Modular heat exchanger systems

Patent metadata

Field	Value
Publication number	US-12434845-B2
Application number	US-202318169910-A
Country	US
Kind code	B2
Filing date	Feb 16, 2023
Priority date	Feb 16, 2023
Publication date	Oct 7, 2025
Grant date	Oct 7, 2025

Abstract

A heat exchanger system and method includes a securing frame, a heat transfer core having heat transfer panels removably secured to the securing frame, the heat transfer panels optionally including a plurality of segment modules coupled together, and one or more filter screens removably secured to the securing frame at one or both of an inlet end or an outlet end. The heat transfer core is disposed between the inlet end and the outlet end.

First claim

What is claimed is:

1. A heat exchanger system, comprising:
a securing frame;
a heat transfer core removably secured to the securing frame, wherein the heat transfer core comprises heat transfer panels removably coupled to the securing frame, wherein a size and shape of the heat transfer core is selectively changeable, and wherein each of the heat transfer panels comprises:
fluid passages in fluid communication to form a fluid circuit that extends between a fluid inlet and a fluid outlet; and
heat transfer fins separated by fluid channels; and

one or more filter screens secured to the securing frame at one or both of an inlet end or an outlet end, wherein the heat transfer core is disposed between the inlet end and the outlet end.

2. The heat exchanger system of claim 1 , wherein each of the heat transfer panels further comprises a plurality of segment modules removably coupled together.

3. The heat exchanger system of claim 2 , wherein each of the plurality of segment modules is configured to removably stack onto another of the plurality of segment modules via removably couplings.

4. The heat exchanger system of claim 1 , wherein the heat transfer panels are devoid of guard fins.

5. The heat exchanger system of claim 1 , wherein the one or more filter screens are removably coupled to the securing frame.

6. The heat exchanger system of claim 1 , wherein the one or more filter screens comprise a protective barrier within a protective opening.

7. The heat exchanger system of claim 6 , wherein the protective barrier comprises rigid cross beams spaced apart by openings.

8. The heat exchanger system of claim 7 , wherein the protective barrier further comprises a wire mesh screen extending between the rigid cross beams.

9. The heat exchanger system of claim 7 , wherein the protective barrier further comprises columns that intersect the rigid cross beams.

10. The heat exchanger system of claim 1 , wherein the one or more filter screens comprise an inlet filter screen at the inlet end.

11. The heat exchanger system of claim 10 , wherein the one or more filter screens further comprise an outlet filter screen at the outlet end.

12. The heat exchanger system of claim 1 , wherein the one or more filter screens are spaced apart from the heat transfer core.

13. The heat exchanger system of claim 1 , wherein the heat exchanger system is in fluid communication with a RAM air cooling system of an aircraft.

14. The heat exchanger system of claim 1 , wherein the heat transfer core and the one or more filter screens are slidably secured to slots of the securing frame.

15. The heat exchanger system of claim 1 , wherein the securing frame comprises a coupling wall having coupling portions configured to receive and removably retain one or more portions of the one or more filter screens and the heat transfer core.

16. The heat exchanger system of claim 15 , wherein the coupling wall comprises a fluid manifold configured to fluidly couple with one or more fluid couplers of the heat transfer core.

17. An aircraft comprising:
a RAM air cooling system; and
a heat exchanger system in fluid communication with the RAM air cooling system, the heat exchanger system comprising:
a securing frame;
a heat transfer core removably secured to the securing frame, wherein the heat transfer core comprises heat transfer panels removably coupled to the securing frame, wherein a size and shape of the heat transfer core is selectively changeable, and wherein the heat transfer panels comprise heat transfer fins separated by fluid channels, and fluid passages in fluid communication to form a fluid circuit that extends between a fluid inlet and a fluid outlet; and
one or more filter screens removably secured to the securing frame at one or both of an inlet end or an outlet end, wherein the heat transfer core is disposed between the inlet end and the outlet end, and wherein the one or more filter screens comprises a protective barrier within a protective opening.

18. The aircraft of claim 17 , wherein each of the heat transfer panels further comprises a plurality of segment modules removably coupled together.

19. The aircraft of claim 17 , wherein the one or more filter screens are spaced apart from the heat transfer core.

20. A method for a heat exchanger system, the method comprising:
removably securing heat transfer panels of a heat transfer core to a securing frame, wherein each of the heat transfer panels comprises a plurality of segment modules removably coupled together; and
removably securing one or more filter screens to the securing frame at one or both of an inlet end or an outlet end, wherein the heat transfer core is disposed between the inlet end and the outlet end.

21. The method of claim 20 , wherein a size and shape of the heat transfer core is selectively changeable.

Assignees

• Boeing Co

Inventors

• Chestine Ralph E

Classifications

• B64D2013/0674

  comprising liquid subsystems · CPC title

• B64D2013/0651

  comprising filters, e.g. dust filters · CPC title

• B64D2013/0618

  with arrangements for reducing or managing bleed air, using another air source, e.g. ram air · CPC title

• F28F2275/122

  by crimping, caulking or clinching · CPC title

• F28F2275/14

  by using form fitting connection, e.g. with tongue and groove · CPC title