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GH5605


GH5605 is a Co-Cr-Ni based solid solution strengthened deformed superalloy with service temperature below 1000 ℃. Cobalt-based superalloy GH5605 is a cobalt-based alloy strengthened by 20% Cr and 15% W (mass percentage) solid solution. It has medium endurance and creep strength below 815 ℃, excellent oxidation resistance below 1090 ℃, and satisfactory processing properties such as molding and welding. It is the key material of aviation engine, rocket engine, naval ship and industrial gas turbine.

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