Chinese Journal of Lasers, Volume. 47, Issue 5, 0500002(2020)

Laser Additive Manufacturing of High-Performance Metallic Aerospace Components

Dongdong Gu1,2,3、*, Hongmei Zhang1,2, Hongyu Chen1,2, Han Zhang1,2, and Lixia Xi1,2
Author Affiliations
  • 1College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, China
  • 2Jiangsu Provincial Engineering Laboratory for Laser Additive Manufacturing of High-Performance Metallic Components, Nanjing, Jiangsu 210016, China
  • 3National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing, Jiangsu 210016, China
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    Figures & Tables(16)
    Microstructure control of Al-based nano/in-situ composite processed by laser additive manufacturing. (a) Ring-structured TiC reinforcing phase[37]; (b) strip-structured in-situ Al4SiC4 reinforcing phase[42]; (c) fine equiaxed structure of Al-matrix with TiB2 reinforcement[43]
    Selective laser melting (SLM) additive manufacturing of 7075 aluminum alloy: transformation of columnar dendrites to fine equiaxed crystals and attendant crack suppression via nano-particle modification[36]
    Comparison of microstructures between TC4 alloy and Ti-8.5Cu alloy processed by laser additive manufacturing[67]. (a) TC4 alloy showing coarse columnar grain structure; (b) Ti-8.5Cu alloy showing fine and fully equiaxed grain structure
    Microstructure control of TC4 alloy processed by laser additive manufacturing combined with high-intensity ultrasound [69]. (a) Schematic of laser melting deposition process combined with high-intensity ultrasound; (b) conventional laser melting deposition TC4 alloy showing large columnar grains; (c) ultrasound combined laser additive manufacturing TC4 alloy showing fine equiaxed grains
    Mechanisms for metallurgical modification by nanoparticles during laser melting of Ni-based composites[95]
    Microstructure and property control of laser additive manufacturing of Ni-based gradient interface composites and nanoparticle reinforced composites. (a) Gradient interface of micron-WC reinforced composites[96]; (b) cellular structure of nano-TiC reinforced composites[101]; (c) superhydrophobic surface of Ni-based nanocomposites[102]
    LMD additive manufacturing of large-scale integral metal components[104]. (a) Large-scale load-bearing titanium alloy components for aircrafts; (b) titanium alloy integral disk with gradient performance for aeroengine; (c) solidified grain structures in gradient transition zone between disk and blades
    Laser melting deposition and selective laser melting additive manufacturing of large-scale complex-shaped metal components. (a) LMD forming C919 titanium alloy rib edge strip with length of 3100 mm; (b) SLM forming titanium alloy fan blade edge wrapping with length of 1200 mm; (c) SLM forming nickel-based superalloy engine casing with size of Ф 576 mm×200 mm
    Selective laser melting manufactured copper alloy integral components and performance tests at NASA. (a) Hot-fire test of laser additive manufactured component conducted by NASA and Aerojet Rocketdyne[106]; (b) integral components of copper alloy liner in combustion chamber of rocket engine[107]
    Fuel nozzle components in aeroengine manufactured by General Electric Company using selective laser melting technology[110]. (a) Advanced turboprop engine (ATP); (b) working principle of fuel nozzles in aeroengine; (c) laser additive manufactured fuel nozzle components
    Additive manufacturing of a designed lattice structure inspired by crystal microstructure based on hardening mechanism of metal crystal. (a) Lattice structure inspired by crystal microstructure; (b) difference of stress-strain curves between single-phase and multi-phase crystal lattice structures; (c) finite element method (FEM) simulation of stress distribution of lattice structure inspired by hexagonal close-packed (HCP) crystal [113]
    New bionic lattice cabin partition designed by Airbus and manufactured by selective laser melting technology[115-117]. (a) Structure of bionic lattice cabin partition; (b) photograph of assembled bionic lattice cabin partition; (c) cross-scale structure design of bionic lattice cabin partition; (d) components of bionic partition processed by SLM additive manufacturing
    Laser additive manufacturing of lightweight and impact resistant bionic functional structures[122,125]. (a) Macroscopic feature of mantis shrimp telson; (b) SLM process of bio-inspired bi-directionally corrugated panel impact resistant structure; (c) effect of height and wavelength of bi-directionally corrugated panel on crush force efficiency (CFE); (d) diving bell of water spider; (e) bionic reticulated
    • Table 1. Mechanical properties of aluminum alloy and its composites prepared by laser additive manufacturing

      View table

      Table 1. Mechanical properties of aluminum alloy and its composites prepared by laser additive manufacturing

      MaterialForming processHeat treatmentTensile strength /MPaElongation /%Ref.
      AlSi10MgSLM396±83.47±0.6[28]
      SLM450 ℃/2 h282.36±6.113.4±0.51[29]
      AlSi12SLM3803[22]
      SLM400±294[30]
      Al-Cu-MgSLM4026±1.4[31]
      SLMT6455±106.2±1.8[32]
      Al-Mg-Sc-ZrSLM427±817.2--20.2[33]
      SLM350 ℃/2 h515±1624[33]
      Al-ZnSLM203±120.5±0.2[34]
      SLMT6206±25.70.4[34]
      AlSi10Mg-CNTsSLM4997.6[35]
      AlSi10MgSLM3157.3[36]
      AlZnMgCu+ZrSLMT6383--4173.8--5.4[36]
      AlSi10Mg-TiCSLM48610.9[37]
      AlSi10Mg-TiB2SLM53015.5[38]
    • Table 2. Mechanical properties of titanium and titanium alloy prepared by laser additive manufacturing

      View table

      Table 2. Mechanical properties of titanium and titanium alloy prepared by laser additive manufacturing

      MaterialForming processHeat treatmentMicrostructureTensilestrength /MPaElongation /%Ref.
      CP-TiSLMα757±1219.5±1.8[52]
      CP-TiLMDα+β58519[56]
      Ti-6Al-4VSLMα'1140±108.2±0.3[57]
      Ti-6Al-4VSLMStress relievingthermal treatmentα+β+α'1046±69.5±1[58]
      Ti-6Al-4VSLMHot isostaticpressing (920 ℃/4 h)α+β1040±3012.5±0.5[59]
      Ti-6Al-4VSLMIn-situ annealingRefined α+β124011.5[54]
      Ti-6Al-4VLMDNeedlelike α'1099±24.9±0.1[60]
      Ti-13Nb-13ZrSLMPrimary β1020±156.5±0.3[61]
      Ti-5Al-2.5SnSLMNeedlelike α'11737.7[62]
      Ti-15Ta-xZrSLMα+β960±3218±1.9[63]
      Ti-5Al-5V-5Mo-3CrSLMPrimary β80014[64]
      Ti-6.5Al-3.5Mo-1.5Zr-0.3SiLMDα1101± 910.2± 2.2[65]
      Ti6Al4V-xBLMDPrimary β11089[66]
    • Table 3. Mechanical properties of nickle-based superalloys and their composites prepared by laser additive manufacturing

      View table

      Table 3. Mechanical properties of nickle-based superalloys and their composites prepared by laser additive manufacturing

      MaterialForming processThermal treatmentTensilestrength /MPaElongation /%Ref.
      111716[81]
      Inconel 718SLM980 ℃/1 h+720 ℃/8 h+620 ℃/8 h137112.3[82]
      95327[83]
      LMD1150 ℃/1 h133434.1[83]
      955±641±1[84]
      SLM1100 ℃/1 h886±1156±5[84]
      Inconel 62571547[85]
      LMD900 ℃/1 h75040[85]
      1010±101.6±0.2[86]
      Inconel 738LCSLMHIP (100 MPa/1175 ℃/4 h)11003.9[86]
      LMD107410.8[87]
      Hastelloy-XSLM79027[88]
      K418SLM1072±38.611.27±2.14[89]
      CM247LCSLM10507.5[90]
      Inconel 718-WCSLM1464.619.74[91]
      Inconel 718-TiCSLM102912.32[92]
      1070 ℃/1 h+720 ℃/8 h+620 ℃/8 h1380.869.08[92]
      K418-grapheneSLM120010.3[93]
      Inconel 625-grapheneLMD969.89±3813.36±0.73[94]
      Inconel 625-CNTsLMD1005.55±11.121.44±2.8[94]
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    Dongdong Gu, Hongmei Zhang, Hongyu Chen, Han Zhang, Lixia Xi. Laser Additive Manufacturing of High-Performance Metallic Aerospace Components[J]. Chinese Journal of Lasers, 2020, 47(5): 0500002

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    Paper Information

    Category: reviews

    Received: Feb. 28, 2020

    Accepted: Mar. 31, 2020

    Published Online: May. 12, 2020

    The Author Email: Gu Dongdong (dongdonggu@nuaa.edu.cn)

    DOI:10.3788/CJL202047.0500002

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