Method of fabricating a working component for magnetic heat exchange
US-9524816-B2 · Dec 20, 2016 · US
US9978487B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9978487-B2 |
| Application number | US-201113817304-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2011 |
| Priority date | Aug 18, 2010 |
| Publication date | May 22, 2018 |
| Grant date | May 22, 2018 |
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An article for magnetic heat exchange includes a functionally-graded monolithic sintered working component including La 1-a R a (Fe 1-x-y T y M x ) 13 H z C b with a NaZn 13 -type structure. M is one or more of the elements from the group consisting of Si and Al, T is one or more of the elements from the group consisting of Mn, Co, Ni, Ti, V and Cr and R is one or more of the elements from the group consisting of Ce, Nd, Y and Pr. A content of the one or more elements T and R, if present, a C content, if present, and a content of M varies in a working direction of the working component and provides a functionally-graded Curie temperature. The functionally-graded Curie temperature monotonically decreases or monotonically increases in the working direction of the working component.
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The invention claimed is: 1. A method for fabricating a functionally-graded monolithic sintered working component for magnetic heat exchange, comprising: providing powder comprising elements in amounts sufficient for forming a La 1-a R a (Fe 1-x-y T y M x ) 13 H z C b phase with a NaZn 13 structure, wherein T is one or more of the elements selected from the group consisting of Mn, Co, Ni, Ti, V and Cr, M is one or more of the elements selected from the group consisting of Si and Al, and R is one or more of the elements selected from the group consisting of Ce, Nd, Y and Pr, wherein a is such that 0≤a≤0.5, b is such that 0≤b≤1.5, x is such that 0.05≤x≤0.2, y is such that 0≤y≤0.2, and z is such that 0≤z≤3; forming the powder to provide a green body in which an amount of at least one element selected from the group consisting of T, R, C and M varies in a pre-determined direction of the green body, heat treating the green body at a temperature T and for a time t selected to allow diffusion of one or more of the elements selected from the group consisting of T, R and C, and the heat treating step including forming a sintered working component comprising a Curie temperature that monotonically increases or monotonically decreases in the pre-determined direction, wherein the temperature T and the time t are selected to provide the monotonically increasing or monotonically decreasing Curie temperature, and wherein the monotonically increasing or monotonically decreasing Curie temperature changes with a gradient that lies within +/−50% of a linear function over 80% of a length of the working component, wherein the linear function is defined as the difference between the Curie temperature at one end of the working component and the Curie temperature at the opposing end of the working component divided by the distance between the two ends, and wherein nowhere along the length of the working component is there a gradient that exceeds 10° C./0.5 mm of length. 2. The method according to claim 1 , wherein the elements T, or C, or both, are present, and wherein the temperature T is selected to provide a diffusion rate of the elements T, or C, or both of at least 2×10 −11 m 2 /s. 3. The method according claim 1 , wherein the element C is present, and wherein the temperature T is selected to provide a diffusion rate of the element C of at least 1×10 −10 m 2 /s. 4. The method according to claim 1 , wherein the temperature T is 900° C.≤T≤1200° C. 5. The method according to claim 1 , wherein the temperature T is 1050° C.≤T≤1150° C. 6. The method according to claim 1 , wherein the time t is 1 h≤t≤100 h. 7. The method according to claim 1 , further comprising forming the powder from a plurality of powders with each powder comprising different amounts of at least one element selected from the group consisting of R, T, M and C and each powder being selected to provide a different Curie temperature when heat treated to form the NaZn 13 structure. 8. The method according to claim 7 , wherein layers of the plurality of powders are stacked such that the content of at least one element selected from the group consisting of R, T, M and C increases or decreases in a direction of the stack. 9. The method according to claim 7 , wherein each of the powders is mixed with a liquid and optionally with a binder and/or a dispersant to form a slurry or paste. 10. The method according to claim 9 , wherein the viscosity of the slurry or paste is between 200 mPas and 100,000 mPas. 11. The method according to claim 10 , wherein the slurries or pastes are applied to a surface layer by layer to form a stack such that the content of at least one element selected from the group consisting of R, T, M and C increases or decreases in a direction of the stack. 12. The method according to claim 11 , wherein each layer in the stack of layers has a thickness of 10 μm to 60 μm. 13. The method according to claim 9 , wherein before sintering, the liquid, binder and dispersant, if present, are removed at a temperature of 500° C. or below. 14. The method according to claim 7 , wherein varying proportions of the powders are mixed with one another before being arranged in a former such that the content of at least one element selected from the group consisting of R, T, M, and C of the powder in the former increases or decreases over a length of the former. 15. The method according to claim 7 , wherein varying proportions of the powders are introduced in a former such that the content of at least one element selected from the group consisting of R, T, M and C increases or decreases in an insertion direction of the powder into the former. 16. The method according to claim 1 , wherein the powder is formed into the green body by applying pressure. 17. The method according to claim 1 , wherein the green body is sintered at a temperature of 900° C. or greater to produce a density of 90% or more of a theoretical density of the La 1-a R a (Fe 1-x-y T y M x ) 13 H z C b phase with the NaZn 13 structure. 18. The method according to claim 1 , wherein M is Si and the amount of Si is selected according to Si m =3.85−0.0573×Co m −0.045×Mn m 2 +0.2965×Mn m , wherein Si m is the metallic weight fraction of silicon, Mn m is the metallic weight fraction of manganese and Co m is the metallic weight fraction of cobalt. 19. The method according to claim 1 , wherein M is Si and the amount of Si is selected according to Si m =3.85−0.045×Mn m 2 +0.2965×Mn m +(0.198−0.066×Mn m )×Ce(MM) m , wherein Si m is the metallic weight fraction of silicon, Mn m is the metallic weight fraction of manganese and Ce(MM) m is the metallic weight fraction of cerium misch metal. 20. The method according to claim 1 , further comprising hydrogenating the working component after the heat treating step. 21. The method according to claim 20 , wherein the working component is hydrogenated to produce a working component comprising a hydrogen content z of at least 90% of the hydrogen saturation value, z sat , of the NaZn 13 -structure. 22. The method according to claim 20 , wherein the working component is hydrogenated to produce a hydrogen content z of 1.4≤z≤3 in the La 1-a R a (Fe 1-x-y T y M x ) 13 H z phase. 23. The method according to claim 20 , wherein the hydrogenating comprises heat treating under a H 2 partial pressure of 0.5 to 2 bar. 24. The method according to claim 20 , wherein a H 2 partial pressure is increased during hydrogenating. 25. The method according to claim 20 , wherein the hydrogenating comprises treating at a temperature in the range 0° C. to 100° C. 26. The method according to claim 25 , wherein the hydrogenating comprises treating at a temperature in the range 15° C. to 35° C. 27. The method according to claim 20 , wherein the hydrogenating comprises a dwell at a temperature T hyd , wherein 300° C.≤T hyd ≤700° C. 28. The method according to claim 27 , wherein the hydrogenating comprises a dwell at a temperature T hyd , wherein 300° C.≤T hyd ≤700° C. followed by cooling in a hydrogen atmosphere to a temperature of less than 100° C. 29. The method according to claim 20 , wherein the hydrogenating comprises: heating the working component from a temperature of less than 50° C. to at least 300° C. in an inert atmosphere, introducing hydrogen gas only when a temperature of at least 300° C. is reached, maintaining th
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