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EOS NickelAlloy IN625 DMSL Powder
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Nickel Alloy

Material Notes: 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 thermal fatigue 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 certain anisotropy.

Information provided by EOS GmbH (Electro Optical Systems).

Key Words: UNS N06625
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/ccPart; ISO 3369
Particle Size 29 - 41 µmd50; ISO 13320
 
Mechanical PropertiesOriginal ValueComments
Hardness, Rockwell C 27EN ISO 6508-1:2005
Tensile Strength, Ultimate 860 - 880 MPain vertical direction (Z), As built; ISO 6892-1 B10
 975 - 985 MPain horizontal direction (XY), As built; ISO 6892-1 B10
 880 - 900 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 990 - 1010 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
Tensile Strength, Yield 625 - 635 MPain vertical direction (Z), As built; ISO 6892-1 B10
 715 - 725 MPain horizontal direction (XY), As built; ISO 6892-1 B10
 635 - 645 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 675 - 685 MPa
@Treatment Temp. 870 °C,
Time 3600 sec
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
Elongation at Break 31 - 35 %in horizontal direction (XY), As built; ISO 6892-1 B10
 46 - 50 %in vertical direction (Z), As built; ISO 6892-1 B10
 32 - 36 %
@Treatment Temp. 870 °C,
Time 3600 sec
in horizontal direction (XY), Heat treated; ISO 6892-1 B10
 47 - 51 %
@Treatment Temp. 870 °C,
Time 3600 sec
in vertical direction (Z), Heat treated; ISO 6892-1 B10
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al <= 0.40 %
Carbon, C <= 0.10 %
Chromium, Cr 20 - 23 %
Cobalt, Co <= 1.0 %
Iron, Fe <= 5.0 %
Manganese, Mn <= 0.50 %
Molybdenum, Mo 8.0 - 10 %
Nickel, Ni 58 - 68.85 %Balance
Niobium, Nb (Columbium, Cb) 3.15 - 4.15 %
Phosphorus, P <= 0.015 %
Silicon, Si <= 0.50 %
Sulfur, S <= 0.015 %
Tantalum, Ta <= 0.050 %
Titanium, Ti <= 0.40 %
 
Descriptive Properties
Surface roughness1-5 µmRa, after shot peening
 3-10 µmRz, after shot peening
Volume rate4.2 mm³/s

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