Descriptio:
Titanium 8-1-1（ etiam ut Ti-8Al-1Mo-1V） est firmus, valde obrepat renitens, altum robur stannum ad usum usque ad 455 °C. Summum modulum et infimum densitatem omnium Titanium alloys. It is used in annealed condition for such applications as airframe and jet engine parts that demand high strength, superior repre resist, and good rigorness-to-density ratio. Huius gradus machinabilitas similis est cum Titanio 6Al-4V.
| Applicationem | Airframe Parts, Jet Engine Parts |
| Signa | AMS 4972, AMS 4915, AMS 4973, AMS 4955, AMS 4916 |
| Formae Available | Bar, Plate, Sheet, Forgings, Fastener, Wire |
Compositio chemica (nominalis) %:
|
Fe |
Al |
V |
Mo |
H |
O |
N |
C |
|
≤0.3 |
7.5-8.5 |
0.75-1.75 |
0.75-1.25 |
0.0125-0.15 |
≤0.12 |
≤0.05 |
≤0.08 |
Ti=Bal.