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Titanium alloys are often enhanced by adding β-stabilizing elements such as molybdenum (Mo), chromium (Cr), and vanadium (V) to create β-titanium alloys. These alloys exhibit high strength, excellent formability, and can be further strengthened through quenching and aging treatments. When aged, the microstructure of the alloy consists of a fine α-phase distributed throughout a β matrix, which contributes to its mechanical properties and durability.
One of the most commonly used grades of β-titanium alloy is TB1, which has a composition of Ti-3Al-13V-11Cr. This alloy is typically employed in applications where temperatures remain below 350°C. It is particularly well-suited for manufacturing heavy-duty components such as compressor blades, shafts, and turbine discs, as well as critical parts in aerospace engineering. Due to its favorable combination of strength, toughness, and thermal stability, TB1 is widely used in high-performance environments where reliability is essential. Its ability to maintain structural integrity under demanding conditions makes it an ideal choice for both industrial and aerospace applications.