Patent ID: 7332043

Claim:
Titanium-based alloy for production of large sized parts and fasteners for aeronautical engineering, consisting of aluminum, vanadium, molybdenum, chromium, iron and titanium, wherein the content of the components is in the following ratio, percentage by mass: aluminum 4.0-6.3 vanadium 4.5-5.9 molybdenum 4.5-5.9 chromium 2.0-3.6 iron 0.2-0.5 titanium balance, while the molybdenum equivalent Mo 3 ⁢ KB = % ⁢ Mo 1 + % ⁢ V 1.5 + % ⁢ Cr 0.6 + % ⁢ Fe 0.4 ≥ 13.8 .