High-strength high-elasticity modulus titanium alloy
A high-elasticity, titanium alloy technology, applied in the field of titanium alloys, can solve problems such as poor deformation coordination ability, titanium alloy processing performance, and plastic index deterioration, and achieve the effect of increasing the elastic modulus
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Embodiment 1
[0022] Sponge titanium, sponge zirconium, pure aluminum, pure hafnium, aluminum vanadium master alloy, aluminum molybdenum master alloy, aluminum niobium master alloy and titanium boron master alloy according to composition Ti-4.5Al-3Zr-0.5Hf-4Mo-1V-1Nb -1.2B-0.06O ingredients are used to press electrodes, which are smelted in a shell-condensing furnace and a vacuum consumable furnace, and smelted into ingots twice. The ingot is forged and rolled to prepare a φ12 mm rod. After the bar is annealed at 850°C / 1h / AC, it is prepared into a standard tensile sample according to the national standard GB / T228-2000, and the mechanical properties are tested on a Shimadzu AG50KNE universal material testing machine. The obtained tensile strength Rm, Elongation A 5 and tensile modulus E are shown in Table 1.
Embodiment 2
[0024] Sponge titanium, sponge zirconium, pure aluminum, pure iron, pure chromium, aluminum-molybdenum master alloy, aluminum-niobium master alloy and titanium-boron master alloy respectively according to composition Ti-6Al-2Mo-2Cr-2Zr-0.5Fe-0.6B-0.22 The O ingredients are pressed into the electrode, and the ingot is smelted twice in a vacuum consumable furnace. The ingot is forged and rolled to prepare a φ12 mm rod. After the bar is annealed at 850°C / 1h / AC, it is prepared into a standard tensile sample according to the national standard GB / T228-2000, and the mechanical properties are tested on a Shimadzu AG50KNE universal material testing machine. The obtained tensile strength Rm, Elongation A 5 and tensile modulus E are shown in Table 1.
Embodiment 3
[0026] Sponge titanium, pure aluminum, pure chromium, aluminum-vanadium master alloy, aluminum-molybdenum master alloy and titanium-boron master alloy are respectively pressed into electrodes according to the ingredients of Ti-8Al-2Mo-2V-1Cr-0.7B-0.12O, and plasma melting and Vacuum self-consumption smelting, twice smelting into ingots. The cast ingots were slab forged and plate rolled to produce plates with a thickness of 2.0 mm. After the plate is annealed at 900°C / 1h / AC, the surface is sandblasted and pickled, prepared into a standard tensile sample according to the national standard GB / T228-2000, and tested for mechanical properties on a Shimadzu AG50KNE universal material testing machine. Tensile strength Rm, elongation A 5 and tensile modulus E are shown in Table 1.
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