Chemical Composition (wt.%): Element Content Ni ≥70 Cr 14.0-17.0 Fe 5.0-9.0 Ti 2.25-2.75 Al 0.4-1.0 Nb+Ta 0.7-1.2

Mechanical Properties: Property Typical Value Tensile Strength ≥1035 MPa Yield Strength ≥690 MPa Elongation ≥12%

Applications: Aircraft engine components High temperature springs Nuclear reactor components Bolting applications

Chemical Composition (wt.%): Element Content Ni ≥70 Cr 14.0-17.0 Fe 5.0-9.0 Ti 2.25-2.75 Al 0.4-1.0 Nb+Ta 0.7-1.2

Mechanical Properties: Property Typical Value Tensile Strength ≥1035 MPa Yield Strength ≥690 MPa Elongation ≥12%

Applications: Aircraft engine components High temperature springs Nuclear reactor components Bolting applications

Alloy X-750 / UNS N07750

Grade: Inconel X-750/UNS N07750/Inconel X750/Alloy X-750/Alloy X750/Nickel Alloy X750/Nickel Alloy X-750/Nicrofer 7016TiNb/W.Nr. 2.4669/NiCr15Fe7TiAl

Sheet/Plate: 0.3mm-150mm

Strip/Foil: 0.02mm-16mm

Pipe: 6mm*0.5mm-1200mm*100mm

Bar: Ф6mm – Ф600mm

Wire: Ф0.01mm – Ф6mm

Others: Forged Rings, Flanges, Elbows, Tees, Reducers etc.

Standard: ASTM/ASME/AMS

INCONEL X-750 is a precipitation-hardenable nickel-chromium alloy strengthened primarily by gamma-prime precipitation. It combines good corrosion resistance, oxidation resistance and high-temperature strength, making it widely used for springs, fasteners and aerospace components.

Chemical Composition (wt.%):