Inconel 718

A high-performance nickel-chromium alloy known
for its excellent strength, corrosion resistance
and ability to maintain its properties
at extremely high temperatures.

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

Standard delivery time 10 days
Production layer 0,04 – 0,08 mm
Minimum wall thickness 0,5 mm
Maximum part´s dimensions 390 x 390 x 390 mm

 

Datasheet

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

 

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