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 129-152RL 16.129MM DIA | 1436 LBS 651 KG |
Alloy 901 - DUE DATE: 10-15-25 | 0.635 DIA X 160 RL 16.129MM DIA | 2000 LBS 907 KG |
Alloy 901 - DUE DATE: 09-20-25 | 0.760 DIA X 120-144" RL 19.304MM DIA | 2000 LBS 907 KG |
Alloy 901 | 0.760 DIA X 144" RL 19.304MM DIA | 673 LBS 305 KG |
Alloy 901 - DUE DATE: 09-25-25 | 1.010 DIA X 25.654MM DIA | 2000 LBS 907 KG |
Alloy 901 | 1.010 DIA X 84-153RL 25.654MM DIA | 1751 LBS 794 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: 09-25-25 | 1.510 DIA X 161" RL 38.354MM DIA | 2000 LBS 907 KG |
Alloy 901 - DUE DATE: 09-25-25 | 2.010 DIA X 160" rl 51.054MM DIA | 2000 LBS 907 KG |
Alloy 901 - DUE DATE: 09-25-25 | 2.510 DIA X 160.063" RL 63.754MM DIA | 2000 LBS 907 KG |
Alloy 901 - DUE DATE: 09-25-25 | 3.635 DIA X 160 RL 92.329MM DIA | 3000 LBS 1361 KG |
Alloy 901 | 3.635 DIA X 178.5+178+169 92.329MM DIA | 1627 LBS 738 KG |