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Alloy 718: Premium Nickel-Chromium Alloy for High-Performance Applications

2.4668 (NiCr19NbMo) is a precipitation hardening nickel-chromium alloy that also contains additions of iron, niobium, molybdenum, aluminium and titanium, providing a unique combination of high strength and corrosion resistance together with excellent weldability. It shows the following features and properties:


  • Excellent tensile, fatigue, creep and rupture strengths across a wide temperature range from around -253ºC to 705ºC
  • Excellent oxidation resistance, up to temperatures of around 980ºC due to the high chromium content
  • Outstanding corrosion resistance in many environments including organic and inorganic acids, other than when strongly oxidising, hydrogen sulphide and sour gases
  • Especially resistant to chloride stress-corrosion cracking
  • Exceptional weldability
  • Properties

    General

    PropertyTemperatureValue

    Density

    23.0 °C

    8.22 g/cm³

    Mechanical

    PropertyTemperatureValue

    Elastic modulus

    23.0 °C

    204 GPa

    Elongation

    23.0 °C

    12 - 17 %

    Hardness, Brinell

    23.0 °C

    313 - 354 [-]

    Reduction of area

    23.0 °C

    15 %

    Tensile strength

    23.0 °C

    1034 - 1276 MPa

    Yield strength Rp0.2

    23.0 °C

    827 - 1034 MPa

    Thermal

    PropertyTemperatureValueComment

    Coefficient of thermal expansion

    23.0 °C

    1.35E-5 1/K

    Melting point

    1260 - 1335 °C

    Thermal conductivity

    23.0 °C

    14.2 W/(m·K)

    for 0-200°C

    Magnetic

    PropertyTemperatureValue

    Relative magnetic permeability

    23.0 °C

    1 [-]

    Chemical properties

    PropertyValue

    Aluminium

    0.5 %

    Chromium

    19 %

    Iron

    18 - 18.5 %

    Molybdenum

    3 %

    Nickel

    53 %

    Niobium

    5 %

    Titanium

    0.9 %

    Technological properties

    Property
    Application areas

    Offshore & marine: Fasteners, valves, choke stems, down-hole tooling, cryogenic storage tanks and pump bodies;Aerospace: Jet engine components, rocket motors and thrust reversers;Power generation: Nuclear reactor parts, gas turbine components, nuclear fuel element spacers, containment vessels and valves;Other: Hot extrusion tooling

    Corrosion properties

    Excellent corrosion resistance

    Hot forming

    It can be hot worked between 985-1150°C.


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