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LJ
GH141 is a high-temperature alloy of nickel-based deformation. Within 650-950 ° C, it has high stretching and long-lasting creep intensity and good antioxidant performance. Due to the high content of aluminum, titanium, and molybdenum in alloy, it is difficult to billet in ingots, but the deformation materials have a good plasticity. The varieties of alloys include thin plates, bands, silk, disk, ring parts, forged parts, rods, and precision castings. It is suitable for manufacturing aerospace engines parts with high-strength.
Chemical Composition(%)
| C | Cr | Ni | Co | Mo |
| 0.06-0.12 | 18.0-20.0 | Bal | 10.0-12.0 | 9.00-10.50 |
| Al | Ti | B | Fe | Zr |
| 1.40-1.80 | 3.00-3.50 | 0.003-0.010 | ≤5.00 | ≤0.07 |
| Mn | Si | P | S | Cu |
| ≤0.50 | ≤0.50 | ≤0.015 | ≤0.015 | ≤0.50 |
GH141 is a high-temperature alloy of nickel-based deformation. Within 650-950 ° C, it has high stretching and long-lasting creep intensity and good antioxidant performance. Due to the high content of aluminum, titanium, and molybdenum in alloy, it is difficult to billet in ingots, but the deformation materials have a good plasticity. The varieties of alloys include thin plates, bands, silk, disk, ring parts, forged parts, rods, and precision castings. It is suitable for manufacturing aerospace engines parts with high-strength.
Chemical Composition(%)
| C | Cr | Ni | Co | Mo |
| 0.06-0.12 | 18.0-20.0 | Bal | 10.0-12.0 | 9.00-10.50 |
| Al | Ti | B | Fe | Zr |
| 1.40-1.80 | 3.00-3.50 | 0.003-0.010 | ≤5.00 | ≤0.07 |
| Mn | Si | P | S | Cu |
| ≤0.50 | ≤0.50 | ≤0.015 | ≤0.015 | ≤0.50 |
