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TC11 titanium alloy, as a high-performance α-β heat-resistant material, has a unique chemical composition design, with an aluminum equivalent of 3.5 and a molybdenum equivalent of 7.3, which is designed to meet the harsh requirements of the aviation field. It shows a wide range of potential applications in compressor components, the core part of aircraft engines, covering a range of key components such as blades, disc components, drums and shafts, significantly improving the reliability and durability of these components under extreme conditions.

The TC11 is not limited to precision mechanical parts, but is also suitable for the manufacture of complex shapes of castings, demonstrating its versatility. In terms of heat treatment, the alloy shows excellent durability: in the annealed state, it can last 500 hours at 500 ° C, or 100 hours at 550 ° C, and even up to 1000 hours at 450 ° C; After intensive treatment, it is more adaptable to 100 hours of continuous operation at 500℃, and even competent for the challenge of short-term peak temperature of 700℃.

The greatest highlight of the alloy is its excellent thermal strength and long-term high temperature stability, even in the high temperature environment of 500℃, still can maintain high strength and excellent creep resistance. In addition, TC11 titanium alloy also shows high strength characteristics at room temperature, and has superior processing properties, whether it is conventional hot processing, cold processing or the use of its unique superplastic forming, can be easily achieved, coupled with good weldability, greatly expanding its application in aerospace structural parts manufacturing.