NickelAlloy HX

NickelAlloy HX raw material is a nickel-chromium-iron-molybdenum alloy 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. 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.

Standard laser processing parameters results in full melting of the entire geometry, typically with 40 μm layer thickness. Parts built from 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.

The chemical composition in compliance with UNS N06002, AMS 5390
Ultimate Tensile Strength 750 MPa
Yield Strength 590 MPa
Elongation @ Break 33%

High temperature applications requiring excellent oxidation resistance up to 1.200 °C
Aerospace components
Gas turbine parts