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High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine

    Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
     
    Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers
    • Buy cheap High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine from wholesalers

    High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine

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    Brand Name : Victory
    Model Number : GH3128
    Certification : CE,ROHS,ISO 9001
    Price : Negotiable
    Payment Terms : L/C, T/T, Western Union, MoneyGram
    Supply Ability : 300 tons per month
    Delivery Time : 5-21 days
    • Product Details
    • Company Profile

    High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine

    Introduction:


    GH3128 (GH128) is a nickel-based alloy solid solution reinforced with tungsten and molybdenum and grain boundaries reinforced with boron, cerium and zirconium. It has high plasticity, high lasting creep strength, good oxidation resistance and stamping, welding and other properties. . Its comprehensive performance is better than similar nickel-based solid solution alloys such as GH3044 and GH3536. It is suitable for manufacturing combustion chamber flame tubes, afterburner casings, regulator plates and other high-temperature parts of aeroengines that operate at 950°C for a long time. The main products are cold-rolled sheets, and hot-rolled plates, bars, etc. can also be supplied. Forgings, wire and tubing.


    Parameter:


    Chemical Composition ( % )
    BrandCSiMnSPCrCoWMoTiAlFeNiother
    Less than
    GH31280.050.80.50.0130.01319~227.5~97.590.40.80.40.8≤2.0restB≤0.005
    Ce≤0.05
    Zr≤0.06

    The minimum mechanical properties of the alloy at room temperature
    Brandheat treatmenttensile strength
    RmN/mm²
    Yield strength
    Rp0.2N/mm2
    Elongation
    As%
    Brinell hardness
    HB
    Rockwell hardness
    HRC
    GH3128solid solution75040

    • Thermal conductivity
    θ/℃
    100
    200
    300
    400
    500
    600
    700
    800
    900
    950
    λ/(W/(m·C))
    11.30
    12.56
    14.24
    15.49
    16.75
    18.42
    19.68
    21.35
    23.02
    23.86

    • Linear expansion coefficient
    θ/℃
    18~100
    18~200
    18~300
    18~400
    18~500
    18~600
    18~700
    18~800
    18~900
    18~1000
    α/10-6C-1
    11.25
    11.86
    12.68
    12.80
    13.37
    13.68
    14.46
    15.19
    15.66
    15.29

    Characteristic:


    • High temperature strength: GH3128 wire has excellent high temperature strength and can maintain high mechanical properties in high temperature environments.
    • Antioxidant properties: It exhibits good antioxidant properties and can resist oxidation and corrosion at high temperatures.
    • Creep resistance: GH3128 wire has good creep resistance and can withstand long-term continuous loading at high temperatures without deformation.
    • Anti-corrosion properties: It has good anti-corrosion properties in many corrosive media, including acidic, alkaline and chloride environments.

    Specific application areas:


    1. Aeroengine combustion chamber flame tube, afterburner housing, regulator plate
    2. Structural parts of gas turbine combustion chamber
    3. Turbine engine combustion chamber parts
    4. Afterburner parts
    High Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft EngineHigh Temperature Alloy High Plasticity Wire GH3128 Wire In Aircraft Engine

    contact us

    email:victory@dlx-alloy.com

    Oem service:
    Welcome customized size
    We are experience factory for OEM&ODM service


    Process performance and requirements:


    The alloy has a single-phase austenite structure in the solid solution state and contains a small amount of fine and evenly distributed TiN and M6C.

    1. The furnace temperature for steel ingot forging should not be higher than 700°C, and the final forging temperature should be higher than 900°C.
    2. The average grain size of the alloy is closely related to the deformation degree and final forging temperature of the forging.
    3. Alloys can be welded by argon arc welding, spot welding, seam welding and other methods.

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