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High-Performance Nickel Alloy GH901 for Demanding Applications

Superalloy Series

Discover the exceptional capabilities of Nickel Alloy GH901, engineered to excel in the most demanding environments. Renowned for its outstanding resistance to high-temperature oxidation and corrosion, GH901 is the go-to choice for aerospace, gas turbine, and industrial applications requiring reliability and performance under extreme conditions. With its exceptional strength, toughness, and thermal stability, GH901 offers superior mechanical properties at elevated temperatures, ensuring reliable operation in critical components such as turbine blades, combustion chambers, and exhaust systems. Trust GH901 to deliver unparalleled performance and durability in your most challenging applications, providing peace of mind and reliability when it matters most.

    CHEMICAL COMPOSITION

    ERAUM

    %

    C

    Cr

    Ni

    Mo

    Al

    Ti

    Fe

    B

    Mn

    Si

    P

    S

    Cu

    Bi

    Pb

    GH901

    MIN

    0.02

    11.0

    40.0

    5.0

    -

    2.8

    balance

    0.01

    -

    -

    -

    -

    -

    -

    -

    MAX

    0.06

    14.0

    45.0

    6.5

    0.30

    3.1

    balance

    0.02

    0.5

    0.4

    0.02

    0.008

    0.2

    0.0001

    0.001

    Physical Properties

    density

    Melting temperature range

    8.21g/cm3

    1360℃

    Product FEATURE

    GH901 is an austenitic age-hardening alloy based on Fe-43Ni-12Cr, adding titanium, aluminum and other strengthening elements, and contains a trace of boron and low carbon, by the sub-stable γ [Ni3 (Ti, Al)] phase dispersion strengthening, a small amount of aluminum can inhibit γ to the conversion of η-Ni3Ti phase. The alloy has high yield strength and endurance strength below 650℃, good oxidation resistance below 760℃, and stable organization for long-term use.

    Product application

    This alloy is a mature alloy developed in the early days and is widely used in the manufacture of rotating disk parts (turbine disks, compressor disks, journals, etc.), static structural parts, turbine outer rings, fasteners and other parts of aviation and ground gas turbine engines operating below 650°C. The alloy is widely used in the manufacture of gas turbine engines.

    Product Display

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