GH586 is Ni-Cr-Co precipitation hardening deformation of high temperature alloy, the use of temperature range -196 ℃ -800 ℃, and can be used in 850 ℃ for a short period of time; alloy to add aluminum, titanium elements to form γ 'precipitation strengthened phases, the addition of cobalt, chromium, tungsten and molybdenum elements for solid solution strengthening; alloy in the appropriate thermal processing and heat Treatment process conditions, precipitation along the grain boundaries of the fine granular carbide, play Supplementary strengthening effect; the alloy has high high-temperature strength, and has good resistance to oxidation, corrosion and ablation, as well as good heat processing and welding 

This alloy is a kind of high-performance high-temperature alloy turbine disk material developed by our country with independent intellectual property rights, and it has been used to make heat-resistant bearing parts for engines in the fields of aviation and aerospace, including the turbine rotor of liquid oxygen/kerosene rocket engine and the turbine rotor drop-forged parts of many types of aerospace engines, which are in good condition.