alloy under   of the particle size distribution ranging from 69 to 117 μm.
            electrical pulse, and found that the current bypassing the   The coating was prepared via LMD in an argon atmosphere
            holes would produce local current density increase and   with oxygen content below 100  ppm, as illustrated in
            Joule heat effect around the holes, and the holes would   Figure  1A.  LMD  experiments  were  conducted  using  an
            be deformed and healed under the action of thermal   LMD 16080 system (Nanjing Zhongke Raycham Laser
            compression stress. Qian et al.  performed EST on the   Technology Co., Ltd., China), with a YLS-2000 laser source
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            interface of stainless steel joined in hot compression   (IPG Photonics) operating at 1800 W. The powder feed rate
            and found that EST promoted recrystallization at the
            interface  and  the  formation  of  fine  equiaxed  crystal   Table 1. Chemical composition of Cu‑Cr‑Zr substrate and
            grains, which contributed to the healing of the interface.   Ti‑6Al‑4V powder (wt.%)
            Taken together, EST induces the microstructure variation   Materials  Cr  Zr  Cu Al  V  C  N  O  Fe  Ti
            of the material, and such microstructural changes are
            closely related to the compression,  tensile,  and fatigue   Cu-Cr-Zr  1.03 0.11 Bal.  -  -  -  -  -  -  -
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            life of the material. 29,30                        Ti-6Al-4V  -  -  -  6.2 4.15 0.01 0.015 0.15 0.056 Bal.
            Volume 1 Issue 4 (2025)                         2                          doi: 10.36922/ESAM025430030
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