CL 101NB (Metal / Nickel-based alloys)

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Material

Vendor

Concept Laser

Description

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.

Standards

ASTM B446-03, UNS N06625

State of starting material

powder

Properties, applications and appearance

Field of application

Rapid Manufacturing


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Process

Manufacturing process

Laser Melting
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

Physical, mechanical and thermal properties

Mechanical Properties

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 %

Thermal Properties

thermal conductivity: 10 W/m °C
coefficient of thermal expansion: 12.8 per °C


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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.