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 - DUE DATE: 01-16-24 | 0.635 DIA X 160" RL 16.129MM DIA | 1846 LBS 837 KG |
| Alloy 901 | 0.760 DIA X 144" RL 19.304MM DIA | 904 LBS 410 KG |
| Alloy 901 | 0.760 DIA X 178"RL 19.304MM DIA | 216 LBS 98 KG |
| Alloy 901 - DUE DATE: 01-26-24 | 1.010 DIA X 160" RL 25.654MM DIA | 1846 LBS 837 KG |
| Alloy 901 - DUE DATE: 07-25-24 | 1.510 DIA X 160" RL 38.354MM DIA | 1857 LBS 842 KG |
| Alloy 901 | 3.635 DIA X 178-181RL+74.3 92.329MM DIA | 2455 LBS 1114 KG |
| Alloy 901 | 4.385 DIA X 7.5 111.379MM DIA | 32 LBS 15 KG |
| Alloy 901 | 5.635 DIA X 3 143.129MM DIA | 23 LBS 10 KG |