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 wnr 24668-0

Nickel

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Inconel 718 (Alloy 718) Nickel Alloy — UNS N07718 / W.Nr. 2.4668

Age-hardenable Ni-Cr-Fe superalloy with outstanding tensile, fatigue, creep & rupture strength from -423°F to 1300°F.

Inconel® 718 (Alloy 718) — UNS N07718 / W.Nr. 2.4668

Inconel 718 (also known as Alloy 718) is a high-strength, corrosion-resistant, age-hardenable nickel-chromium-iron-molybdenum alloy designed for demanding service from -423°F to 1300°F. It is well known for excellent tensile strength, fatigue resistance, creep strength, and rupture strength at elevated temperatures. In addition, Alloy 718 provides strong resistance to oxidation and aqueous corrosion, making it a reliable choice for critical components in harsh industrial environments.

Service Temperature:-423°F to 1300°F | Website:www.voyagemetal.com | Email:[email protected]

Key Advantages

  • Age-hardenable alloy offering high strength and excellent stability at elevated temperatures
  • Strong fatigue, creep, and rupture strength for demanding rotating and pressure-bearing components
  • Excellent resistance to corrosion, oxidation, and aqueous corrosion
  • Widely accepted in critical industries with mature standards and supply forms

Typical Applications

Inconel 718 is used across multiple industries where both strength and corrosion resistance are required. Common application scenarios include:

Industry Typical Components
Aerospace Turbine discs, compressor blades, critical aircraft engine parts
Gas Turbine Engines Turbine wheels, seals, combustion chamber hardware
Oil & Gas Downhole tools, wellhead components, sour-service equipment
Nuclear Reactor-related components requiring long-term strength & corrosion resistance
Chemical Processing Valves, pumps, fasteners for hot & corrosive media
Automotive / Industrial Turbines Turbocharger rotors, exhaust components, high-temperature hardware

Inconel® 718 (Alloy 718) — UNS N07718 / W.Nr. 2.4668

Technical Data

Chemical Composition (Typical, %)

Element Content
Nickel (Ni) 50–55%
Chromium (Cr) 17–21%
Iron (Fe) Remainder
Niobium + Tantalum (Nb+Ta) 4.75–5.50%
Molybdenum (Mo) 2.8–3.3%
Titanium (Ti) 0.65–1.15%
Aluminum (Al) 0.2–0.8%
Cobalt (Co) 1.0% max
Manganese (Mn) 0.35% max
Silicon (Si) 0.35% max
Phosphorus (P) 0.015% max
Sulfur (S) 0.015% max
Carbon (C) 0.08% max
Boron (B) 0.006% max
Copper (Cu) 0.3% max

Physical Properties

Property Value
Density (Annealed) 0.296 lb/in³
Density (Annealed & Aged) 0.297 lb/in³
Melting Range 2300–2437°F (1260–1336°C)
Specific Heat @ 70°F (21°C) 0.104 Btu/lb°F (435 J/kg°C)
Curie Temperature (Annealed) < -320°F (< -196°C)
Curie Temperature (Annealed & Aged) -170°F (-112°C)
Permeability @ 200 Oe & 70°F (Annealed) 1.0013
Permeability @ 200 Oe & 70°F (Annealed & Aged) 1.0011

Mechanical Properties (Typical at 20°C / 68°F)

Yield Strength (Rp0.2) Tensile Strength (Rm) Elongation (A) Reduction of Area (Z)
1030 MPa (149.4 ksi) 1280 MPa (185.6 ksi) 12% 15%

Available Product Forms & Standards

Standard product forms include pipe, tube, sheet, strip, plate, round bar, flat bar, forging stock, hexagon, and wire. Supply can be provided with material certification (MTC) upon request.

Product Category Common Standards
Bar, Rod, Wire & Forgings ASTM B637 / ASME SB637
Seamless Pipe & Tube ASTM B983 / ASME SB983
Plate, Sheet & Strip ASTM B670 / ASME SB670; ASTM B906 / ASME SB906

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Note: Typical values shown are for reference. Final supply can be provided to your required specification and heat-treatment condition.

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