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LJ
GH2132 alloy 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. This alloy can produce various shape deformation products, such as: discs, forgings, plates, rods, wires and rings, etc.
Chemical Composition(%)
| C | Cr | Ni | Mo | Ti | Fe | V |
| ≤0.08 | 13.5~16.0 | 24.0~27.0 | 1.00~1.50 | 1.90~2.30 | Bal | 0.10~0.50 |
| B | Mn | Al | Si | P | S | |
| 0.001~0.010 | 1.00~2.00 | ≤0.35 | ≤1.00 | ≤0.030 | ≤0.020 |
GH2132 alloy 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. This alloy can produce various shape deformation products, such as: discs, forgings, plates, rods, wires and rings, etc.
Chemical Composition(%)
| C | Cr | Ni | Mo | Ti | Fe | V |
| ≤0.08 | 13.5~16.0 | 24.0~27.0 | 1.00~1.50 | 1.90~2.30 | Bal | 0.10~0.50 |
| B | Mn | Al | Si | P | S | |
| 0.001~0.010 | 1.00~2.00 | ≤0.35 | ≤1.00 | ≤0.030 | ≤0.020 |
