Nickel-alloy (Inconel 718) with heat treatment
Nickel-based alloy for the production of components for high-temperature applications.Homogeneous, dense structure. Typical applications are turbine construction (aviation or stationary turbines) or exhaust tracts within motor sports applications.
ASTM B 637 UNS 07718
State of starting material
Parts are built in a metal powder bed through a laser (or lasers) melting the metal powder layer-by-layer. Synonyms: Selective Laser Melting, SLM, Direct Metal Laser Sintering, DMLS, Laser Cusing
12 W/m °C
coefficient of thermal expansion: 13 per °C
Data source: Concept Laser
ATTENTION: The presented values are provided by the material manufacturers and are only indicative. Realized material properties may differ from these value for several reasons. Additively does not guarantee the correctness of this information in any way.
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