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    UNS N07718, Chemistry, Designators, and Bolting Standards

    Inconel 718 / Alloy 718 / W.Nr 2.4668 / Nickel-Chromium-Niobium Precipitation-Hardening Superalloy

    UNS N07718 is the Unified Numbering System designator for the precipitation-hardening nickel-chromium-niobium superalloy commercially branded Inconel 718 by Special Metals and Alloy 718 by other producers. In Europe the equivalent designator is Werkstoff Nr. 2.4668. The same alloy is the subject of ASTM A1014 for bolting components, ASTM B637 for bar and forging stock, SAE AMS 5662 (solution heat treated) and AMS 5663 (solution + precipitation hardened) for aerospace procurement, and ASME PVP Code Case 1993-7 for pressure-vessel service.

    For Inconel 718 bolting: request a quote at +91-22-66157017, WhatsApp +91-22-66157017, or info@torqbolt.com. MTC 3.1 / 3.2 certifications, NACE MR0175 compliance, ITAR-controlled aerospace orders supported.

    What is UNS N07718

    UNS N07718 sits in the SAE/ASTM Unified Numbering System under the "N" prefix for nickel and nickel alloys. The five-digit code identifies a single specific nickel-chromium-niobium chemistry developed in the 1960s by INCO (now Special Metals) for high-temperature aerospace bolting, gas-turbine compressor discs, and oilfield downhole tools. The alloy strengthens through precipitation of γ″ (gamma double-prime, Ni₃Nb) and γ′ (gamma prime, Ni₃(Al,Ti)) phases during age hardening, giving 185 ksi tensile strength at room temperature that retains 145 ksi at 1200 °F (650 °C).

    UNS N07718 Chemistry (per ASTM A1014 Table 1)

    ElementComposition (mass %)
    Nickel + Cobalt50.0 – 55.0
    Chromium17.0 – 21.0
    Molybdenum2.80 – 3.30
    Niobium + Tantalum4.75 – 5.50
    Titanium0.65 – 1.15
    Aluminum0.20 – 0.80
    Cobalt, max1.0
    Carbon, max0.08
    IronRemainder

    Niobium content is the discriminating element: it pushes UNS N07718 into the γ″-strengthened family vs UNS N06625 (Inconel 625) which is primarily solid-solution strengthened. The deliberately slow γ″ precipitation kinetics give UNS N07718 the best weldability of any precipitation-hardening superalloy.

    Mechanical Properties (Age-Hardened Condition)

    PropertyRoom Temperature1200 °F (650 °C)
    Tensile strength, min185 ksi (1275 MPa)145 ksi (1000 MPa)
    0.2% yield strength, min150 ksi (1035 MPa)125 ksi (860 MPa)
    Elongation, min12 %12 %
    Reduction of area, min15 %15 %
    Brinell hardness331 – 444 HBW-
    Stress rupture (100 ksi)-23 hours minimum

    Standards That Govern UNS N07718

    StandardProduct Form / Scope
    ASTM A1014 / A1014MBolting components: bolts, studs, screws (this site)
    ASTM B637Bar, forgings, and forging stock for elevated-temperature service
    SAE AMS 5662Aerospace bar & forging, solution heat treated
    SAE AMS 5663Aerospace bar & forging, solution + age hardened (final bolt condition)
    SAE AMS 5664Aerospace bar & forging, higher-strength solution + age hardened
    SAE AMS 5596Sheet, strip, and plate, solution treated
    SAE AMS 5597Sheet, strip, and plate, age hardened
    SAE AS 7467Aerospace bolts / screws, 185 ksi tensile, stress-rupture rated
    MS14181 / AS3418 / NAS1351Mil-Spec aerospace bolt part numbers in UNS N07718
    ASME PVP Code Case 1993-7Pressure-vessel code case authorizing UNS N07718 bolting

    Where to Order UNS N07718 Bolting

    For finished bolting in UNS N07718 / Inconel 718, browse the ASME B18 dimensional families covered on this site: