| INCONEL®
Alloy X-750 |
2.4669 |
| |
UNS N07750 |
A nickel-chromium alloy similar to INCONEL alloy 600 but made precipitation hardenable by additions of aluminum and titanium. It has good resistance to corrosion and oxidation along with high tensile and creep-rupture properties
at temperatures to 1300°F (700°C). Its excellent relaxation resistance is useful for high-temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.
|
| Limiting |
| Ni¹ |
min. |
70.0 |
% |
| Cr |
14.00 - 17.00 |
% |
| Fe |
5.00 - 9.00 |
% |
| Ti |
2.25 - 2.75 |
% |
| Nb² |
07.0 - 1.20 |
% |
| Al |
0.40 - 1.00 |
% |
| Mn |
max. |
1.00 |
% |
| Co³ |
max. |
1.00 |
% |
| Cu |
max. |
0.50 |
% |
| Si |
max. |
0.50 |
% |
| C |
max. |
0.08 |
% |
| S |
max. |
0.01 |
% |
| |
|
|
|
| ¹ Plus Co |
|
|
|
| ² Plus Ta |
|
|
|
| ³ If determined |
|
|
|
| Density |
| g/cm³ |
8.28 |
| lb/in³ |
0.299 |
| Downloads |
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Datasheet (will follow) |
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