AMS4928 titanium bar

Product Details

The nominal composition of TC11 titanium alloy is TI-6.5AL-3.5MO-1.5Zr-0.3Si, which is an α+β type titanium alloy heat-resistant titanium alloy with an aluminum equivalent of 3.5 and a molybdenum equivalent of 7.3. The alloy also has good properties The thermal processing technology (including conventional process performance and superplasticity), can be welded and processed in various ways. The beta heat treatment and isothermal forging of this alloy have been developed rapidly.

The alloy also has a certain sensitivity to hot salt stress corrosion.

The alloy is mainly used to manufacture parts such as compressor discs, blades, drums and other parts of aero engines, and can also be used for aircraft structural parts. Through thermal deformation and heat treatment in the α-β zone, the maximum long-term temperature of the alloy is 500°C. The semi-finished products produced include bars, forgings and die forgings.

TC11 titanium alloy is a high-temperature titanium alloy widely used in my country, with a maximum operating temperature of 500°C. It is mainly used in aero-engine parts, such as blades, discs, drums and shafts. It can also be made into special-shaped castings. The working conditions of the production are: in the annealed state, it can be used for 500 hours below 500℃, 100 hours below 500℃ and 1000 hours below 450℃, and it can be used for 100 hours work below 500℃ in the strengthened state. Parts and parts that work at a time below 700°C.

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