Key features
Inconel 718 is a precipitation hardened nickel-chromium alloy with good tensile strength and yield strength, good fatigue behaviour, good high temperature tensile strength up to 700 °C. Parts printed from Inconel 718 can be further processed by conventional technologies such as machining, electroless plating, etc.
Suitable uses
The material is ideal for many high temperature applications such as gas turbine components, instrument parts, components for the power and process industries, etc. It also has excellent potential for cryogenic applications. Due to the lay-up method, the parts have a certain anisotropy.
Specific applications
- turbines, exhaust systems, engine parts for aerospace industry
- steam generators, gas turbines and other components for the energetic sector
- components for high-performance engines in the automotive industry
Technological specifications
| Production layer | 0,03 – 0,09 mm |
| Minimum wall thickness | 0,5 mm |
| Maximum part´s dimensions | 600 x 600 x 1500 mm |
Datasheet - EOS M400
| Status | Without heat treatment | Precipitation hardening | ||
| Orientation | XY | Z | XY | Z |
| Tensile strength Rm (MPa) | 1060 | 980 | 1500 | 1430 |
| Yield strength Rp0,2 (MPa) | 750 | 630 | 1250 | 1200 |
| Elongation at break ε (%) | 25 | 29 | 12 | 13 |
| Hardness Vickers HV | – | 467 | ||
| Density ρ (kg/m3) | 8250 | |||
Stáhnout datasheet
Mějte vše na jednom místě. Stáhněte si datasheet všech našich výrobních materiálů.
Download datasheet
