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GH2132 Nickel Alloy: Unmatched Performance in High-Temperature Environments

Superalloy Series

Experience unparalleled performance and durability with GH2132 Nickel Alloy. Engineered to excel in high-temperature environments, GH2132 offers exceptional strength, oxidation resistance, and thermal stability. With its superior creep and rupture properties, this nickel-based alloy is the perfect choice for demanding applications in aerospace, gas turbines, chemical processing, and beyond. Whether you're operating in extreme temperatures or corrosive atmospheres, GH2132 delivers reliability and longevity, ensuring optimal performance in the most challenging conditions. Trust GH2132 Nickel Alloy for your critical high-temperature applications and elevate your operations to new levels of efficiency and durability.

    CHEMICAL COMPOSITION

    ERAUM

    %

    C

    Cr

    Ni

    Mo

    Al

    Ti

    Fe

    B

    V

    Mn

    Si

    P

    S

    Cu

    GH2132

    MIN

    -

    13.5

    24

    -

    -

    1.75

    balance

    0.001

    0.1

    1

    -

    -

    -

    -

    MAX

    0.08

    16

    27

    0.4

    0.4

    2.35

    balance

    0.01

    0.5

    2

    1

    0.03

    0.02

    0.25

    Physical Properties

    density

    melting point

    Alloy state

    tensile strength

    yield strength

    Elongation

    Brinell hardness

    7.93g/cm³

    1364-1424℃

    Solid solution Treatment at 980°C

    Rm N/mm2

    Rp0.2 N/mm2

    A5%

    HRB

    630

    285

    45

    80


    EXECUTIVE STANDARD

    Product

    GB/T 14992

    Cold Drawn Bar

    GB/T 14994

    Hot Rolled Plate

    GB/T 14995

    Cold Rolled Plate

    GB/T 14996

    Aerospace Cold Drawn Bars

    GJB 2611A-2006

    Product FEATURE

    It is a high-temperature, high-strength, high-temperature oxidation-resistant alloy material. Below 650 ℃ has a high yield strength and lasting, creep strength and has a good processing plasticity and satisfactory welding performance.

    Product application

    It is mainly used for combustion chamber parts of turbine engines operating below 800°C and other high-temperature parts requiring oxidation resistance below 1100°C but carrying very small loads.

    Product Display

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