Chemical Composition (wt.%): Element Content Ni Balance Cr 15.7-16.3 Co 8.0-9.0 Mo 1.5-2.0 Al 3.2-3.7 Ti 3.2-3.7 Nb 0.6-1.1

Mechanical Properties: Property Typical Value Tensile Strength ≈950 MPa Yield Strength ≈700 MPa Creep Resistance Excellent at 800-950°C

Applications: Gas turbine blades Industrial turbine vanes Aerospace engine hot section parts

Chemical Composition (wt.%): Element Content Ni Balance Cr 15.7-16.3 Co 8.0-9.0 Mo 1.5-2.0 Al 3.2-3.7 Ti 3.2-3.7 Nb 0.6-1.1

Mechanical Properties: Property Typical Value Tensile Strength ≈950 MPa Yield Strength ≈700 MPa Creep Resistance Excellent at 800-950°C

Applications: Gas turbine blades Industrial turbine vanes Aerospace engine hot section parts

Alloy 738LC / UNS N07138

Grade: Inconel 738LC/UNS R30783/Alloy 738LC/Nickel Alloy 738LC/IN738LC/Nickel Cast Superalloy 738LC

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 738LC is a cast nickel-based superalloy developed for high-temperature gas turbine applications. It provides excellent creep strength, oxidation resistance and thermal stability through gamma-prime precipitation strengthening, making it suitable for demanding turbine blade and vane components.

Chemical Composition (wt.%):