Inconel X-750 is a superalloy composed of nickel with additions of Ni3 (Al, Ti, Nb) that is heat-treated for strength and oxidation resistance up to 980℃, offering superior corrosion protection and superior tensile strength at temperatures up to 800℃.
Inconel X-750 is a superalloy composed of nickel with additions of Ni3 (Al, Ti, Nb) that is heat-treated for strength and oxidation resistance up to 980℃, offering superior corrosion protection and superior tensile strength at temperatures up to 800℃.
| Chemical Composition | 70Ni-15Cr-6Fe-2.5Ti-0.6Al-1Nb-0.02C |
| Physical Property | • Density: 8.28 g/cm³ • Tensile Strength: 1120 MPa • Yield Strength: 850 MPa • Elongation: 22% • Reduction of Area: 30% |
| Stock & Dimensions | Our warehouse has a large number of stock to provide you with a variety of products in different sizes, and can also customize the size according to your needs. • Bar: 0.5~600mm Diameter • Coil: 0.5~150mm Thick • Plate: 0.5~200mm Thick • Pipe: 6~630mm External Diameter; 0.5~40mm Wall Tick • Available in specific sizes |
| Product Forms | We provide you with a variety of product forms, including but not limited to: • Bar/Rod • Pipe/Tube • Coil/Strip • Plate/Sheet/Circle • Wire • Fitting (Flange, Elbow, Tee...) • Customize |
Essential details
Inconel alloy X-750 (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 termperatures.
Application:
- Bellows
- Gas turbine
- Rotor blades
- Rocket engine chambers
- Springs
- Fasteners
