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Titanium alloys can be enhanced by adding β-stabilizing elements such as molybdenum (Mo), chromium (Cr), and vanadium (V), which result in the formation of a β-titanium alloy. These alloys are known for their high strength, good formability, and the ability to undergo strengthening through quenching and aging treatments. When aged, the microstructure consists of fine β-phase with uniformly distributed α-phase particles, contributing to improved mechanical properties.
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 used at temperatures below 350°C and is well-suited for applications requiring high strength and durability. It is often employed in heavy-duty components such as compressor blades, turbine discs, and shafts, as well as critical parts in aerospace engineering. Due to its excellent combination of strength, toughness, and workability, TB1 is a popular choice for demanding industrial and aviation applications. Its versatility makes it an essential material in modern engineering systems where performance and reliability are crucial.