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INCONEL X750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chromium alloy used for its corrosion and oxidation resistance and high strength at temperatures to 1300°F. Although much of the effect of precipitation hardening is lost with increasing temperature over 1300°F, heat-treated material has useful strength up to 1800°F. Alloy X-750 also has excellent properties down to cryogenic temperatures.
In gas turbines, it is used for rotor blades and wheels, bolts, and other structural members. INCONEL X-750 is used extensively in rocket engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems. Large pressure vessels are formed from INCONEL X-750. Other applications are heat-treating fixtures, forming tools, extrusion dies, and test machine grips. For springs and fasteners, INCONEL alloy X-750 is used from sub-zero to 1200°F.
Common Trade Names :
- • ATI X-750
- • Inconel X750
- • Alloy X 750
Inventory of Inonel X-750 Wire:
- Inventory of Inonel X-750 Wire:
• Sizes – 1 mm to 10 mm - • Condition – Spring Hard
Chemical Composition of Inconel X-750 :
| Element | Min | Max |
| Carbon | — | 0.08 |
| Manganese | — | 1.00 |
| Silicon | — | 0.50 |
| Sulfur | — | 0.01 |
| Nickel + Cobalt | 70.0 min | — |
| Chromium | 14.00 | 17.00 |
| Iron | 5.00 | 9.00 |
| Aluminum | 0.40 | 1.00 |
| Titanium | 2.25 | 2.75 |
| Copper | — | 1.00 |
| Cb + Ta | 0.70 | 1.20 |