Chemical Composition (wt.%): Element Content Ni 50-55 Cr 17-21 Fe Balance Mo 2.8-3.3 Nb+Ta 4.75-5.5 Ti 0.65-1.15 Al 0.2-0.8

Mechanical Properties: Property Typical Value Tensile Strength ≥1240 MPa Yield Strength ≥1035 MPa Elongation ≥12%

Applications: Aircraft turbine engines Rocket engines Oil and gas equipment Nuclear components

Chemical Composition (wt.%): Element Content Ni 50-55 Cr 17-21 Fe Balance Mo 2.8-3.3 Nb+Ta 4.75-5.5 Ti 0.65-1.15 Al 0.2-0.8

Mechanical Properties: Property Typical Value Tensile Strength ≥1240 MPa Yield Strength ≥1035 MPa Elongation ≥12%

Applications: Aircraft turbine engines Rocket engines Oil and gas equipment Nuclear components

Alloy 718/UNS N07718

Grade: Inconel 718/UNS N07718/Alloy 718/Nickel Alloy 718/W.Nr. 2.4668/NiCr19Fe19Nb5Mo3/GH4169

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 718 is one of the most widely used nickel-based superalloys. It combines high strength, excellent fatigue resistance, corrosion resistance and creep performance up to approximately 700°C. It is widely used in aerospace and energy industries.

Chemical Composition (wt.%):