Manufacturing method of special spherical powder for additive manufacturing of nanometer multiphase reinforced titanium-based composite material
A technology for a titanium-based composite material and a manufacturing method, applied in the field of metal powder metallurgy, can solve the problems of insufficient laser melting of reinforced phase particle clusters, difficult to precisely control the reinforced phase content, poor fluidity, etc., so as to avoid physical properties and energy absorption coefficients. difference in argon, very few powder argon cavities, low cost effect
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Embodiment 1
[0041] This implementation case provides a kind of reinforcement phase volume fraction that is 5.5% (TiB+Y 2 o 3 +Ti 5 Si 3 ) / Ti-6Al-3Sn-4Zr-0.9Mo-0.3Si nanometer multiphase reinforced spherical powder of high-temperature titanium-based composite material manufacturing method. The alloy composition mass ratio corresponding to the in-situ self-generated high-temperature titanium-based composite material is: Ti-6Al-3Sn-4Zr-0.9Mo-0.3Si-0.4Y-0.6B, that is, 6% Al, 3% Sn, 4 % Zr, 0.9% Mo, 0.3% Si, 0.4% Y, 0.6% B, and the rest Ti. Correspondingly, a eutectic reaction occurs between Ti and B, and TiB with a volume fraction of 3.4% of the reinforcement phase is generated after in-situ authigenesis; Y reacts with solid-dissolved oxygen atoms in the melt to form Y with a volume fraction of 0.95% 2 o 3 ; solid state phase transition process, about the temperature above the β phase transition point, about 1.2% volume fraction of Ti 5 Si 3 Rapid precipitation from the β-Ti matrix.
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Embodiment 2
[0049] This implementation case provides a kind of reinforcement phase volume fraction that is 5.5% (TiB+Y 2 o 3 ) / Ti-6Al-4V nano multi-phase reinforced high-temperature titanium-based composite material spherical powder manufacturing method. The stoichiometric ratio corresponding to the in-situ self-generated high-temperature titanium-based composite material is: Ti-6Al-4V-0.9Y-0.6B (wt.%). Correspondingly, the volume fraction of in situ self-generated TiB is 3.4%, and the in situ self-generated Y 2 o 3 The volume fraction is 2.1%.
[0050] The difference between this embodiment and Example 1 is that step ① is to prepare raw materials according to the stoichiometric ratio of Ti-6Al-4V-0.9Y-0.6B (wt.%), and the titanium sponge, aluminum particles, Al -V intermediate alloy particles, put into V-type mixer for uniform mixing. Then the weighed high-purity boron powder and yttrium powder are uniformly mixed together with high-purity titanium powder of the same quality, then w...
Embodiment 3
[0053] This implementation case provides a kind of reinforcement phase volume fraction that is 5.5% (TiB+Y 2 o 3 +Ti 5 Si 3 ) / Ti-6Al-3Sn-4Zr-0.9Mo-0.3Si nanometer multiphase reinforced spherical powder of high-temperature titanium-based composite material manufacturing method. The alloy composition mass ratio corresponding to the in-situ self-generated high-temperature titanium-based composite material is: Ti-6Al-3Sn-4Zr-0.9Mo-0.3Si-0.4Y-0.6B, that is, 6% Al, 3% Sn, 4% 0.9% of Zr, 0.9% of Mo, 0.3% of Si, 0.4% of Y, 0.6% of B, and the rest of Ti. Correspondingly, the volume fraction of in situ generated reinforcement phase is 3.4% TiB, 0.95% Y 2 o 3 , 1.2% Ti 5 Si 3 .
[0054] The difference between this example and Example 1 is that in step ①, the titanium sponge, aluminum particles, tin particles, silicon particles, zirconium sponge, Al-Mo and Al-V intermediate alloy particles, Ti-Y The intermediate alloy chips are loaded into the V-type mixer for uniform mixing. Hi...
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