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GH4049


GH4049 is a Ni-Co-Cr base precipitation hardening deformation superalloy with service temperature less than 950 ℃. The alloy has been used to manufacture plate structural parts such as aeroengine combustion chamber and afterburner cylinder, and other high-temperature parts, and the service temperature is less than 950 ℃. The alloy has good oxidation resistance below 1000 ℃ and high temperature strength below 950 ℃. It is suitable for manufacturing gas turbine working blades with operating temperature between 850 ℃ and 950 ℃.

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