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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: No vendors are listed for this material. Please click here if you are a supplier and would like information on how to add your listing to this material.
 
Physical PropertiesOriginal ValueComments
Density 8.40 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 30.0EN ISO 6508-1
Tensile Strength 850 - 950 MPain vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 830 - 1030 MPain vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 940 - 1040 MPain horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 940 - 1140 MPain horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
Tensile Strength, Yield 565 - 665 MPa
@Strain 0.2 %
in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 550 - 750 MPa
@Strain 0.2 %
in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 620 - 820 MPa
@Strain 0.2 %
in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 675 - 775 MPa
@Strain 0.2 %
in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
Elongation at Break 30.0 - 40.0 %in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 30.0 - 40.0 %in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 37.0 - 47.0 %in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 39.0 - 49.0 %in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
Modulus of Elasticity 120 - 160 GPain vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 140 - 180 GPain vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 150 - 190 GPain horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 150 - 190 GPain horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 
Thermal PropertiesOriginal ValueComments
Maximum Service Temperature, Air 650 °Cfor parts under load
 980 °COxidation resistance
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al <= 0.400 %
Carbon, C <= 0.100 %
Chromium, Cr 20.0 - 23.0 %
Cobalt, Co <= 1.00 %
Iron, Fe <= 5.00 %
Manganese, Mn <= 0.500 %
Molybdenum, Mo 8.00 - 10.0 %
Nickel, Ni 58.0 - 68.5 %Balance
Niobium, Nb (Columbium, Cb) 3.15 - 4.15 %
Phosphorus, P <= 0.0150 %
Silicon, Si <= 0.500 %
Sulfur, S <= 0.0150 %
Tantalum, Ta <= 0.0500 %
Titanium, Ti <= 0.400 %

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NPROTO803 / 322916

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