TI-8AL-1MO-1V
| Common Name | |
|---|---|
| Ti-8Al-1Mo-1V | |
| Ti-8-1-1-1 | |
| UNS | |
| R54810 | |
| General Information | |
| Ti-8Al-1Mo-1V is a “near alpha” alloy. It is primarily used in aircraft engine applications. The alloy is noted for being difficult to fabricate in larger sections. The alloy is available as wire (for welding), bar, billet, sheet, plate, extrusions, and forgings. | |
| Common Specification | |
| Specification | Product Form |
| AMS 4915 | Sheet, Strip, and Plate, Single Annealed |
| AMS 4916 | Sheet, Strip, and Plate, Duplex Annealed |
| AMS 4933 | Extrusions and Rings, Heat Treated |
| AMS 4955 | Weld Wire |
| AMS 4972 | Bar, Wire, and Rings, Heat Treated |
| Chemistry Requirements | ||||||||
|---|---|---|---|---|---|---|---|---|
| N | C | H | Fe | O | Al | V | Mo | Ti |
| 0.05 | 0.08 | 0.0125 | 0.3 | 0.15 | 7.35-8.35 | 0.75-1.25 | 0.75-1.25 | Balanc |
% Maximum unless given as a range.
| Minimum Tensile Properties | ||||
|---|---|---|---|---|
| Condition | UTS ksi (Mpa) | >0.2%YS ksi (MPA) | % El. | % RA* |
| Annealed | 130 (895) | 120 (828) | 10 | 20 |
| Heat Treated | 170 (1180) | 155 (1070) | 10 | 20 |
| Heat Treated at 800F | 90 (620) | 70 (480) | 10 | 25 |
| Typical Tensile Properties | ||||
|---|---|---|---|---|
| Condition | UTS ksi (Mpa) | >0.2%YS ksi (MPA) | % El. | % RA* |
| Annealed | 148 (1021) | 134 (924) | 19 | 40 |
Note: Typical properties are not to be utilized as a requirement, but are only listed for guidance. These properties may or may not be attainable in all circumstances.
* %Ra not required by all specifications
Trademark Notice: Some names are trade names and/or trademarks of specific manufacturers. Titan Singapore is not affiliated with any manufacturer(s). Orders will be filled to meet specifications from any available source(s). Names are listed solely for reference to help identify products consistent with listed specifications.