Nickel-based alloy (Inconel 625), with heat treatment
For the production of components for high-temperature applications: turbine construction (aviation or stationary turbines) or exhaust tracts within motor sports applications.
ASTM B446-03, UNS N06625
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
ultimate tensile strenght:
920 - 990 MPa
yield stress Rp 0.2%: 640 - 670 MPa
tensile modulus (Young's / E- ): 200,000 MPa
elongation at break: 20 - 32 %
10 W/m °C
coefficient of thermal expansion: 12.8 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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