GH3536 Alloy

GH3536 alloy is a nickel based high-temperature alloy with high iron content, mainly strengthened by solid solution of chromium and molybdenum. It has good oxidation resistance and corrosion resistance, with moderate endurance and creep strength below 900 ℃, and good cold and hot working formability and welding performance.

Suitable for manufacturing combustion chamber components and other high-temperature components of aircraft engines, with long-term use below 900 ℃ and short-term working temperature reaching 1080 ℃. An alloy that can withstand certain stresses and has oxidation or corrosion resistance at high temperatures of 600-1200 ℃.

According to the matrix elements, it can be mainly divided into iron-based high-temperature alloys, nickel based high-temperature alloys, and cobalt based high-temperature alloys.

According to the preparation process, it can be divided into deformed high-temperature alloys, cast high-temperature alloys, and powder metallurgy high-temperature alloys.

According to strengthening methods, there are solid solution strengthening, precipitation strengthening, oxide dispersion strengthening, and fiber strengthening (see strengthening of metals).

GH3536 Chemical Element Content (%)

Our services 

We can cut and bend steel plate according to customer's requriement or drawing, packaging according to customers' request.

Application 

Industrial and aviation steam turbines (combustion chamber, rectifier, structural cover)

Industrial furnace components, support rollers, grating plates, ribbons, and radiation tubes

Spiral tubes in petrochemical furnaces

High temperature gas cooled nuclear reactors