Heat exchangers

Patent metadata

Field	Value
Publication number	US-11293703-B2
Application number	US-202117226973-A
Country	US
Kind code	B2
Filing date	Apr 9, 2021
Priority date	Jan 12, 2016
Publication date	Apr 5, 2022
Grant date	Apr 5, 2022

Abstract

A counter-flow heat exchanger core includes a first wall defining a longitudinal axis. The first flow path is defined within the first wall. The first flow path includes a primary flow inlet and a primary flow outlet downstream from the primary flow inlet. The heat exchanger core includes at least two hollow vanes circumferentially spaced apart and extending in a radially inward direction from the first wall. Each of the at least two hollow vanes includes a first vane wall and a second vane wall. The heat exchanger core includes a second flow path defined within the at least two hollow vanes between the first vane wall and second vane wall of each of the at least two hollow vanes. The heat exchanger core includes at least one fin extending between two of the at least two circumferentially spaced apart vanes.

First claim

What is claimed is:

1. A counter-flow heat exchanger core comprising:
a first wall defining a longitudinal axis;
a first flow path defined within the first wall, wherein the first flow path includes a primary flow inlet and a primary flow outlet downstream from the primary flow inlet;
at least two hollow vanes circumferentially spaced apart and extending in a radially inward direction from the first wall, wherein each of the at least two hollow vanes includes a first vane wall and a second vane wall;
a second flow path defined within the at least two hollow vanes between the first vane wall and second vane wall of each of the at least two hollow vanes; and
at least one fin extending between two of the at least two hollow vanes.

2. The counter-flow heat exchanger core as recited in claim 1 , wherein the at least one fin is at least one of a non-linear fin or a portion of a cylindrical wall.

3. The counter-flow heat exchanger core as recited in claim 1 , further comprising a second wall radially inward from the first wall.

4. The counter-flow heat exchanger core as recited in claim 1 , wherein the at least one non-linear fin includes a plurality of non-linear fins between two of the hollow vanes, wherein each of the plurality of non-linear fins are equally spaced apart from adjacent fins in a radial direction.

5. The counter-flow heat exchanger core as recited in claim 1 , wherein the at least one non-linear fin includes a plurality of non-linear fins between two of the hollow vanes, wherein the plurality of non-linear fins are variably spaced apart in a radial direction to the first wall.

6. The counter-flow heat exchanger core as recited in claim 5 , wherein the non-linear fins more proximate to the longitudinal axis are spaced farther apart from one another than the non-linear fins more proximate to the first wall.

7. The counter-flow heat exchanger core as recited in claim 1 , wherein the heat exchanger core includes a housing wall radially outward from the first wall.

8. The counter-flow heat exchanger core as recited in claim 7 , wherein the housing wall defines a second flow path inlet and a second flow path outlet, wherein the second flow path outlet is downstream from the second flow path inlet.

9. The counter-flow heat exchanger core as recited in claim 7 , wherein a fluid distributor inlet annulus is defined between the first wall and the housing wall.

10. The counter-flow heat exchanger core as recited in claim 9 , wherein the fluid distributor inlet annulus is in fluid communication with the second flow path of each of the hollow vanes.

11. The counter-flow heat exchanger core as recited in claim 9 , wherein a fluid distributor outlet annulus is defined between the first wall and the housing wall downstream from the fluid distributor inlet annulus and the circumferentially spaced apart hollow vane.

12. The counter-flow heat exchanger core as recited in claim 11 , wherein the housing wall defines a second flow path inlet and a second flow path outlet, wherein the second flow path outlet is downstream from the second flow path inlet and the fluid distributor outlet annulus.

13. The counter-flow heat exchanger core as recited in claim 7 , wherein the housing wall defines a second flow path inlet and a second flow path outlet, wherein the second flow path outlet is downstream from the second flow path inlet, wherein the second flow path inlet and the second flow path outlet are spaced apart from one another along the longitudinal axis.

14. The counter-flow heat exchanger core as recited in claim 13 , wherein the second flow path inlet and a second flow path outlet are offset from one another by 180 degrees.

15. The counter-flow heat exchanger core as recited in claim 1 , further comprising an inner wall radially inward from the first wall, wherein the first wall is an outer wall, wherein the at least two hollow vanes are formed by the inner wall and define channels, wherein the first vane wall is a first portion of the inner wall and the second vane wall is a second portion of the inner wall, wherein the second flow path is defined at least partially within the channels.

16. The counter-flow heat exchanger core as recited in claim 15 , wherein the at least one fin is a portion of a cylindrical wall between the first vane wall of one of the at least two vanes and the first vane wall of another of the at least two vanes.

17. A method of manufacturing a counter-flow heat exchanger core, the method comprising:
forming a heat exchanger core body using additive manufacturing, wherein the heat exchanger core body includes:
a first wall defining a longitudinal axis;
a first flow path defined within the first wall, wherein the first flow path includes a primary flow inlet and a primary flow outlet downstream from the primary flow inlet;
at least two hollow vanes circumferentially spaced apart and extending in a radially inward direction from the first wall, wherein each of the at least two hollow vanes includes a first vane wall and a second vane wall;
a second flow path defined within the at least two hollow vanes between the first vane wall and second vane wall of each of the at least two hollow vanes; and
at least one fin extending between two of the at least two hollow vanes.

18. The method as recited in claim 17 , wherein the at least one fin is at least one of a non-linear fin or a portion of a cylindrical wall.

19. The method as recited in claim 17 , wherein the additive manufacturing is via selective laser melting.

Assignees

• Utc Aerospace Systems Wroclaw Sp Z O O
• Hamilton Sundstrand Corp

Inventors

• Meczkowski Tomasz
• Siudzinski Hubert
• Rubalewski Jaroslaw
• Saltzman David
• Drzewiecki Jakub
• Turney Joseph
• Kelley Ryan Matthew

Classifications

• F28F1/40

  the means being only inside the tubular element · CPC title

• F28D9/0018

  without any annular circulation of the heat exchange media · CPC title

• F28D7/106 Primary

  consisting of two coaxial conduits or modules of two coaxial conduits · CPC title

• F28F1/006

  with variable shape, e.g. with modified tube ends, with different geometrical features (F28F1/025, F28F1/06, F28F1/08, F28F9/16, F28F9/18 take precedence) · CPC title

• F28F2210/02

  with particular branching, e.g. fractal conduit arrangements · CPC title