| RA330® |
5592 5716 |
N08330 1.4886 |
19 |
35 |
|
1.25 |
43 |
0.05 C, 1.5 Mn |
The workhorse of austenitic heat resistant alloys. Good strength, carburization and oxidation resistance up to 2100°F. |
| RA333® |
5593 5717 |
N06333 2.4608 |
25 |
45 |
3.0 |
1.0 |
18 |
3.0 Co, 0.05 C, 3.0 W |
A nickel base superalloy with excellent carburization, oxidation, and hot corrosion resistance. It has high creep rupture strength with exceptional ability to withstand repeated thermal shock. |
| RA 602 CA® |
- |
N06025 2.4633 |
25 |
63 |
- |
- |
9.5 |
0.18 C, 2.2 Al, 0.1 Y, 0.08 Zr |
One of the most oxidation resistant high strength, heat resistant nickel alloys available. Useful through 2200°F. |
| 600 |
- |
N06600 2.4816 |
15.5 |
76 |
- |
0.2 |
8.0 |
0.2 Al, 0.2 Ti |
A nickel-chromium alloy with good carburization and oxidation resistance through 2000°F. |
| 601 |
5870 5715 |
N06601 2.4851 |
22.5 |
61.5 |
- |
0.2 |
14 |
1.4 Al, 0.3 Mn, 0.05 C |
A nickel base alloy with high chromium and an aluminum addition. Outstanding oxidation resistance to 2200°F, good strength and carburization resistance. |
| 625 |
5599 5666 5837 |
N06625 2.4856 |
21.5 |
61 |
9.0 |
0.1 |
5.0 |
3.6 Cb, 0.4 Al, 0.4 Ti |
High creep-rupture strength, oxidation resistant to 1800°F (982°C). Excellent resistance to hot seawater, scrubber environments and reducing acids. |
| 718 |
5596 5662 5663 5832 |
N07718 2.4668 |
19 |
52 |
3.0 |
- |
19 |
0.5 Al, 0.9 Ti, 5.0 Cb, 0.002 B |
Nickel alloy precipitation hardened by gamma prime and double prime. Readily fabricated, weldable even in the hardened condition. Used for gas turbine components to 1200°F, as well as for cryogenic equipment. |
| 718 NACE |
- |
N07718 2.4668 |
19 |
52 |
3.0 |
0.1 |
19 |
5.0 Cb |
Age hardened nickel alloy commonly used in oil and gas applications for its high strength and moderate corrosion resistance. Meets API 6A. |
| X |
5536 5754 5798 |
N06002 2.4665 |
22 |
47 |
9.0 |
- |
18 |
1.7 Co, 0.5 Al, 0.15 Ti, 0.6 W |
Good strength, fabricability and excellent oxidation resistance through 2000°F. Widely used for aircraft, marine and industrial gas turbine combustors. |
| INVAR 36 |
- |
K93600 K93603 1.3912 |
0.25 |
36 |
0.25 |
0.2 |
63 |
0.05 C |
Low expansion alloy used for molds and dies to form composites. |
| AL-6XN® |
- |
N08367 |
20.5 |
24 |
6.3 |
0.4 |
48 |
0.3 Mn, 0.22 N, 0.02 C |
A high molybdenum superaustenitic with outstanding resistance to chloride pitting, crevice corrosion and stress corrosion cracking. Suitable for use in pulp mill bleach plants, seawater heat exchangers
and chemical process equipment. |
| 800H/AT |
- |
N08811 N08810 1.4959 1.4876 |
21 |
31 |
- |
0.4 |
45 |
0.4 AI, 0.6 Ti |
High strength austenitic heat resistant alloy for ASME code applications to 1650°F. |
| Alloy 20 |
- |
N08020 2.4660 |
20 |
33 |
2.2 |
0.4 |
40 |
3.3 Cu, 0.5 Cb, 0.4 Mn, 0.02 C |
The alloy designated specifically to withstand sulfuric acid. Practical
immunity to chloride stress corrosion cracking. Stabilized to prevent
intergranular corrosion as welded. Resistant to polythionic acid SCC. |
| 230® |
5878 |
N06230 2.4733 |
22 |
60 |
1.5 |
|
1.0 |
0.3 Al, 0.02 La, 0.004 B, 14 W |
High strength nickel based alloy used for land based gas turbines. |
| X-750 |
|
NO7750 |
14.0 |
70.0 |
|
- |
5.0 |
|
|
