Fluid channels having performance enhancement features and devices incorporating same
US-2015377562-A1 · Dec 31, 2015 · US
US10132522B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10132522-B2 |
| Application number | US-201414230682-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 31, 2014 |
| Priority date | Mar 31, 2014 |
| Publication date | Nov 20, 2018 |
| Grant date | Nov 20, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A counter flow air-to-air energy exchange assembly may include a plurality of air channel levels configured to allow air to pass therethrough. Each of the air channels may include a spacer layer having a plurality of modular spacer components secured together. At least two of the modular spacer components are identical in size and shape. The spacer layer includes a plurality of air channels. Each of the plurality of air channels extends from an air inlet to an air outlet.
Opening claim text (preview).
What is claimed is: 1. A counter flow air-to-air energy exchange assembly including a plurality of air channel levels configured to allow air to pass therethrough, wherein each of the plurality of air channel levels comprises: a spacer layer including: (a) a plurality of modular spacer components secured together, and (b) a plurality of air channels, wherein each of the plurality of air channels extends from an air inlet to an air outlet, wherein an outer boundary of the spacer layer is shaped as a hexagon, and wherein the plurality of modular spacer components comprises a first spacer component and a second spacer component that is identical in size and shape to the first spacer component, and each of the first and second spacer components has an outer boundary shaped as a trapezoid, the outer boundary of each spacer component formed by a plurality of walls. 2. The counter flow air-to-air energy exchange assembly of claim 1 , wherein each of the plurality of air channels forms a Z-shape. 3. The counter flow air-to-air energy exchange assembly of claim 1 , wherein each of the plurality of air channels forms a U-shape. 4. The counter flow air-to-air energy exchange assembly of claim 1 , wherein the first spacer component directly secures to the second spacer component. 5. The counter flow air-to-air energy exchange assembly of claim 1 , wherein the plurality of modular spacer components further comprises a third spacer component that differs from the first and second spacer components, wherein the third spacer component is positioned between the first and second spacer components. 6. The counter flow air-to-air energy exchange assembly of claim 5 , wherein an outer boundary of the third spacer is shaped as a hexagon. 7. The counter flow air-to-air energy exchange assembly of claim 5 , wherein the plurality of modular spacer components further comprises a fourth spacer component that is identical to the third spacer component, wherein the fourth spacer component connects to the third spacer component, and wherein the third and fourth spacer components are positioned between the first and second spacer components. 8. The counter flow air-to-air energy exchange assembly of claim 1 , wherein the plurality of modular spacer components further comprises third and fourth spacer components that are identical to the first and second spacer components. 9. The counter flow air-to-air energy exchange assembly of claim 8 , wherein the plurality of modular spacer components further comprises a fifth spacer component that differs from the first, second, third, and fourth spacer components, wherein the fifth spacer component provides an expansion piece. 10. A method of forming a counter flow air-to-air energy exchange assembly including a plurality of air channel levels configured to allow air to pass therethrough, the method comprising: securing a plurality of modular spacer components together, wherein the plurality of modular spacer components comprises a first spacer component and a second spacer component that is identical in size and shape to the first spacer component, and each of the first and second spacer components has an outer boundary shaped as a trapezoid, the outer boundary of each spacer component formed by a plurality of walls; forming a spacer layer through the securing operation, the spacer layer having an outer boundary shaped as a hexagon; positioning at least one membrane on the spacer layer to form an air channel level; and stacking the air channel level over another air channel level, wherein each of the plurality of air channels extends from an air inlet to an air outlet. 11. The method of claim 10 , wherein each of the plurality of air channels forms a Z-shape. 12. The method of claim 10 , wherein each of the plurality of air channels forms a U-shape. 13. The method of claim 10 , wherein the forming operation comprises directly securing the first spacer component to the second spacer component. 14. The method of claim 10 , wherein the forming operation comprises positioning a third spacer component between the first and second spacer components, wherein the third spacer component differs from the first and second spacer components. 15. The method of claim 14 , wherein an outer boundary of the third spacer is shaped as a hexagon. 16. The method of claim 14 , wherein the forming operation comprises: positioning the third spacer components and a fourth spacer component between the first and second spacer components, wherein the third spacer is identical to the fourth spacer; and connecting the third and fourth spacer components together. 17. The method of claim 10 , wherein the plurality of modular spacer components further comprises third and fourth spacer components that are identical to the first and second spacer components. 18. The method of claim 17 , wherein the plurality of modular spacer components further comprises a fifth spacer component that differs from the first, second, third, and fourth spacer components, wherein the fifth spacer component provides an expansion piece. 19. A spacer layer assembly configured to form part of an air channel level of a counter flow air-to-air energy exchange assembly, the spacer layer assembly comprising: a plurality of modular spacer components secured together to form a single spacer layer having an outer boundary shaped as a hexagon, wherein the plurality of modular spacer components comprises a first spacer component and a second spacer component that is identical in size and shape to the first spacer component, and each of the first and second spacer components has an outer boundary shaped as a trapezoid, the outer boundary of each spacer component formed by a plurality of walls.
using an air-to-air heat exchanger (F24F12/002 takes precedence) · CPC title
heat exchangers {or parts thereof}, e.g. radiators, condensers {fins, headers}(making finned or ribbed tubes by fixing strip material or the like to tubes B21C37/22) · CPC title
the heat being recuperated from waste air or from vapors (for air conditioning F24F12/001) · CPC title
Heat exchanger or boiler making · CPC title
with means for changing flow direction of one heat exchange medium, e.g. using deflecting zones · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.