• Acta Optica Sinica
  • Vol. 44, Issue 4, 0422002 (2024)
Xiaofeng Shang1, Jianzhou Dong1,2, Yingwei Zhang4, Zhiguo Wang2,3,*..., Yuhui Zhao2,3,**, Zhenfeng He2,3 and Jibin Zhao2,3|Show fewer author(s)
Author Affiliations
  • 1School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang 110135, Liaoning, China
  • 2Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, Liaoning, China
  • 3Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, Liaoning, China
  • 4AVIC Shenyang Aircraft Industrial (Group) Co., Ltd., Shenyang 110850, Liaoning, China
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    DOI: 10.3788/AOS231659 Cite this Article Set citation alerts
    Xiaofeng Shang, Jianzhou Dong, Yingwei Zhang, Zhiguo Wang, Yuhui Zhao, Zhenfeng He, Jibin Zhao. DED Joining Process and Ultrasonic-Assisted Performance Optimization of High-Strength Aluminum Alloys Manufactured by SLM[J]. Acta Optica Sinica, 2024, 44(4): 0422002 Copy Citation Text show less
    DED system and schematic for joining. (a) Robot and laser system; (b) powder feeder and ultrasonic vibration system; (c) robot arm; (d) schematic of DED joining; (e) pore changes under ultrasonic vibration assistance
    Fig. 1. DED system and schematic for joining. (a) Robot and laser system; (b) powder feeder and ultrasonic vibration system; (c) robot arm; (d) schematic of DED joining; (e) pore changes under ultrasonic vibration assistance
    Al-Mg-Sc-Zr alloy substrate formed by SLM and powder for joining. (a) Al-Mg-Sc-Zr substrate formed by SLM; (b) schematic of slot size; (c) slotted aluminum alloy substrate; (d) Al-Mg-Sc-Zr powder
    Fig. 2. Al-Mg-Sc-Zr alloy substrate formed by SLM and powder for joining. (a) Al-Mg-Sc-Zr substrate formed by SLM; (b) schematic of slot size; (c) slotted aluminum alloy substrate; (d) Al-Mg-Sc-Zr powder
    Samples joined with different process parameters and size of tensile sample. (a) Sample under energy density of 75 J/mm2 and size of tensile sample; (b) sample under energy density of 100 J/mm2; (c) sample under energy density of 125 J/mm2; (d) sample under energy density of 150 J/mm2
    Fig. 3. Samples joined with different process parameters and size of tensile sample. (a) Sample under energy density of 75 J/mm2 and size of tensile sample; (b) sample under energy density of 100 J/mm2; (c) sample under energy density of 125 J/mm2; (d) sample under energy density of 150 J/mm2
    Metallographic structure of samples with and without ultrasonic vibration and hot isostatic pressing. (a) Energy density is 150 J/mm2; (b) energy density is 75 J/mm2; (c) energy density is 100 J/mm2; (d) energy density of 125 J/mm2; (e) ultrasonic current is 0.8 A; (f) ultrasonic current is 1.2 A; (g) ultrasonic current is 1.6 A; (h) sample surface without hot isostatic pressing; (i) sample surface with hot isostatic pressing; (j) metallographic structure without ultrasonic vibration and with hot isostatic pressing; (k) metallographic structure with ultrasonic vibration and with hot isostatic pressing and microhardness curve
    Fig. 4. Metallographic structure of samples with and without ultrasonic vibration and hot isostatic pressing. (a) Energy density is 150 J/mm2; (b) energy density is 75 J/mm2; (c) energy density is 100 J/mm2; (d) energy density of 125 J/mm2; (e) ultrasonic current is 0.8 A; (f) ultrasonic current is 1.2 A; (g) ultrasonic current is 1.6 A; (h) sample surface without hot isostatic pressing; (i) sample surface with hot isostatic pressing; (j) metallographic structure without ultrasonic vibration and with hot isostatic pressing; (k) metallographic structure with ultrasonic vibration and with hot isostatic pressing and microhardness curve
    SEM images of pores. (a) Pores distributed around the interface; (b) magnified morphology of the pore
    Fig. 5. SEM images of pores. (a) Pores distributed around the interface; (b) magnified morphology of the pore
    Efficiency of space filling and microhardness of samples with and without ultrasonic vibration assistance. (a) Efficiency of space filling of samples with and without ultrasonic vibration assistance; (b) microhardness of samples with and without ultrasonic vibration assistance
    Fig. 6. Efficiency of space filling and microhardness of samples with and without ultrasonic vibration assistance. (a) Efficiency of space filling of samples with and without ultrasonic vibration assistance; (b) microhardness of samples with and without ultrasonic vibration assistance
    Tensile properties and fracture morphologies of specimens with and without ultrasonic vibration assistance. (a) Stress-strain curves; (b) fracture location of different tensile samples; (c) fracture location with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (d) fracture location with 150 J/mm2 energy density and without ultrasonic vibration; (e) fracture morphology with 150 J/mm2 energy density and without ultrasonic vibration; (f) magnified fracture morphology with 150 J/mm2 energy density and without ultrasonic vibration; (g) fracture morphology with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (h) magnified fracture morphology with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (i) stress-strain curves with and without ultrasonic vibration and with hot isostatic pressing; (j) fracture morphology with 1.6 A current ultrasonic vibration and hot isostatic pressing; (k) magnified fracture morphology with 1.6 A current ultrasonic vibration and hot isostatic pressing
    Fig. 7. Tensile properties and fracture morphologies of specimens with and without ultrasonic vibration assistance. (a) Stress-strain curves; (b) fracture location of different tensile samples; (c) fracture location with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (d) fracture location with 150 J/mm2 energy density and without ultrasonic vibration; (e) fracture morphology with 150 J/mm2 energy density and without ultrasonic vibration; (f) magnified fracture morphology with 150 J/mm2 energy density and without ultrasonic vibration; (g) fracture morphology with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (h) magnified fracture morphology with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (i) stress-strain curves with and without ultrasonic vibration and with hot isostatic pressing; (j) fracture morphology with 1.6 A current ultrasonic vibration and hot isostatic pressing; (k) magnified fracture morphology with 1.6 A current ultrasonic vibration and hot isostatic pressing
    Microstructure and chemical composition distribution in the joining zone of specimens fabricated with and without ultrasonic vibration. (a) Microstructure with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (b) distribution of strengthening phase with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (c) element content of strengthening and non-strengthening phase with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (d) microstructure and element distribution of specimens with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (e) microstructure and element distribution of specimens with 150 J/mm2 energy density and without ultrasonic vibration
    Fig. 8. Microstructure and chemical composition distribution in the joining zone of specimens fabricated with and without ultrasonic vibration. (a) Microstructure with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (b) distribution of strengthening phase with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (c) element content of strengthening and non-strengthening phase with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (d) microstructure and element distribution of specimens with 1.6 A current ultrasonic vibration and 150 J/mm2 energy density; (e) microstructure and element distribution of specimens with 150 J/mm2 energy density and without ultrasonic vibration
    XRD spectra of substrate and joining zone with and without ultrasonic vibration. (a) 30°-80°; (b) 30°-45°
    Fig. 9. XRD spectra of substrate and joining zone with and without ultrasonic vibration. (a) 30°-80°; (b) 30°-45°
    ElementMgScZrSiAl
    Mass fraction /%7.60.50.31.5Bal.
    Table 1. Mass fraction of Al-Mg-Sc-Zr alloy powder and substrate
    No.Laser power /WScanning rate /(mm·s-1Powder feeding rate /(g·min-1Energy density /(J·mm-2
    1#3000103.775
    2#30007.53.7100
    3#250053.7125
    4#300053.7150
    Table 2. Parameters for joining by DED process
    No.Current /APower /WFrequency /kHz
    U10.817619.66
    U21.226419.66
    U31.635219.66
    Table 3. Ultrasonic vibration parameters
    No.

    Temperature / ℃

    Pressure /MPaHolding time /hUltrasonic vibration
    HIP13251706
    HIP2×
    Table 4. Hot isostatic pressing parameters
    No.1#2#3#4#U1U2U3HIP1
    A /%0.730.680.440.581.361.291.517.58
    Table 5. Elongations of specimens with and without ultrasonic vibration and with hot isostatic pressing
    Xiaofeng Shang, Jianzhou Dong, Yingwei Zhang, Zhiguo Wang, Yuhui Zhao, Zhenfeng He, Jibin Zhao. DED Joining Process and Ultrasonic-Assisted Performance Optimization of High-Strength Aluminum Alloys Manufactured by SLM[J]. Acta Optica Sinica, 2024, 44(4): 0422002
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