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Cobalt base with high strength and oxidation resistance to 2000°F, used for gas turbine combustor cans.
| Cr | Ni | Co | W | La | B | C | Fe | Mn | Si | P | S | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 20.0 | 20.0 | - | 13.0 | 0.02 | - | 0.05 | - | - | 0.2 | - | - |
| MAX | 24.0 | 24.0 | Balance | 16.0 | 0.12 | 0.015 | 0.015 | 3.0 | 1.25 | 0.5 | 0.02 | 0.015 |
Cobalt base, solid solution strengthened alloy.
| Cr | Ni | Co | W | C | Fe | Mn | Si | P | S | |
|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 19.0 | 9.0 | - | 14.0 | 0.05 | - | 1.0 | - | - | - |
| MAX | 21.0 | 11.0 | Balance | 16.0 | 0.15 | 3.0 | 2.0 | 0.4 | 0.04 | 0.03 |
Precipitation hardened nickel alloy with excellent strength through 1600°F. Used for gas turbine and missile hot components, including bolting and springs.
| Cr | Ni | Mo | Co | Al | Ti | B | C | Fe | Mn | Si | S | Cu | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 18.00 | -- | 9.00 | 10.00 | 1.40 | 3.00 | 0.003 | -- | -- | -- | -- | -- | -- |
| MAX | 20.00 | Balance | 10.50 | 12.00 | 1.80 | 3.30 | 0.01 | 0.12 | 5.00 | 0.10 | 0.50 | 0.015 | 0.50 |
Nickel alloy precipitation hardened by gamma prime with high strength and oxidation resistance to 1600°F. Applications are gas turbine components including shafts and fasteners.
| Cr | Ni | Mo | Co | Al | Ti | B | C | Zr | Fe | Mn | Si | P | S | Cu | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 18.00 | -- | 3.50 | 12.00 | 1.20 | 2.75 | 0.003 | 0.02 | 0.02 | -- | -- | -- | -- | -- | -- |
| MAX | 21.00 | Balance | 5.00 | 15.00 | 1.60 | 3.25 | 0.01 | 0.10 | 0.08 | 2.00 | 0.10 | 0.15 | 0.015 | 0.015 | 0.10 |
High strength age hardening grade for gas turbine combustors.
| Cr | Ni | Mo | Co | Al | Ti | Al+Ti | B | C | Fe | Mn | Si | P | S | Ag | Bi | Pb | Cu | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN | 19 | 5.6 | 19.0 | 0.3 | 1.9 | 2.4 | - | 0.01 | - | - | - | - | - | - | - | - | - | |
| MAX | 21.00 | Balance | 6.10 | 21.00 | 0.60 | 2.40 | 2.80 | 0.005 | 0.08 | 0.70 | 0.60 | 0.40 | 0.015 | 0.007 | 0.0005 | 0.0001 | 0.002 | 0.20 |
Hardfacing wire for turbine blade interlock surfaces. Resists wear, thermal fatigue and oxidation.
| Cr | Ni | Mo | Co | W+Mo | V | B | C | Fe | Mn | Su | |
|---|---|---|---|---|---|---|---|---|---|---|---|
| MIN |
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