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GH3536


GH3536 alloy has good oxidation resistance and corrosion resistance, moderate endurance and creep strength below 900 ℃, and good cold and hot working formability and weldability. It is suitable for manufacturing combustion chamber components and other high-temperature components of aero-engines. It can be used for a long time below 900 ℃, and its short-term working temperature can reach 1080 ℃. Alloys that can bear certain stress and have oxidation or corrosion resistance at 600~1200 ℃. According to the matrix elements, it can be divided into iron-based superalloy, nickel-based superalloy and cobalt-based superalloy; According to the preparation process, it can be divided into deformed superalloy, cast superalloy and powder metallurgy superalloy. According to the strengthening methods, there are solid solution strengthening, precipitation strengthening, oxide dispersion strengthening and fiber strengthening (see metal strengthening). High temperature alloys are mainly used to manufacture high temperature components such as turbine blades, guide vanes, turbine discs, high pressure compressor discs and combustion chambers of aviation, naval and industrial gas turbines; It can also be used to manufacture energy conversion devices such as aerospace vehicles, rocket engines, nuclear reactors, petrochemical equipment and coal conversion.

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