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  • C4

    C4 is a nickel-chromium-molybdenum alloy engineered to perform under high-temperature conditions.

    C4 Overview

    Alloy C4 is a nickel-chromium-molybdenum alloy engineered to perform under high-temperature conditions, particularly in situations where weld design leads to unavoidable heat concentration. It offers comparable resistance to general corrosion, localized corrosion, and stress corrosion cracking as Alloy C276. The alloy’s high chromium and molybdenum content provides strong protection against both oxidizing and non-oxidizing acids, and it resists pitting and crevice corrosion in chloride-rich and halide-containing environments. Like many nickel-based alloys, Alloy C-4 is known for its ductility and ease of fabrication and welding.

    Aleación

    C4 Composition

     crMesFeCSiCoMinnesotaPAGStiNi
    Min %1414bala
    Max %181730.0150.08210.040.030.7
    Aeroespacial

    Designations and Specifications

    Designations

    • W.NR 2.4610
    • UNS N06455

     

    Specifications

    • ASTM B574

    Aplicaciones

    Common C4 applications include:

    • Procesamiento químico
    • muelles
    • Composition

    Fuerza de Tensión

    Condition N/mm² KSI
    Annealed <1100 <159
    ConditionAs Drawn
    N/mm²KSI
    Spring Temper1300 – 1700189 – 247
    Información del Producto
    Opciones de embalaje
    • Bobinas
    • Carretes
    • Bars/Cut Lengths
    • Embalaje personalizado disponible

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