High-temperature high-entropy alloy with light weight and high strength in as-cast state and preparation method thereof
US-2024410035-A1 · Dec 12, 2024 · US
US10119180B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10119180-B2 |
| Application number | US-201515538119-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 14, 2015 |
| Priority date | Dec 22, 2014 |
| Publication date | Nov 6, 2018 |
| Grant date | Nov 6, 2018 |
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A titanium-based intermetallic alloy includes, in atomic percent, 16% to 26% Al, 18% to 28% Nb, 0% to 3% of a metal M selected from Mo, W, Hf, and V, 0.1% to 2% of Si, 0% to 2% of Ta, 1% to 4% of Zr, with the condition Fe+Ni≤400 ppm, the balance being Ti, the alloy also presenting an Al/Nb ratio in atomic percent lying in the range 1.05 to 1.15.
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The invention claimed is: 1. A titanium-based intermetallic alloy comprising, in atomic percent, 19.3% to 26% Al, 18% to 24.3% Nb, 0% to 3% of a metal M selected from Mo, W, Hf, and V, 0.1% to 2% of Si, 0% to 2% of Ta, 1% to 4% of Zr, with the condition Fe+Ni≤400 ppm, the balance being Ti, the alloy also presenting an Al/Nb ratio in atomic percent of about 1.07. 2. An alloy according to claim 1 , comprising 20% to 22% Nb, in atomic percent. 3. An alloy according to claim 1 , comprising 23% to 24% Al, in atomic percent. 4. An alloy according to claim 1 , comprising 0.1% to 0.8% Si, in atomic percent. 5. An alloy according to claim 1 claim 1 , comprising 0.8% to 3% of M, in atomic percent. 6. An alloy according to claim 1 , comprising 1% to 3% Zr, in atomic percent. 7. An intermetallic alloy according to claim 1 , wherein: the content of Al lies in the range 20% to 25%, in atomic percent; the content of Nb lies in the range 20% to 22%, in atomic percent; the content of M lies in the range 0.8% to 3%, in atomic percent; and the content of Zr lies in the range 1% to 3%, in atomic percent. 8. A turbomachine including a part including an alloy according to claim 1 . 9. An engine including a turbomachine according to claim 8 . 10. An aircraft including an engine according to claim 9 .
of titanium or alloys based thereon · CPC title
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