High-strength discontinuosly-reinforced titanium matrix composites and method for manufacturing the same
a titanium matrix and discontinuous reinforcement technology, applied in the field of titanium metal matrix composites, can solve the problems of high production cost, inability to manufacture components, limited process stability, etc., and achieve the effect of improving mechanical characteristics
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example 1
[0052]A TiB2 and SiC-reinforced titanium composite material based on the Ti-6Al-4V alloy matrix was manufactured by (a) preparing a basic powder blend containing titanium powder and having a particle size ≦200 mesh (≦74 microns) for 95% of the powder, 5% of graphite, 2.5% of dispersing SiC powder. 7.5% of dispersing TiB2 particles, and 2.5% of dispersing powders of AlTi2Si3, (Ti, V)(B,C), and TiVB4 complex intermetallic particles partially soluble in the matrix at 1500-2300° F., (b) co-attrition and mechanical alloying of the basic blend components to manufacture reinforcing particles of complex composition and controlled particle size, (c) making a powder of Al-V master alloy having a particle size of 10 μm and less, (d) co-attrition of 30% of this master alloy powder with reinforcing powders of graphite. SiC powder, TiB2 particles, and powders of AlTi2Si3, (Ti,V)(B,C), and TiVB4 complex intermetallic particles, (e) mixing the basic powder blend with the master alloy powder and rei...
example 2
[0054]A carbide-reinforced titanium composite material based on the Ti-6Al-4V alloy matrix was manufactured by (a) preparing a basic powder blend containing titanium powder having a particle size ≦140 mesh (≦100 μm) for 95% of the powder, 2% of graphite, 15% of dispersing SiC powder, and 4% of dispersing AlV2C. Ti2AlC, and V2C particles partially soluble in the matrix at 1500-2300° F., (b) co-attrition and mechanical alloying of the basic blend components to manufacture reinforcing particles of complex composition and controlled particle size, (c) making a powder of Al-V master alloy having a particle size of 10 μm and less, (d) mixing and co-attriting the basic powder blend with the master alloy powder, at the ratio of 9:1 to obtain a chemical composition of titanium matrix composite material, (e) compacting the powder mixture at room temperature by die-pressing, (f) sintering at 2350° F., (g) forging at 1600° F., and (h) cooling.
[0055]Sintered semi-product had a density of 99% wit...
example 3
[0056]The titanium matrix composite was manufactured using the same raw materials for Ti-6Al-4V matrix alloy and carbide reinforcements, and the same mode of sintering as in Example 1. The final hot deformation was made by hot rolling at 1650° F. instead of forging.
[0057]The resulting TiC / Ti-6Al-4V. composite material also had 100% density, and exhibited satisfied yield strength at room temperature and at 930° F. (500° C.).
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