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GH4080A


GH4080A alloy is formed by adding aluminum and titanium with nickel-chromium as matrix γ′ The phase dispersion strengthened superalloy, with the exception of slightly higher aluminum content, is similar to GH4033, with a service temperature of 700~800 ℃ and good creep resistance and oxidation resistance between 650~850 ℃. The alloy has good cold and hot working properties. The alloy has been used to manufacture rotor blades, guide vane supports, sector mounting rings, bolts, blade lock plates and other parts of aero-engines.

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