Self-supporting additively-manufactured heat exchanger header
US-2021148655-A1 · May 20, 2021 · US
US12130099B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12130099-B2 |
| Application number | US-202217959399-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 4, 2022 |
| Priority date | Oct 12, 2021 |
| Publication date | Oct 29, 2024 |
| Grant date | Oct 29, 2024 |
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A header for a high-pressure heat exchanger includes a first high-pressure transition section with inlets for multiple first high-pressure flow channels that are spaced from one another in a radial direction and collectively arranged in a substantially circular shape. The inlets for the multiple first high-pressure flow channels on a radially outer edge of the first high-pressure transition section are spaced further apart in a circumferential direction from adjacent inlets of the multiple first high-pressure flow channels than radially inward inlets are spaced from adjacent radially inward inlets of the multiple first high-pressure flow channels. The header also includes multiple first high-pressure flow channels extending from the first high-pressure transition section to a second-high pressure transition section that is configured to divide each of the multiple first high-pressure flow channels into at least two first high-pressure sub-flow channels.
Opening claim text (preview).
The invention claimed is: 1. A first header for a high-pressure heat exchanger, the header comprising: a first high-pressure inlet configured to connect to a source of high-pressure fluid and through which the high-pressure fluid flows therethrough to enter the first header; a first high-pressure tube extending from the high-pressure inlet to a first high-pressure transition section; the first high-pressure transition section configured to divide the high-pressure fluid from the first high-pressure tube into multiple first high-pressure flow channels extending in an axial direction, the first high-pressure transition section having inlets of the multiple first high-pressure flow channels spaced from one another in a radial direction and collectively arranged in a substantially circular shape, the inlets of the multiple first high-pressure flow channels on a radially outer edge of the first high-pressure transition section being spaced further apart in a circumferential direction from adjacent inlets of the multiple first high-pressure flow channels than radially inward inlets are spaced from adjacent radially inward inlets of the multiple first high-pressure flow channels; the multiple first high-pressure flow channels extending from the first high-pressure transition section to a second-high pressure transition section; the second high-pressure transition section being adjacent a core of the heat exchanger and configured to divide each of the multiple first high-pressure flow channels into at least two first high-pressure sub-flow channels, the first high-pressure sub-flow channels being configured to connect to high-pressure flow passages of the core; a low-pressure outlet configured to connect to a component able to accept low-pressure fluid; a low-pressure tube extending from a first low-pressure transition section to the low-pressure outlet; the first low-pressure transition section configured to merge the low-pressure fluid from multiple low-pressure flow channels into the low-pressure tube; the second low-pressure transition section being adjacent the core and configured to merge at least two low-pressure sub-flow channels into each of the multiple low-pressure flow channels; and the low-pressure sub-flow channels being configured to connect to low-pressure flow passages of the core. 2. The first header of claim 1 , wherein each flow channel of the first high-pressure flow channels and each sub-flow channel of the first high-pressure sub-flow channels have a round cross-sectional shape. 3. The first header of claim 1 , wherein each of the low-pressure sub-flow channels has a substantially diamond cross-sectional shape. 4. The first header of claim 2 , wherein the number of multiple low-pressure flow channels remains constant between the second low-pressure transition section and the first low-pressure transition section. 5. The first header of claim 2 , wherein the multiple first high-pressure flow channels, second high-pressure transition section, the first high-pressure sub-flow channels, the multiple low-pressure flow channels, the second low-pressure transition section, and the low-pressure sub-flow channels are all in a solid block. 6. The first header of claim 1 , wherein the low-pressure flow path changes direction forty-five degrees or less between the second low-pressure transition section and the first low-pressure transition section. 7. The first header of claim 1 , wherein the high-pressure fluid is at a pressure greater than approximately 300 bars (4350 psi). 8. The first header of claim 1 , wherein the low-pressure fluid is at a pressure greater than approximately 65 bars (950 psi). 9. The first header of claim 1 , wherein the round cross-sectional shape of each of the multiple first high-pressure flow channels and each of the first high-pressure sub-flow channels are circular. 10. The first header of claim 1 , wherein the multiple first high-pressure flow channels converge and then diverge between the first high-pressure transition section and the second high-pressure transition section. 11. The first header of claim 1 , wherein the multiple first high-pressure flow channels change direction forty-five degrees or less between the first high-pressure transition section and the second high-pressure transition section. 12. The first header of claim 1 , wherein the first high-pressure transition section is semi-ellipsoidal in a flow direction of the high-pressure fluid. 13. The first header of claim 1 , wherein the second high-pressure transition section is configured to divide each of the multiple first high-pressure flow channels into six first high-pressure sub-flow channels. 14. The first header of claim 1 , wherein the first high-pressure tube has a substantially circular cross-sectional shape. 15. A heat exchanger comprising: the core having high-pressure flow passages and low-pressure flow passages; and the first header of claim 1 connected to the core. 16. The heat exchanger of claim 15 , wherein the high-pressure flow passages have a substantially circular cross-sectional shape. 17. The heat exchanger of claim 15 , further comprising: a second header configured to extend from the core to a component able to accept high-pressure fluid, the second header comprising: a third high-pressure transition section adjacent to the core and configured to merge at least two second high-pressure sub-flow channels, which are configured to connect to high-pressure flow passages of the core, into one of multiple second high-pressure flow channels; the multiple second high-pressure flow channels extend between the third high-pressure transition section and a fourth high-pressure transition section; the fourth high-pressure transition section configured to merge the multiple second high-pressure flow channels extending in the axial direction into a second high-pressure tube, the fourth high-pressure transition section having outlets of the multiple second high-pressure flow channels spaced from one another in a radial direction and collectively arranged in a substantially circular shape, the outlets of the multiple second high-pressure flow channels on a radially outer edge of the fourth high-pressure transition section being spaced further apart in the circumferential direction from adjacent outlets of the multiple second high-pressure flow channels than radially inward outlets are spaced from adjacent radially inward outlets of the multiple second high-pressure flow channels; a second high-pressure tube extending from the fourth high-pressure transition section to a high-pressure outlet; the high-pressure outlet configured to connect to the component able to accept high-pressure fluid, wherein each of the second high-pressure flow channels and each of the second high-pressure sub-flow channels have a round cross-sectional shape. 18. The heat exchanger of claim 17 , wherein the second header further comprises: a second low-pressure flow path configured to extend from a source of low-pressure fluid to the core. 19. The heat exchanger of claim 17 , wherein the first header, the core, and the second header are one continuous and monolithic component constructed via additive manufacturing. 20. The first header of claim 1 , wherein the first high-pressure tube changes direction forty-five degrees or less between the first high-pressure inlet and the first high-pressure transition section.
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