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  • A286

    Learn about our high-performance, age hardenable, Iron-Nickel-Chromium Alloy, A286.

    A286 Overview

    Alloy A286 is an age-hardenable iron-nickel-chromium alloy developed for use in environments that demand both high strength and reliable corrosion resistance at temperatures reaching up to 700°C (1290°F). Its robust mechanical properties make it well-suited for components in aircraft and industrial gas turbines. Additionally, it is commonly employed in the offshore oil and gas sector, as well as in fasteners and automotive engine parts exposed to elevated heat and stress conditions.

    Ageing process – heat treatment to be held 705 – 760 °C (1300 – 1400 °F) for 16 hours and then air cooled.

    Legierung

    A286 Composition

    C Mn Si P S Kr Ni Mo Ti B V Co Al Cu Pb Fe
    Min % 0,03 1 13.5 24 1 1.9 0,003 0.1 Bal
    Max % 0,08 2 0.5 0,02 0,015 16 27 1.5 2.3 0,01 0.5 1 0,35 0.5 0,005
    Luft- und Raumfahrt

    Designations and Specifications

    Designations

    • W.Nr 1.4944
    • W.Nr 1.4980
    • UNS S66286

     

    Specifications

    • AMS 5731
    • AMS 5734
    • AMS 5737
    • AMS 5853
    • ASTM A453
    • BS HR 52
    • BS HR 650
    • ISO 15156-3
    • NACE MR 0175

    Anwendungen

    Common A286 applications include:

    • Super Chargers
    • After Burner Parts
    • Verbindungselemente
    • Jet Engines

    Zerreißfestigkeit

    Condition Annealed After Ageing
    N/mm² KSI N/mm² KSI
    Annealed & Aged <750 <109 950 – 1300 138 – 188
    Condition As Drawn After Ageing
    N/mm² KSI N/mm² KSI
    Spring Temper & Aged 1050 – 1250 152 – 181 1200 – 1500 174 – 218
    Produktinformation
    Verpackungsoptionen
    • Spulen
    • Spulen
    • Bars/Cut Lengths
    • Kundenspezifische Verpackung verfügbar

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