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LJ
GH3625 is a solid solution strengthened nickel-based deformed superalloy with molybdenum and niobium as the main strengthening elements. It has excellent corrosion resistance and oxidation resistance, good tensile properties and fatigue properties from low temperature to 980°C. It can be widely used in manufacturing aerospace engine parts, aerospace structural components and chemical equipment. The alloy has good processing and welding properties and can be supplied in a variety of plates, rods, tubes, wires, strips and forgings.
Chemical Composition(%)
| C | Si | Mn | P | S | Cr | Ni |
| ≤ 0.10 | ≤ 0.50 | ≤ 0.50 | ≤ 0.015 | ≤ 0.015 | 20.0-23.0 | Bal |
| Mo | Cu | Al | Ti | Fe | Co | |
| 8.0-10.0 | ≤ 0.07 | ≤ 0.40 | ≤ 0.40 | ≤ 5.00 | ≤ 1.00 |
Mechanical Property
| Tensile Strength σb/MPa | Yield Strength σp0.2/MPa | Elongation σ5 /% | Hardness HBS |
| 830 | 410 | 30 | ≤290 |
GH3625 is a solid solution strengthened nickel-based deformed superalloy with molybdenum and niobium as the main strengthening elements. It has excellent corrosion resistance and oxidation resistance, good tensile properties and fatigue properties from low temperature to 980°C. It can be widely used in manufacturing aerospace engine parts, aerospace structural components and chemical equipment. The alloy has good processing and welding properties and can be supplied in a variety of plates, rods, tubes, wires, strips and forgings.
Chemical Composition(%)
| C | Si | Mn | P | S | Cr | Ni |
| ≤ 0.10 | ≤ 0.50 | ≤ 0.50 | ≤ 0.015 | ≤ 0.015 | 20.0-23.0 | Bal |
| Mo | Cu | Al | Ti | Fe | Co | |
| 8.0-10.0 | ≤ 0.07 | ≤ 0.40 | ≤ 0.40 | ≤ 5.00 | ≤ 1.00 |
Mechanical Property
| Tensile Strength σb/MPa | Yield Strength σp0.2/MPa | Elongation σ5 /% | Hardness HBS |
| 830 | 410 | 30 | ≤290 |
