DIN 17742 NiCr25FeAl3YC Solution-Annealed Alloy with Aging Treatment
The material NiCr25FeAl3YC with the material number 2.4647, which is applied in the form of strips, sheets, bars and wires for gas turbines, is a highly creep-resistant, corrosion-resistant and carbide-hardened nickel-base alloy.
Properties
General
| Property | Temperature | Value |
|---|---|---|
Density | 20.0 °C | 7.9 g/cm³ |
Mechanical
| Property | Temperature | Value |
|---|---|---|
Elastic modulus | 20.0 °C | 214 GPa |
Elongation | 20.0 °C | 30 % |
Hardness, Brinell | 20.0 °C | 220 [-] |
Tensile strength | 20.0 °C | 680 MPa |
Yield strength Rp0.2 | 20.0 °C | 270 MPa |
Yield strength Rp1.0 | 20.0 °C | 330 MPa |
Thermal
| Property | Temperature | Value | Comment |
|---|---|---|---|
Coefficient of thermal expansion | 400.0 °C | 1.43E-5 1/K | |
Melting point | 1200 - 1480 °C | Typical for Nickel Chromium Iron Alloy | |
Specific heat capacity | 23.0 °C | 285 - 545 J/(kg·K) | Typical for Nickel Chromium Iron Alloy |
Thermal conductivity | 23.0 °C | 8 - 35 W/(m·K) | Typical for Nickel Chromium Iron Alloy |
Electrical
| Property | Temperature | Value |
|---|---|---|
Electrical resistivity | 20.0 °C | 1.25E-6 Ω·m |
Chemical properties
| Property | Value |
|---|---|
Aluminium | 2.4 - 3 % |
Carbon | 0.2 - 0.4 % |
Chromium | 24 - 26 % |
Copper | 0.15 % |
Iron | 8 - 11 % |
Manganese | 0.1 % |
Nickel | 58.3 % |
Phosphorus | 0.02 % |
Silicon | 0.5 % |
Sulfur | 0.015 % |
Titanium | 0.1 - 0.25 % |
Yttrium | 0.05 - 0.15 % |
Zirconium | 0.01 - 0.1 % |
Metal
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