Chemical Composition (wt.%): Element Content Ni Balance Cr 14.0-17.0 Fe 5.0-9.0 Ti 1.8-2.6 Al 1.0-1.7 Nb 0.7-1.2

Mechanical Properties: Property Typical Value Tensile Strength ≈1000 MPa Yield Strength ≈700 MPa Creep Strength High temperature resistant

Applications: Automotive turbocharger components Gas turbine parts High temperature fasteners

Chemical Composition (wt.%): Element Content Ni Balance Cr 14.0-17.0 Fe 5.0-9.0 Ti 1.8-2.6 Al 1.0-1.7 Nb 0.7-1.2

Mechanical Properties: Property Typical Value Tensile Strength ≈1000 MPa Yield Strength ≈700 MPa Creep Strength High temperature resistant

Applications: Automotive turbocharger components Gas turbine parts High temperature fasteners

Alloy 751 / UNS N07751

Grade: Inconel 751/UNS N07751/Alloy 751/Nickel Alloy 751/W.Nr. 2.4694/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 751 is a nickel-chromium alloy modified from Inconel 750 with increased aluminum content for improved gamma-prime strengthening. It provides excellent creep rupture strength and oxidation resistance at elevated temperatures, especially for exhaust and turbine applications.

Chemical Composition (wt.%):