A nickel-iron-chromium alloy containing titanium and aluminum for precipitation hardening and molybdenum for solid-solution strengthening. The alloy has high yield strength and creep resistance at temperatures to about 1110°F (600°C). A substantial iron content enables the alloy to combine high strength with good forging characteristics. Used in gas turbines for discs and shafts. Standard products form is round.
| ALLOY | SIZE | WEIGHT |
|---|---|---|
| CURRENT BAR INVENTORY | ||
| Alloy 901 | 0.635 DIA X 133-152RL 16.129MM DIA | 1253 LBS 568 KG |
| Alloy 901 - DUE DATE: 10-15-25 | 0.635 DIA X 160 RL 16.129MM DIA | 1846 LBS 837 KG |
| Alloy 901 - DUE DATE: 11-15-25 | 0.760 DIA X 120-144" RL 19.304MM DIA | 1753 LBS 795 KG |
| Alloy 901 | 0.760 DIA X 144" RL 19.304MM DIA | 599 LBS 272 KG |
| Alloy 901 - DUE DATE: 10-25-25 | 1.010 DIA X 160.1 RL 25.654MM DIA | 1857 LBS 842 KG |
| Alloy 901 - DUE DATE: 01-02-25 | 1.510 DIA X 160" RL 38.354MM DIA | 1857 LBS 842 KG |
| Alloy 901 - DUE DATE: 10-10-25 | 1.510 DIA X 161" RL 38.354MM DIA | 1842 LBS 836 KG |
| Alloy 901 - DUE DATE: 12-17-25 | 2.010 DIA X 160" rl 51.054MM DIA | 1797 LBS 815 KG |
| Alloy 901 - DUE DATE: 01-10-26 | 2.510 DIA X 160.063" RL 63.754MM DIA | 1867 LBS 847 KG |
| Alloy 901 - DUE DATE: 01-10-26 | 3.635 DIA X 160 RL 92.329MM DIA | 1797 LBS 815 KG |
| Alloy 901 | 3.635 DIA X 178.5+178+169 92.329MM DIA | 1627 LBS 738 KG |