| 188 |
5608 5801 |
R30188 2.4683 |
22 |
22.5 |
- |
37.7 |
2.0 |
14 W |
Cobalt base with high strength and oxidation resistance to 2000°F, used for gas turbine combustor cans. |
| L-605 |
5537 5796 |
R30605 2.4964 |
20 |
10.5 |
- |
50 |
2.0 |
15 W |
Cobalt base, solid solution strengthened alloy. |
| René 41 |
5545 5712 5713 5800 |
N07041 2.4973 |
19.3 |
52.7 |
9.4 |
10.6 |
3.0 |
3.2 Ti, 1.5 Al, 0.006 B |
Precipitation hardened nickel alloy with excellent strength through 1600°F. Used for gas turbine and missile hot components, including bolting and springs. |
| WASPALOY® |
5544 5828 |
N07001 2.4654 |
19 |
57 |
4.0 |
13 |
2.0 |
3.0 Ti, 1.4 Al, 0.006 B |
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. |
| C263 |
5966 |
N07263 2.4650 |
20 |
51 |
5.8 |
20 |
- |
2.2 Ti, 0.4 Al, 0.02 Zr, 0.001 B |
High strength age hardening grade for gas turbine combustors. |
| 694 (CM-64) |
- |
- |
27.3 |
5.0 |
- |
42.7 |
2.0 |
0.9 C, 20 W+Mo, 1.0 V |
Hardfacing wire for turbine blade interlock surfaces. Resists wear, thermal fatigue and oxidation. |
| TRIBALOY® T-800 |
- |
- |
17.8 |
1.0 |
29 |
49 |
1.0 |
3.4 Si |
Anti-galling hardfacing wire. Low coefficient of friction. |
