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Powder Reuse and Its Effects on Laser Based Powder Fusion Additive Manufactured Alloy 718

Journal Article
2016-01-2071
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/2016-01-2071
Published September 20, 2016 by SAE International in United States
Powder Reuse and Its Effects on Laser Based Powder Fusion Additive Manufactured Alloy 718
Sector:
Citation: Hann, B., "Powder Reuse and Its Effects on Laser Based Powder Fusion Additive Manufactured Alloy 718," SAE Int. J. Aerosp. 9(2):209-213, 2016, https://doi.org/10.4271/2016-01-2071.
Language: English

References

  1. Ardila , L.C. , Garciandia. F. , González-Díaz , J.B. , Álvarez , P. et al. Effect of IN718 recycled powder reuse on properties of parts manufactured by means of Selective Laser Melting Physics Procedia 56 99 107 2014 10.1016/j.phpro.2014.08.152
  2. Tang , H.P. , Qian , M. , Liu , N. et al. Effect of Powder Reuse Times on Additive Manufacturing of Ti-6Al-4V by Selective Electron Beam Melting JOM 2015 67 555 10.1007/s11837-015-1300-4
  3. Standard Specification for Additive Manufacturing Nickel Alloy (UNS N07718) with Powder Bed Fusion ASTM Standard F3055 - 14a
  4. Standard Test Method for Particle Size Distribution of Metal Powders and Related Compounds by Light Scattering ASTM Standard B822 - 10
  5. Standard Test Methods for Determination of Carbon, Sulfur, Nitrogen, and Oxygen in Steel, Iron, Nickel, and Cobalt Alloys by Various Combustion and Fusion Techniques ASTM Standard E1019-11
  6. Appa Rao , G. , , Srinivasa , M. , and Sarma , D.S. Effect of oxygen content of powder on microstructure and mechanical properties of hot isostatically pressed superalloy Inconel 718 Materials Science and Engineering: A 435-436 84 99 2006
  7. Standard Test Methods for Tension Testing of Metallic Materials ASTM Standard E8/E8M-15
  8. SAE International Aerospace Material Specificiation Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable SAE Standard AMS5662 TM June 2016
  9. SAE International Aerospace Material Specification Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, Foil and Plate 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode Remelted or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated SAE Standard AMS5596 Aug. 2016
  10. P. Kantzos , P. , Bonacuse , P. , Telesman , J. , Gabb , T. et al. Effect of Powder Cleanliness on the Fatigure Behavior of Powder Metallurgy Ni-Disk Alloy Udimet 720 Superalloys 2004 ed. Green et al. TMS Warrendale, PA 2004 409 417
  11. Standard Test Method for Strain-Controlled Fatigue Testing ASTM Standard E606/606M-12

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