EN 10095 NiCr20Ti Alloy – Solution Annealed (With AT)
NiCr20Ti is also contained as a aviation material (mat. No 2.4630) in material-performance specifications of the German Aviation WL 2.4630-1, -2, -3,-4, -100 : 1993-08 (Werkstoff-Leistungsblätter der Deutschen Luftfahrt WL). It is non-scaling up to approx. 1150 °C (highest application temperature in air) and shows high corrosion resistance and creep rupture strength up to 750°C as well as favorable resistance to thermal shocks. Application in carburizing or sulfureous furnace athmospheres is not advisable at higher temperatures. Use for components in gas turbines (rings, casing parts), parts for industrial furnace construction, palletts and boxes for component`s heat-treatment as well as for components in aerospace. Processing properties: formability: good weldability: good
Properties
General
| Property | Temperature | Value |
|---|---|---|
Density | 20.0 °C | 8.4 g/cm³ |
Mechanical
| Property | Temperature | Value |
|---|---|---|
Elastic modulus | 20.0 °C | 221 GPa |
100.0 °C | 217 GPa | |
200.0 °C | 211 GPa | |
300.0 °C | 204 GPa | |
400.0 °C | 197 GPa | |
500.0 °C | 190 GPa | |
600.0 °C | 182 GPa | |
700.0 °C | 174 GPa | |
800.0 °C | 165 GPa | |
900.0 °C | 154 GPa | |
1000.0 °C | 140 GPa | |
Elongation | 20.0 °C | 30 % |
Hardness, Brinell | 20.0 °C | 230 [-] |
Tensile strength | 20.0 °C | 650 - 850 MPa |
Yield strength Rp0.2 | 20.0 °C | 240 MPa |
Thermal
| Property | Temperature | Value | Comment |
|---|---|---|---|
Coefficient of thermal expansion | 100.0 °C | 1.17E-5 1/K | |
200.0 °C | 1.26E-5 - 1.27E-5 1/K | ||
300.0 °C | 1.32E-5 1/K | ||
400.0 °C | 1.38E-5 - 1.39E-5 1/K | ||
500.0 °C | 1.43E-5 1/K | ||
600.0 °C | 1.48E-5 - 1.5E-5 1/K | ||
700.0 °C | 1.54E-5 1/K | ||
800.0 °C | 1.6E-5 - 1.65E-5 1/K | ||
900.0 °C | 1.66E-5 1/K | ||
1000.0 °C | 1.75E-5 - 1.82E-5 1/K | ||
Max service temperature, long | 0 - 1150 °C | ||
Melting point | 1400 °C | Typical for Nickel Chromium Alloy | |
Specific heat capacity | 20.0 °C | 445 - 460 J/(kg·K) | |
100.0 °C | 465 J/(kg·K) | ||
200.0 °C | 490 J/(kg·K) | ||
300.0 °C | 515 J/(kg·K) | ||
400.0 °C | 540 J/(kg·K) | ||
500.0 °C | 570 J/(kg·K) | ||
600.0 °C | 600 J/(kg·K) | ||
700.0 °C | 620 J/(kg·K) | ||
800.0 °C | 650 J/(kg·K) | ||
900.0 °C | 675 J/(kg·K) | ||
1000.0 °C | 700 J/(kg·K) | ||
Thermal conductivity | 20.0 °C | 12 - 12.1 W/(m·K) | |
100.0 °C | 13.7 W/(m·K) | ||
200.0 °C | 15.6 W/(m·K) | ||
300.0 °C | 17.1 W/(m·K) | ||
400.0 °C | 18.8 W/(m·K) | ||
500.0 °C | 20 - 20.5 W/(m·K) | ||
600.0 °C | 22.6 W/(m·K) | ||
700.0 °C | 24.5 W/(m·K) | ||
800.0 °C | 26.4 W/(m·K) | ||
900.0 °C | 28.1 W/(m·K) | ||
1000.0 °C | 29.9 W/(m·K) | ||
Electrical
| Property | Temperature | Value |
|---|---|---|
Electrical resistivity | 20.0 °C | 1.09E-6 Ω·m |
100.0 °C | 1.1E-6 Ω·m | |
200.0 °C | 1.12E-6 Ω·m | |
300.0 °C | 1.15E-6 Ω·m | |
400.0 °C | 1.17E-6 Ω·m | |
500.0 °C | 1.17E-6 Ω·m | |
600.0 °C | 1.15E-6 Ω·m | |
700.0 °C | 1.15E-6 Ω·m | |
800.0 °C | 1.15E-6 Ω·m | |
900.0 °C | 1.15E-6 Ω·m | |
1000.0 °C | 1.16E-6 Ω·m | |
Chemical properties
| Property | Value |
|---|---|
Aluminium | 0.3 % |
Carbon | 0.08 - 0.15 % |
Chromium | 18 - 21 % |
Cobalt | 5 % |
Copper | 0.5 % |
Iron | 5 % |
Manganese | 1 % |
Nickel | 65.4 % |
Phosphorus | 0.02 % |
Silicon | 1 % |
Sulfur | 0.015 % |
Titanium | 0.2 - 0.6 % |
Metal
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