Alloy 718: Premium Nickel-Chromium Alloy for High-Performance Applications
2.4668 (NiCr19NbMo) is a precipitation hardening nickel-chromium alloy that also contains additions of iron, niobium, molybdenum, aluminium and titanium, providing a unique combination of high strength and corrosion resistance together with excellent weldability. It shows the following features and properties:
Properties
General
| Property | Temperature | Value |
|---|---|---|
Density | 23.0 °C | 8.22 g/cm³ |
Mechanical
| Property | Temperature | Value |
|---|---|---|
Elastic modulus | 23.0 °C | 204 GPa |
Elongation | 23.0 °C | 12 - 17 % |
Hardness, Brinell | 23.0 °C | 313 - 354 [-] |
Reduction of area | 23.0 °C | 15 % |
Tensile strength | 23.0 °C | 1034 - 1276 MPa |
Yield strength Rp0.2 | 23.0 °C | 827 - 1034 MPa |
Thermal
| Property | Temperature | Value | Comment |
|---|---|---|---|
Coefficient of thermal expansion | 23.0 °C | 1.35E-5 1/K | |
Melting point | 1260 - 1335 °C | ||
Thermal conductivity | 23.0 °C | 14.2 W/(m·K) | for 0-200°C |
Magnetic
| Property | Temperature | Value |
|---|---|---|
Relative magnetic permeability | 23.0 °C | 1 [-] |
Chemical properties
| Property | Value |
|---|---|
Aluminium | 0.5 % |
Chromium | 19 % |
Iron | 18 - 18.5 % |
Molybdenum | 3 % |
Nickel | 53 % |
Niobium | 5 % |
Titanium | 0.9 % |
Technological properties
| Property | ||
|---|---|---|
| Application areas | Offshore & marine: Fasteners, valves, choke stems, down-hole tooling, cryogenic storage tanks and pump bodies;Aerospace: Jet engine components, rocket motors and thrust reversers;Power generation: Nuclear reactor parts, gas turbine components, nuclear fuel element spacers, containment vessels and valves;Other: Hot extrusion tooling | |
| Corrosion properties | Excellent corrosion resistance | |
| Hot forming | It can be hot worked between 985-1150°C. | |
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