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Inconel 718 (Nickel Superalloy)

Metals
Inconel718SuperalloyAerospace

Precipitation-hardened nickel-chromium superalloy for high-temperature service up to 700 °C.

Inconel 718 is a nickel-chromium superalloy that retains strength at elevated temperatures and resists corrosion in harsh chemical environments. Standard for jet-engine components, turbocharger wheels, and oilfield downhole tools.

Mechanical and physical properties

PropertyValue
Tensile strength1240 MPa
Yield strength1035 MPa
Elongation at break12%
Density8.19 g/cm³
Modulus200 GPa
Max service temperature700 °C
Machinability ratingDifficult
Cost and lead time

Inconel 718 stock is expensive and machining is slow. Use only when temperature, fatigue, or corrosion demand it — not as a generic 'high-strength' alternative to steel.

Typical applications

  • Jet engine combustor and turbine components.
  • Turbocharger and exhaust parts.
  • Oilfield and downhole tools.
  • Cryogenic structural fittings.
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