System and method for cooling a leading edge of a high speed vehicle
US-2021147061-A1 · May 20, 2021 · US
US2022411901A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2022411901-A1 |
| Application number | US-202117361961-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jun 29, 2021 |
| Priority date | Jun 29, 2021 |
| Publication date | Dec 29, 2022 |
| Grant date | — |
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An oxide dispersion strengthened refractory-based alloy is provided, along with methods of its formation and use. The oxide dispersion strengthened refractory-based alloy may include a refractory-based alloy comprising two or more refractory elements and forming a continuous phase; and a rare earth refractory oxide comprising at least one rare earth element and at least one of the two or more refractory elements. The rare earth refractory oxide forms discrete particles within the continuous phase, and the oxide dispersion strengthened refractory-based alloy comprises 0.1 volume % to 5 volume % of the rare earth refractory oxide.
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What is claimed is: 1 . An oxide dispersion strengthened refractory-based alloy, comprising: a refractory-based alloy comprising two or more refractory elements and forming a continuous phase; and an in-situ precipitated rare earth refractory oxide comprising at least one rare earth element and at least one of the two or more refractory elements, wherein the rare earth refractory oxide forms discrete particles within the continuous phase, and wherein the oxide dispersion strengthened refractory-based alloy comprises 0.1 volume % to 5 volume % of the rare earth refractory oxide. 2 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the oxide dispersion strengthened refractory-based alloy comprises 0.5 volume % to 2.5 volume % of the rare earth refractory oxide. 3 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the in-situ precipitated rare earth refractory oxide has a pyrochlore structure. 4 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the in-situ precipitated rare earth refractory oxide has a chemical formula of Ln 2 A 2 O 7 where Ln is the at least one rare earth element and A is the at least one of the two or more refractory elements, wherein the at least one rare earth element comprises scandium, yttrium, lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or mixtures thereof. 5 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the refractory-based alloy is a high entropy alloy. 6 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein rare earth refractory oxide comprises Ln 2 Hf 2 O 7 . 7 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the discrete particles have an average diameter of 0.001 μm to 5 μm. 8 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the refractory-based alloy comprises greater than 75 atomic % of refractory elements. 9 . The oxide dispersion strengthened refractory-based alloy of claim 1 , wherein the refractory-based alloy comprises greater than 95 atomic % of refractory elements. 10 . A leading edge for a hypersonic vehicle, the leading edge comprising the oxide dispersion strengthened refractory-based alloy of claim 1 . 11 . A method of forming an oxide dispersion strengthened refractory-based alloy, the method comprising: forming a physical powder mixture from a refractory powder and a rare earth oxide powder, wherein the refractory powder comprises at least two refractory elements, and wherein the rare earth oxide powder comprises a rare earth oxide; mechanically alloying the physical powder mixture to form an alloyed mixture having the rare earth oxide at least partially dissolved therein; and thereafter, consolidating the alloyed mixture to form the oxide dispersion strengthened refractory-based alloy, wherein consolidating reacts the dissolved rare earth oxide with at least one of the at least two refractory elements to precipitate dispersed discrete particles therein to form the oxide dispersion strengthened refractory-based alloy, wherein the continuous phase includes the two or more refractory elements, and wherein the discrete precipitated particles comprise a rare earth refractory oxide. 12 . The method of claim 11 , wherein the rare earth refractory oxide has a pyrochlore structure. 13 . The method of claim 11 , wherein the rare earth oxide powder comprises 0.1% by volume to 5% by volume of the powder mixture. 14 . The method of claim 11 , wherein the rare earth refractory oxide having a pyrochlore structure has a chemical formula of Ln 2 A 2 O 7 where Ln is the at least one rare earth element and A is the at least one of the two or more refractory elements, wherein the at least one rare earth element comprises scandium, yttrium, lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, or mixtures thereof. 15 . The method of claim 14 , wherein hafnium is included in the two or more refractory elements such that the rare earth refractory oxide having a pyrochlore structure has a chemical formula of Ln 2 Hf 2 O 7 where Ln is the at least one rare earth element. 16 . The method of claim 11 , wherein mechanically alloying the powder mixture comprises: milling the powder mixture until greater than 75% by weight of all of the starting rare earth oxide is dissolved. 17 . The method of claim 16 , wherein milling the powder mixture is performed in an inert atmosphere or under vacuum, and wherein milling is performed a temperature of 20° C. to 150° C. 18 . The method of claim 11 , wherein consolidating the powder mixture comprises: heating the alloyed mixture at a consolidation temperature that is 50% of the melting point of the refractory-based alloy or greater. 19 . The method of claim 18 , wherein the consolidation temperature is 50% to 90% of the melting point of the refractory-based alloy. 20 . The method of claim 11 , wherein each refractory element in the refractory powder is supplied to the physical powder mixture via a substantially pure refractory element powder.
Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00 · CPC title
by mechanical alloying (blending, milling) · CPC title
Alloys containing less than 50% by weight of each constituent · CPC title
with in situ formation of hard compounds · CPC title
with only oxides · CPC title
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