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Specialty Compounds RTP Company
EOS NickelAlloy IN625 Powder Processed by DMSL on EOSINT M 270
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Nickel Alloy
Material Notes: Description: Parts built from EOS NickelAlloy IN625 have chemical composition corresponding to UNS N06625, AMS 5666F, AMS 5599G, W.Nr 2.4856, DIN NiCr22Mo9Nb. This type of alloy is characterized by having high tensile, creep and rupture strength. Conventionally cast or wrought components in this type of nickel alloy have typically excellent fatigue and thermalfatigue properties combined with good oxidation resistance. EOS NickelAlloy IN625 is expected to have good corrosion resistance in various corrosive environments. Especially sea-water applications require high pitting and crevice corrosion resistance, stress-corrosion resistance against chloride-ions, high tensile and corrosion-fatigue strength. However, corrosion resistance has not been verified yet and therefore it is recommended to conduct relevant corrosion tests and studies prior to use in specific corrosive environment. Parts built from EOS NickelAlloy IN625 can be heat treated and material properties can be varied within specified range. Parts can be machined, spark-eroded, welded, micro shot-peened, polished and coated in both as-built and in heat treated conditions. Due to the layerwise building method, the parts have a certain anisotropy - see Technical Data for examples.

Stress relieve: anneal at 870 °C (1600 °F) for 1 hour, rapid cooling

Information provided by Proto3000
Key Words: Direct Metal Laser Sintering
Vendors:
Available Properties
  • Density
  • Hardness, Rockwell C, EN ISO 6508-1
  • Tensile Strength, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), As built
  • Tensile Strength, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), Stress relieved
  • Tensile Strength, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), As built
  • Tensile Strength, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), Stress relieved
  • Tensile Strength, Yield, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), As built
  • Tensile Strength, Yield, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), Stress relieved
  • Tensile Strength, Yield, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), Stress relieved
  • Tensile Strength, Yield, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), As built
  • Elongation at Break, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), As built
  • Elongation at Break, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), Stress relieved
  • Elongation at Break, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), As built
  • Elongation at Break, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), Stress relieved
  • Modulus of Elasticity, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), As built
  • Modulus of Elasticity, ISO 6892 -1:2009 (B) Annex D, in vertical direction (Z), Stress relieved
  • Modulus of Elasticity, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), As built
  • Modulus of Elasticity, ISO 6892 -1:2009 (B) Annex D, in horizontal direction (XY), Stress relieved
  • Maximum Service Temperature, Air, for parts under load
  • Maximum Service Temperature, Air, Oxidation resistance
  • Aluminum, Al
  • Carbon, C
  • Chromium, Cr
  • Cobalt, Co
  • Iron, Fe
  • Manganese, Mn
  • Molybdenum, Mo
  • Nickel, Ni, Balance
  • Niobium, Nb (Columbium, Cb)
  • Phosphorus, P
  • Silicon, Si
  • Sulfur, S
  • Tantalum, Ta
  • Titanium, Ti
  
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Manufacturer Notes:
Electro Optical Systems GMBH

Category Notes
none

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