Inconel 718+(Ni-Cr-Co-Nb-Mo-W)


1. Introduce

– Polycrystalline precipitation hardening nickel-based superalloy for air engine disk applications

– Alloy designed to overcome the limitations of Inconel 718 and meet the enhanced operating conditions of jet engines

– Alloys designed to have the high temperature performance and thermal stability of Waspaloy alloys while maintaining the machining characteristics of Inconel 718

– Superior machining, formability, wear resistance, and weld crack resistance compared to Waspaloy and other high-temperature nickel-based alloys
→ A promising replacement for γ’ strengthened alloys such as Waspaloy or Udimet 720

– Typically applied to parts requiring creep and stress fracture resistance to 760°C and oxidation resistance to 982°C

– UNS N07818

* Inconel 718+ vs Inconel 718

– Inconel 718 Limitations: Lack of microstructural thermal stability above 650℃ due to γ” phase transformation at high temperatures

– The chemical composition of Inconel 718+ adds alloying elements (Co and Al) that promote precipitation of γ” phase instead of the unstable γ” phase

– Inconel 718+ : Can be operated at 55℃ higher temperature than Inconel 718

    * Inconel

    1. Features
      – Resists oxidation and submersion in oxidizing and sulfurizing atmospheres above 900℃
      – Non-corrosive to organic and salt solutions
      – Excellent mechanical properties such as tensile and yield strength up to about 600℃
    2. Applications
      – High temperature heat resistant equipment(Heat treatment furnace, boiler, jet engine parts, electric heater parts)
    3. Types
      – Incoenl 600/601, Inconel 625, Inconel 690, Inconel 718, Inconel 718+, Inconel X-750, etc.

    * Precipitation hardening Ni-based superalloys

    – Most nickel-based superalloys are strengthened by precipitation of intermetallic compounds, primarily within the austenitic face cubic (FCC) base

    – This is accomplished with elements such as Al, Ti, Nb, etc.

    Strenthening PhaseType
    γ’ strengthened nickel-based superalloysInconel 718+, Waspaloy, Astroloy, U-700, U-720
    γ” Reinforced nickel-based superalloysInconel 718
    γ’ and γ” strengthened superalloysInconel 706, Inconel 909

    * UNS

    1. Abbreviation for Unified Numbering Systems for Metals and Alloys
    2. Unified unique numbering system for metals and alloys
    3. A representative number that is compatible with metals and alloys defined in many material-related codes such as ASTM, AISI, ASME, AWS, etc.

    * N : Nickel and Nickel Alloys

    * UNS N07818 : 07XXX : Chromium(Precipitation-hardenable alloy)

    2. Property

    – Excellent high temperature properties, processability, moldability, wear resistance, and crack resistance

    – Improved temperature performance

    ElementImpact
    CrProvides corrosion resistance, oxidation resistance
    CoHighly reinforced element, provides strength and creep properties
    NbHighly strengthened element, provides high temperature strength
    MoHighly strengthened element, provides high temperature oxidation resistance, cryogenic oxidation resistance, and weldability
    WHighly strengthening element, provides high temperature creep properties

    [Inconel 718+ Chemical Composition (%)]

    NiCrFeCAl
    44.92 ~ 56.7917.00 ~ 21.008.00 ~ 10.000.01 ~ 0.051.20 ~ 1.70
    TiCuSiMnMo
    0.50 ~ 1.00Max. 0.30Max. 0.35Max. 0.352.50 ~ 3.10
    CoNbWPB
    8.00 ~ 10.005.20 ~ 5.800.80 ~ 1.40Max. 0.02Max. 0.01

    [Inconel 718+ Mechanical Properties]

    Tensile Strength
    (Mpa)
    Yield Strength
    (Mpa)
    Elongation
    (%)
    1170117025

    [Inconel 718+ Physical Properties]

    Density
    (g/㎤)
    Melting Range
    (℃)
    Curie Temperature
    (℃)
    8.251260 ~ 1343-113

    3. Standard & Specification

    – Specification : UNS N07818

    4. Available Form

    – Bar, Rod

    – Plate, Sheet, Strip

    – Wire

    – Forgings, Billets

    5. Application & Product

    – Aerospace

    ApplicationProduct
    AerospaceFasteners, Blades, Aircraft Engine Disks, Gas Turbine Engine Components, Turbine Casings, Combustors

    (1) Fasteners / (2) Blades / (3) Turbine Cases / (4) Combustors

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