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UNS N07718
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UNS N07718

Inconel 718 is a precipitation-hardened nickel-chromium-iron superalloy renowned for its high-temperature strength, corrosion resistance, and excellent processability. Operating effectively from -253°C to 700°C (short-term up to 800°C), it is widely used in aerospace, energy, and chemical industries.

    Inconel 718 Nickel-Based Superalloy: Global Standards, Performance Comparison & Key Properties
    Overview

     

     

    904 5

    Inconel 718 is a precipitation-hardened nickel-chromium-iron superalloy renowned for its high-temperature strength, corrosion resistance, and excellent processability. Operating effectively from -253°C to 700°C (short-term up to 800°C), it is widely used in aerospace, energy, and chemical industries.

     

    Key Properties

     

     

    High-Temperature Performance

    Ultimate Tensile Strength: 965 MPa (room temperature), maintaining ~690 MPa at 650°C.

    Oxidation Resistance: Superior stability under 1000°C, with exceptional creep and fatigue resistance.

    01

    Corrosion Resistance

    Resists acids, alkalis, salt solutions, and stress corrosion cracking.

    02

    Machining & Welding

    Compatible with TIG, MIG, and plasma welding without post-weld cracking.

    Requires solution treatment (980-1080°C) and aging (720-760°C) for optimal properties.

    03

    Cryogenic Performance

    Retains toughness at -253°C, ideal for liquid hydrogen/oxygen storage systems.

    04

    Physical Properties

    Density: 8.19-8.24 g/cm³; Melting Point: 1260-1383°C; Low magnetic permeability.

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    Performance vs. Competing Alloys

     

     

    Alloy

    Advantages

    Limitations

    Inconel 625

    Better corrosion resistance

    Lower high-temperature strength

    Haynes 282

    Higher thermal stability (up to 870°C)

    Complex processing, high cost

    Waspaloy

    Superior creep resistance (>800°C)

    Poor weldability

     

    Note: Inconel 718 excels in balanced performance for applications requiring both strength and manufacturability.

     

    Applications

     

     

    Aerospace

    Turbine blades, combustion chambers, rocket fuel ducts.

    01

    Energy

    Nuclear reactor components, gas turbine parts.

    02

    Chemical Processing

    High-temperature reactors, corrosion-resistant piping.

    03

    Medical Devices

    Implants and surgical tools (excellent biocompatibility).

    04

     

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    Global Material Standards

     

     

    Country/Standard

    Designation

    China

    GH4169

    USA

    UNS N07718

    Europe

    W.Nr. 2.4668

    France

    NC19FeNb

    Germany

    NiCr19Fe19Nb5

    UK

    NA51

    ISO

    NiCr19Nb5Mo3

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