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A nickel-chromium-cobalt alloy that is precipitation hardenable and also contains a relatively high (7%) level of molybdenum for solid-solution strengthening. It has an exceptional combination of high-temperature strength, creep resistance, and ductility when welded. The alloy is especially suitable for welded sheet structures. Used in gas turbines for flame tubes and other components.
|
| Limiting |
| Ni |
balancet |
|
| Cr |
16.00 - 20.00 |
% |
| Co |
12.00 - 16.00 |
% |
| Mo |
5.00 - 9.00 |
% |
| Ti |
1.50 - 3.00 |
% |
| Al |
1.70 - 2.50 |
% |
| Fe |
max. |
1.00 |
% |
| Mn |
max. |
0.50 |
% |
| Si |
max. |
0.50 |
% |
| Cu |
max. |
0.20 |
% |
| Zr |
max. |
0.06 |
% |
| S |
max. |
0.015 |
% |
| B |
max. |
0.005 |
% |
| Density |
| g/cm³ |
8.21 |
| lb/in³ |
0.297 |
| Downloads |
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Datasheet (will follow) |
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