This age hardenable nickel base super alloy has very good strength in temperatures up to about 980°C (1800°F). It’s strength is generally comparable to that of Rene 41 and is generally superior to that of Alloy 718 at temperatures exceeding 650 – 705°C (1200 – 1300°F). Applications include: Gas turbine engine parts, aerospace components, springs and fasteners.
| Composição química aproximada (%) |
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| Densidade (g/cm3) |
8.16 | Ponto de fusão (°C) |
1330°C | ||
| Coeficiente de dilatação | 12.2 µ m/m °C at 21 - 93°C | ||||
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| Tracção aprox. | Solution Annealed | Stabilize at 843°C
(1550°F) for 4 hours and air cool and age harden at 760°C (1400°F) for 16 hours and air cool |
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| Spring Temper | Anneal at 1050°C
(1920°F) for 4 hours and air cool and stabilize at 843°C (1550°F) for 24 hours and air cool and age harden at 760°C (1400°F) for 16 hours and air cool |
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| Avvicinarsi Estensibile | Solution Annealed | 800 - 1100 N/mm2 | |||
| Solution Annealed + Aged | 1300 - 1500 N/mm2 | ||||
| Spring Temper | 1300 - 1600 N/mm2 | ||||
| Spring Temper + Annealed + Aged |
1300 - 1500 N/mm2 | ||||
| Módulo de Young | 211 kN/mm2 | ||||
| Temperatura de trabalho aproximada | Up to 550°C dipendere dal progetto primaverile e le condizioni operative | ||||
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