GH2132 5188 High Temperature Alloy Pipe

GH2132 5188 high temperature alloy pipe

GH2132 is a Fe-25Ni-15Cr-based high-temperature alloy, which is comprehensively strengthened by adding molybdenum, titanium, aluminum, vanadium and trace amounts of boron. It has high yield strength, durability and creep strength below 650℃, and has good processing plasticity and satisfactory welding performance. It is suitable for manufacturing high-temperature load-bearing parts of aeroengines that work for a long time below 650°C, such as turbine discs, compressor discs, rotor blades and fasteners, etc. The alloy can produce deformed products of various shapes, such as discs, forgings, plates, rods, wires and rings, etc.
GH5188 is a solid solution reinforced cobalt-based superalloy with good high-temperature thermal strength and high-temperature oxidation resistance. It is one of the important industrial materials used in manufacturing aviation and is often used to prepare aerospace engine vortexes. High-temperature components such as plates, combustion chamber walls, outer walls, cooling rings, etc. The room temperature plasticity of high-temperature alloys is low, and its plastic forming process is a process at high temperatures. Due to the high-temperature deformation of gh5188 alloy, this has important guiding significance for the formulation of the forming process. This article proposes a constitutive equation describing the material flow characteristics that describes the high-temperature deformation behavior of GH 5188 alloy, thereby providing a theoretical basis for its thermal processing process.