Electrode material for aluminum electrolytic capacitors and method for producing same
US-2024301561-A1 · Sep 12, 2024 · US
US2017292174A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017292174-A1 |
| Application number | US-201715473343-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 29, 2017 |
| Priority date | Apr 7, 2016 |
| Publication date | Oct 12, 2017 |
| Grant date | — |
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New aluminum alloys having iron, vanadium, silicon, and copper, and with a high volume of ceramic phase therein are disclosed. The new products may include from 3 to 12 wt. % Fe, from 0.1 to 3 wt. % V, from 0.1 to 3 wt. % Si, from 1.0 to 6 wt. % Cu, from 1 to 30 vol. % ceramic phase, the balance being aluminum and impurities. The ceramic phase may be homogenously distributed within the alloy matrix.
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What is claimed is: 1 . An aluminum alloy consisting essentially of: from 3 to 12 wt. % Fe; from 0.1 to 3 wt. % V; from 0.1 to 3 wt. % Si; from 1.0 to 6 wt. % Cu; and from 1.0 to 30 vol. % ceramic phase; the balance being aluminum and impurities. 2 . An aluminum alloy body made from the aluminum alloy of claim 1 , the aluminum alloy body having an alloy matrix and a ceramic phase, wherein the aluminum alloy body comprises a homogenous distribution of the ceramic phase within the alloy matrix. 3 . The aluminum alloy body of claim 2 , wherein the aluminum alloy body is in the form of an engine component for an aerospace vehicle. 4 . The aluminum alloy body of claim 2 , comprising from 5 to 35 vol. % AlFeVSi dispersoids. 5 . The aluminum alloy body of claim 4 , wherein the AlFeVSi dispersoids comprise at least some copper. 6 . The aluminum alloy body of claim 2 , comprising a cellular structure comprising iron and copper. 7 . The aluminum alloy of claim 1 , wherein the ceramic phase is selected from the group consisting of TiB 2 , TiC, and combinations thereof. 8 . The aluminum alloy of claim 1 , wherein the ceramic phase is TiB 2 . 9 . A method of making an aluminum alloy body, comprising: (a) dispersing a powder comprising in a bed, wherein the powder consists essentially of: from 3 to 12 wt. % Fe; from 0.1 to 3 wt. % V; from 0.1 to 3 wt. % Si; from 1.0 to 6 wt. % Cu; from 1.0 to 30 vol. % ceramic phase; and the balance being aluminum (Al) and impurities; (b) selectively heating a portion of the powder to a temperature above the liquidus temperature of the particular aluminum alloy body to be formed; (c) forming a molten pool having the Fe, V, Si, Cu, Al, and ceramic phase; (d) cooling the molten pool at a cooling rate of at least 1000° C. per second; and (e) repeating steps (a)-(d) to form an additively manufactured aluminum alloy body. 10 . The method of claim 9 , comprising: completing the additively manufactured aluminum alloy body, thereby realizing a final aluminum alloy product; naturally aging the final aluminum alloy product; and after the natural aging, artificially aging the final aluminum alloy product. 11 . The method of claim 10 , comprising: after the naturally aging step, deforming the final aluminum alloy product by from 1 to 10%. 12 . The method of claim 10 , wherein the artificial aging comprises: heating the final aluminum alloy product at a temperature of from 125° C. to 300° C. and for a period of from 2 to 48 hours. 13 . The method of claim 12 , wherein the final aluminum alloy product is in the form of an engine component for an aerospace or automotive vehicle, wherein the method comprises: incorporating the engine component into the aerospace or automotive vehicle. 14 . The method of claim 13 , comprising: operating the aerospace or automotive vehicle. 15 . The method of claim 13 , wherein the final aluminum alloy product is a compressor wheel for a turbo charger. 16 . The method of claim 13 , wherein the final aluminum alloy product is a blade for a turbine. 17 . The method of claim 13 , wherein the final aluminum alloy product is a heat exchanger.
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