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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: 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 PropertiesMetricEnglishComments
Density 8.40 g/cc0.303 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Hardness, Rockwell C 30.030.0EN ISO 6508-1
Tensile Strength 850 - 950 MPa123000 - 138000 psiin vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 830 - 1030 MPa120000 - 149000 psiin vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 940 - 1040 MPa136000 - 151000 psiin horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 940 - 1140 MPa136000 - 165000 psiin horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
Tensile Strength, Yield  565 - 665 MPa
@Strain 0.2 %
81900 - 96500 psi
@Strain 0.2 %
in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 550 - 750 MPa
@Strain 0.2 %
79800 - 109000 psi
@Strain 0.2 %
in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 620 - 820 MPa
@Strain 0.2 %
89900 - 119000 psi
@Strain 0.2 %
in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 675 - 775 MPa
@Strain 0.2 %
97900 - 112000 psi
@Strain 0.2 %
in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
Elongation at Break 30.0 - 40.0 %30.0 - 40.0 %in horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 30.0 - 40.0 %30.0 - 40.0 %in horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 37.0 - 47.0 %37.0 - 47.0 %in vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 39.0 - 49.0 %39.0 - 49.0 %in vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
Modulus of Elasticity 120 - 160 GPa17400 - 23200 ksiin vertical direction (Z), As built; ISO 6892 -1:2009 (B) Annex D
 140 - 180 GPa20300 - 26100 ksiin vertical direction (Z), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 150 - 190 GPa21800 - 27600 ksiin horizontal direction (XY), As built; ISO 6892 -1:2009 (B) Annex D
 150 - 190 GPa21800 - 27600 ksiin horizontal direction (XY), Stress relieved; ISO 6892 -1:2009 (B) Annex D
 
Thermal PropertiesMetricEnglishComments
Maximum Service Temperature, Air 650 °C1200 °Ffor parts under load
 980 °C1800 °FOxidation resistance
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al <= 0.400 %<= 0.400 %
Carbon, C <= 0.100 %<= 0.100 %
Chromium, Cr 20.0 - 23.0 %20.0 - 23.0 %
Cobalt, Co <= 1.00 %<= 1.00 %
Iron, Fe <= 5.00 %<= 5.00 %
Manganese, Mn <= 0.500 %<= 0.500 %
Molybdenum, Mo 8.00 - 10.0 %8.00 - 10.0 %
Nickel, Ni 58.0 - 68.5 %58.0 - 68.5 %Balance
Niobium, Nb (Columbium, Cb) 3.15 - 4.15 %3.15 - 4.15 %
Phosphorus, P <= 0.0150 %<= 0.0150 %
Silicon, Si <= 0.500 %<= 0.500 %
Sulfur, S <= 0.0150 %<= 0.0150 %
Tantalum, Ta <= 0.0500 %<= 0.0500 %
Titanium, Ti <= 0.400 %<= 0.400 %

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NPROTO803 / 322916

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