Enhancing the Strength of Al-B4C Composites to a High Degree by Mg Addition
US-2023257308-A1 · Aug 17, 2023 · US
US10815552B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10815552-B2 |
| Application number | US-201414309216-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 19, 2014 |
| Priority date | Jun 19, 2013 |
| Publication date | Oct 27, 2020 |
| Grant date | Oct 27, 2020 |
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An aluminum alloy includes, in weight percent, 0.50-1.30% Si, 0.2-0.60% Fe, 0.15% max Cu, 0.5-0.90% Mn, 0.6-1.0% Mg, and 0.20% max Cr, the balance being aluminum and unavoidable impurities. The alloy may include excess Mg over the amount that can be occupied by Mg—Si precipitates. The alloy may be utilized as a matrix material for a composite that includes a filler material dispersed in the matrix material. One such composite may include boron carbide as a filler material, and the resultant composite may be used for neutron shielding applications.
Opening claim text (preview).
What is claimed is: 1. A composite material comprising: a matrix of an aluminum alloy consisting essentially of, in weight percent: Si 0.50-1.30 Fe 0.2-0.60 Cu 0.15 max Mn 0.5-0.90 Mg 0.6-1.0 Cr 0.20 max Ti>0, the balance being aluminum and unavoidable impurities, wherein the alloy has excess magnesium over an amount that can be occupied by Mg—Si precipitates, wherein the excess magnesium is calculated using: Excess Mg═Mg−(Si−(Mn+Fe+Cr)/3)/1.16 where the excess magnesium is expressed as Excess Mg, and all values are expressed in weight percent; and particles of a boron carbide filler material dispersed within the matrix, wherein the boron carbide filler material has a volume fraction of 4-20% in the composite material, wherein the particles include a reaction product comprising titanium-containing intermetallic compound coating at least a portion of a surface thereof, and wherein the matrix of the aluminum alloy comprises Al—Fe—Mn—Si intermetallic phases dispersed therein, and wherein the matrix is formed from a molten aluminum alloy having a Ti content of at least 0.2 wt % prior to the formation of said reaction product. 2. The composite material of claim 1 , wherein the filler material has greater neutron absorption and radiation shielding capabilities than the matrix. 3. The composite material of claim 1 , wherein the filler material has a higher hardness and a higher melting point than the aluminum alloy of the matrix. 4. The composite material of claim 1 , wherein the Cu content of the alloy is up to 0.1 max wt. %. 5. The composite material of claim 1 , wherein the Si content of the alloy is 0.70-1.30 weight percent. 6. The composite material of claim 1 , wherein the Mg content of the alloy is 0.60-0.80 weight percent. 7. The composite material of claim 1 , wherein the alloy has at least 0.25 wt. % excess magnesium. 8. The composite material of claim 1 , wherein the matrix is formed from a molten aluminum alloy having a Ti content of 0.2-2 wt. % prior to formation of the reaction product. 9. A method comprising: preparing a molten aluminum alloy consisting essentially of, in weight percent: Si 0.50-1.30 Fe 0.2-0.60 Cu 0.15 max Mn 0.5-0.90 Mg 0.6-1.0 Cr 0.20 max the balance being aluminum and unavoidable impurities, wherein the alloy has excess magnesium over an amount that can be occupied by Mg—Si precipitates, wherein the excess magnesium is calculated using: Excess Mg═Mg−(Si−(Mn+Fe+Cr)/3)/1.16 where the excess magnesium is expressed as Excess Mg, and all values are expressed in weight percent; adding particles of a boron carbide filler material to the molten aluminum alloy to form a molten mixture having the filler material dispersed throughout the alloy; and casting the molten mixture to form a composite material having the aluminum alloy as a matrix and the filler material dispersed throughout the matrix, wherein the boron carbide filler material has a volume fraction of 4-20% in the composite material, wherein the particles include a reaction product comprising titanium-containing intermetallic compound coating at least a portion of a surface thereof, and wherein the matrix of the aluminum alloy comprises Al—Fe—Mn—Si intermetallic phases dispersed therein. 10. The method of claim 9 , further comprising extruding the composite material to form an extruded product. 11. The method of claim 9 , further comprising: stirring the molten mixture to wet the aluminum alloy to the particles of the boron carbide filler material and to distribute the particles throughout a volume of the molten mixture, prior to casting.
based on B4C · CPC title
starting from a melt · CPC title
Alloys containing non-metals (C22C1/05, C22C1/08 take precedence) · CPC title
with silicon · CPC title
Alloys based on aluminium · CPC title
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