Flow body for a gas turbine, gas turbine, method for manufacturing a flow body for a gas turbine, and method for repairing a flow body of a gas turbine
US-2024376825-A1 · Nov 14, 2024 · US
US11945033B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11945033-B2 |
| Application number | US-202217709498-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 31, 2022 |
| Priority date | Mar 31, 2021 |
| Publication date | Apr 2, 2024 |
| Grant date | Apr 2, 2024 |
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A method is provided for the heat treatment of an object comprising at least one rare-earth element with a high vapor pressure. One or more objects comprising at least one rare-earth element with a high vapor pressure are arranged in an interior of a package. An external source of the at least one rare-earth element is arranged so as to compensate for the evaporation of this same rare-earth element from the object and/or to increase the vapor pressure of the rare-earth element in the interior of the package, and the package is heat treated.
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The invention claimed is: 1. A method for heat treating an object, the method comprising the following: providing a lower box comprising a base, walls that surround the base, and an open side, providing an upper box comprising a cover, walls that surround the cover and an open side, arranging one or more objects on the base of the lower box, the one or more objects including at least one of Sm, Dy, Er, Eu, and Yb, and the lower box and/or the upper box comprising iron foil and/or an iron plate, arranging an external source of the at least one of Sm, Dy, Er, Eu, and Yb within the lower box and/or the upper box, the external source being provided by an alloy of iron and the at least one of Sm, Dy, Er, Eu, and Yb, covering the one or more objects with the upper box such that the open side of the upper box faces the base of the lower box, the walls of the upper box are arranged on the base of the lower box and a gap is formed between the walls of the upper box and the walls of the lower box, introducing a powder material into the gap in order to form an assembly having an interior, the powder material providing a mechanical obstacle to gas exchange between the interior and an environment outside of the interior of the assembly, and heat treating the assembly. 2. A method according to claim 1 , wherein the object comprises an SmCo alloy that is heat treated in order to produce a Sm 2 Co 17 - or SmiCos-type magnet. 3. A method according to claim 1 , wherein the assembly is subjected to heat treatment at a temperature above 1000° C. 4. A method according to claim 1 , wherein the external source comprises at least 0.04 wt % of the at least one of Sm, Dy, Er, Eu, and Yb, based on the total weight of the one or more objects. 5. A method according to claim 1 , wherein a layer of powder comprising the at least one of Sm, Dy, Er, Eu, and Yb is applied to an inside of the assembly. 6. A method according to claim 1 , wherein the external source comprises samarium hybrid. 7. A method according to claim 1 , wherein the alloy of iron and the at least one of Sm, Dy, Er, Eu, and Yb is formed on the surface of the iron foil and/or iron plate by heat treating the iron foil and/or the iron plate in an atmosphere containing the at least one of Sm, Dy, Er, Eu, and Yb. 8. A method according to claim 1 , wherein the assembly further comprises a support structure for the objects and the objects are arranged in the support structure. 9. A method according to claim 8 , wherein the support structure comprises iron and the external source is provided on the surface of the support structure by an alloy of iron and the at least one of Sm, Dy, Er, Eu, and Yb that is formed by heat treating the support structure in an atmosphere containing the at least one of Sm, Dy, Er, Eu, and Yb. 10. A method according to claim 9 , wherein a layer of a powder comprising the at least one of Sm, Dy, Er, Eu, and Yb is applied to the support structure. 11. A method according to claim 1 , wherein the powder material is an additional external source of the at least one of Sm, Dy, Er, Eu, and Yb that is contained in the object. 12. A method according to claim 11 , wherein the powder material comprises a content of the at least one of Sm, Dy, Er, Eu, and Yb of at least 15 wt %. 13. A method according to claim 1 , wherein the powder material is made up of different powder materials. 14. A method according to claim 13 , wherein the powder material comprises the external source of the at least one of Sm, Dy, Er, Eu, and Yb and an active material. 15. A method according to claim 14 , wherein the powder material comprises a lower layer comprising the at least one of Sm, Dy, Er, Eu, and Yb, and an upper layer comprising an active material. 16. A method according to claim 15 , wherein the active material is an oxygen getter.
with one or more parts not made from powder {(B22F7/062 takes precedence)} · CPC title
based on cobalt · CPC title
and magnetic transition metals, e.g. SmCo5 · CPC title
for manufacturing permanent magnets · CPC title
Treatment under specific atmosphere · CPC title
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