Nickel alloys material characteristics make it ideal for a wide range of applications, for example in gas turbines for both aerospace and energy industries, process industry, oil and gas, ship building.
The nickel alloy family of powders encompasses the IN625, IN718, IN939, HX and HAYNES® 282® alloys. All these powders are designed and tested for use on EOS’ metal systems.
All EOS nickel alloy powders are shipped with an inspection certificate (according to EN 10204, Type 3.1) showing the results of the extensive QA testing not only of the powder itself, but also of test parts built on a dedicated system with a dedicated process.
EOS also offers a wide range of validated processes for each of the above materials. These offer the optimal combination of parameters (e.g. laser power, layer thickness, etc.) in order to ensure that the properties of the 3D printed part are consistently achieved.
Parts are characterized by having high tensile, creep and rupture strength and are heat and corrosion resistant. This combination is ideal for for racing applications, gas turbines in aerospace and energy as well as ship building industries.
Typical Part Properties
Chemical composition in compliance with | UNS N06625, AMS 5666, AMS 5599, 2.4856, NiCr22Mo9Nb |
Ultimate Tensile Strength | 920 MPa |
Yield Strength | 670 MPa |
Elongation @ Break | 40 % |
Parts show good tensile, fatigue, creep and rupture strength at temperatures up to 700°C making it ideal for many high temperature applications such as gas turbine parts, instrumentation parts, power and process industry parts, etc.
Typical Part Properties
Chemical composition in compliance with | UNS N07718, AMS 5662, AMS 5664, 2.4668, NiCr19Fe19NbMo3 |
Ultimate Tensile Strength | 1020 MPa |
Yield Strength | 710 MPa |
Elongation @ Break | 29 % |
Parts show high tensile, fatigue, creep and rupture strength at temperatures up to 850°C (1560°F) as well as excellent corrosion and oxidation resistance. Parts are crack-free in as manufactured and heat-treated condition and are resistant to strain-age cracking. A short AM-optimized heat treatment is needed but not HIP.
Typical Part Properties
Ultimate Tensile Strength | 1510 MPa |
Yield Strength | 1115 MPa |
Elongation @ Break | 12 % |
Parts show high strength and oxidation resistance also at elevated temperatures of up to 1200°C, making it ideal for applications in aerospace, gas turbines, etc.
Typical Part Properties
Chemical composition in compliance with | UNS N06002, AMS 5390 |
Ultimate Tensile Strength | 750 MPa |
Yield Strength | 590 MPa |
Elongation @ Break | 33 % |
This material is a precipitation strengthened nickel-base superalloy with a unique combination of high temperature strength, thermal stability, and fabricability. The alloy was developed for high temperature structural applications.
Typical Part Properties
Ultimate Tensile Strength | 1180 MPa |
Yield Strength | 710 MPa |
Elongation @ Break | 26 % |