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EOS Flexline NickelAlloy HX DMSL on EOS M 290
Categories: Metal; 3D Printing/Additive Manufacturing Metal; Nonferrous Metal; Nickel Alloy

Material Notes: EOS NickelAlloy HX raw material is a nickel-chromium-iron-molybdenum alloy in fine powder form. Its composition corresponds to UNS N06002. While the wrought and cast versions of the alloy generally are solution annealed, the laser melted material manufactured of this powder has a high strength and good elongation already in the as-built condition. Solution annealing of the laser sintered material will homogenize the microstructure, relax internal stresses and increase the elongation, while slightly decreasing the strength. This type of alloy is characterized by having high strength and oxidation resistance also at elevated temperatures, and is often used up to 1200°C. Therefore its applications can be found in aerospace technology, gas turbine parts, etc. Standard laser processing parameters results in full melting of the entire geometry, typically with 40 µm layer thickness. Parts built from EOS NickelAlloy HX can be heat treated and material properties can be varied within specified range. In both as-built and solution heat treated states the parts can be machined, spark-eroded, welded, micro shot-peened, polished, and coated if required. Unexposed powder can be reused.

Information provided by EOS GmbH (Electro Optical Systems).

Key Words: N06002
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Physical PropertiesOriginal ValueComments
Density 8.20 g/cc
 
Mechanical PropertiesOriginal ValueComments
Tensile Strength, Ultimate 625 - 725 MPavertical direction (Z); ISO 6892-1:2009 (B)
 770 - 870 MPahorizontal direction (XY); ISO 6892-1:2009 (B)
Tensile Strength, Yield 495 - 595 MPavertical direction (Z); ISO 6892-1:2009 (B)
 580 - 680 MPahorizontal direction (XY); ISO 6892-1:2009 (B)
Elongation at Break 19 - 35 %horizontal direction (XY); ISO 6892-1:2009
 31 - 47 %vertical direction (Z); ISO 6892-1:2009
Modulus of Elasticity 155 - 195 GPavertical direction (Z); ISO 6892-1:2009 (B)
 175 - 215 GPahorizontal direction (XY); ISO 6892-1:2009 (B)
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al <= 0.50 %
Boron, B <= 0.010 %
Carbon, C <= 0.10 %
Chromium, Cr 20.5 - 23 %
Cobalt, Co 0.50 - 2.5 %
Copper, Cu <= 0.50 %
Iron, Fe 17 - 20 %
Manganese, Mn <= 1.0 %
Molybdenum, Mo 8.0 - 10 %
Nickel, Ni 40.165 - 53.8 %Balance
Phosphorus, P <= 0.040 %
Selenium, Se <= 0.0050 %
Silicon, Si <= 1.0 %
Sulfur, S <= 0.030 %
Titanium, Ti <= 0.15 %
Tungsten, W 0.20 - 1.0 %
 
Descriptive Properties
Surface roughness< 0.5 µmRz, after polishing
 10-30 µmRz, after shot-peening (horizontal / vertical)
 3–6.5 µmRa, after shot-peening (horizontal / vertical)
Volume rate4.2 mm³/s

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NEOS936 / 280596

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