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Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components

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    Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
     
    Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
    • Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
    • Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
    • Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
    • Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers
    • Buy cheap Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components from wholesalers

    Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components

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    Brand Name : Torich
    Model Number : Alloy Steel Pipe Alloy 41
    Certification : CE PED
    Price : negotiable
    Payment Terms : L/C, T/T
    Supply Ability : 200 tons per year
    Delivery Time : 6-8 weeks
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    Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components

    Super Alloy Steel Pipe Precipitation Hardening Alloy 41 For Engine Components


    Alloy Steel Pipe Alloy 41 precipitation hardening Nickel-Base Superalloy


    Alloy41 is a precipitation hardening Nickel-Base Superalloy, and it has higher tensile and lasting creep strength and good oxidation resistance within the temperature range of 650~950℃. Since the alloy of aluminum, titanium, molybdenum content is high, the ingot blooming is more difficult, but the material after deformation has good ductility, which makes it easier to be cold formed or welded in the annealed state. However, the welded part is easy prone to cracking strain aging when heat treated. and precision castings, and is suitable for manufacturing under 870 ℃ demands with high strength and under 980 ℃ high temperature oxidation of aviation and aerospace engine components.


    Standard: GB/T14992,GB/T14993


    Chemical Composition of Alloy 41:


    Chemical Composition (%)
    CCrNiCoMoTiFeZrCuBMnAlSiPS
    0.06-0.1218.0-20.0Margin10.0-12.09.00-10.503.0-3.50≤5≤0.07≤0.5

    0.003-

    0.010

    ≤0.50

    1.40-

    1.80

    ≤0.5≤0.015≤0.015

    Physical Properties of Alloy 41:


    ρ: 8.27g/cm³


    Therming Conductivity:


    therming conductivity
    Temperature/℃100200300400500600700800900
    λ/(w/(m.℃))8.3710.4712.5615.0717.172021.3523.4525.96

    Coefficient of thermal expansion:


    coefficient of thermal expansion
    Temperature/℃20-10020-20020-30020-40020-50020-60020-70020-80020-900
    α1/10-6℃-110.5411.6912.2412.7813.0813.4814.2114.9715.91

    Mechanical Properties of Alloy 41:


    Mechanical Properties
    FormHeat TreatmentTensile Strength
    σb/MPa
    Yield Strength
    σp0.2/Mpa
    Elongation after fracture
    σ5 /%
    Shrink rate
    Ψ/%
    Hardness
    HBS
    ring unite/barsolid solution+aging≥835≥620≥12≥15≥283
    fastenersolid solution+aging≥1070-≥8≥10-








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