Heat exchanger

Patent metadata

Field	Value
Publication number	US-2025035387-A1
Application number	US-202418766341-A
Country	US
Kind code	A1
Filing date	Jul 8, 2024
Priority date	Jul 25, 2023
Publication date	Jan 30, 2025
Grant date	—

Abstract

A layer of a plate-fin heat exchanger includes: an inlet side for receiving a fluid; an outlet side; a plurality of first fins each having a first end located at the inlet side and extending in a direction toward the outlet side to a second end to provide a plurality of first flow channels for the fluid; a plurality of second fins each having a first end adjacent to the second end of the plurality of first fins and extending from the second end of the plurality of first fins toward the outlet side to a second end to provide a plurality of second flow channels for the fluid; and a cavity provided in each of the plurality of first fins and/or each of the plurality of second fins at a boundary between the plurality of first fins and the plurality of second fins.

First claim

1 . A layer of a plate-fin heat exchanger comprising:
an inlet side for receiving a fluid; an outlet side; a plurality of first fins each having a first end located at the inlet side and extending in a direction toward the outlet side to a second end to provide a plurality of first flow channels for the fluid, a plurality of second fins each having a first end adjacent to the second end of each of the plurality of first fins and extending toward the outlet side to a second end to provide a plurality of second flow channels for the fluid, and a cavity provided in each of the plurality of first fins and/or each of the plurality of second fins at a boundary between the plurality of first fins and the plurality of second fins.

2 . The layer according to claim 1 , wherein the plurality of first fins comprise guard fins arranged to protect the plurality of second fins from impact.

3 . The layer according to claim 2 , wherein the plurality of first fins are formed of a stronger material than the plurality of second fins.

4 . The layer according to claim 1 , wherein the cavity is formed in an end surface of each of the first plurality of fins and/or each of the second plurality of fins, wherein the end surface is substantially perpendicular to a direction of the fluid in use.

5 . The layer according to claim 1 , wherein the plurality of first flow channels comprise a first geometry and the plurality of second flow channels comprise a second geometry different from the first geometry.

6 . The layer according to claim 5 , wherein the cavity is arranged to provide a transition region for air flow in use as air travels from the first geometry defined by the plurality of first fins and the second geometry defined by the plurality of second fins.

7 . The layer according to claim 5 , further comprising a plurality of third fins each having a first end adjacent to the second end of each of the plurality of second fins and extending to a second end at the outlet side to provide a plurality of third flow channels for the fluid, wherein the plurality of third flow channels comprise a third geometry which is the same as the first geometry.

8 . The layer according to claim 7 , wherein the cavity is a first cavity, and wherein the layer comprises a second cavity in each of the plurality of second fins and/or each of the plurality of third fins at the boundary between the plurality of second fins and the plurality of third fins.

9 . The layer according to claim 1 , wherein the cavity comprises a concave depression.

10 . The layer according to claim 1 , wherein the plurality of second fins comprise herringbone-shape fins.

11 . The layer according to claim 1 , further comprising a plurality of third fins each having a first end adjacent to the second end of each of the plurality of second fins and extending to a second end at the outlet side to provide a plurality of third flow channels for the fluid.

12 . The layer according to claim 11 , wherein the cavity is a first cavity, and wherein the layer comprises a second cavity in each of the plurality of second fins and/or each of the plurality of third fins at the boundary between the plurality of second fins and the plurality of third fins.

13 . The layer according to claim 11 , wherein the plurality of third fins are formed of the same material as the plurality of first fins.

14 . The layer according to claim 13 , wherein the plurality of third fins are arranged to protect the plurality of second fins from impact on the outlet side.

15 . A plate-fin heat exchanger comprising a plurality of layers as claimed in claim 1 .

16 . A method of manufacturing a layer of a heat exchanger as claimed in claim 1 , the method comprising:
providing a base plate; connecting the plurality of first fins to the base plate; connecting the plurality of second fins to the base plate; joining the second end of each of the plurality of first fins to the first end of each of the plurality of second fins; forming the cavity in each of the plurality of first fins and/or each of the plurality of second fins at the boundary between the plurality of first fins and the plurality of second fins.

17 . The method as claimed in claim 16 , wherein the step of forming the cavity comprises using machining techniques including one of cutting, milling or abrasion.

18 . The method as claimed in claim 16 , wherein the plurality of first fins and the plurality of second fins are formed separately using additive manufacturing techniques, and then are joined together by welding or brazing.

19 . The method as claimed in claim 16 , wherein the plurality of first fins and the plurality of second fins are formed as a single unit using additive manufacturing techniques, the plurality of first fins being formed with a thicker profile to provide more stiffness than the plurality of second fins.

20 . The method as claimed in claim 16 , wherein forming the cavity in each of the plurality of first fins and/or each of the plurality of second fins is achieve by forming the plurality of first fins and the plurality of second fins using additive manufacturing techniques with the cavity already present.

Assignees

• Hs Marston Aerospace Ltd

Inventors

• Mccormick John Patrick
• Mcnab Christopher Arthur
• Pollard Berwyn Owain
• Astley Stuart Anthony

Classifications

• B23P15/26

  heat exchangers {or the like (making heat exchangers by methods covered by other subclasses B21D53/02)} · CPC title

• F28F3/06 Primary

  the means being attachable to the element · CPC title

• F28F2215/04

  Assemblies of fins having different features, e.g. with different fin densities · CPC title

• F28F2265/00

  Safety or protection arrangements; Arrangements for preventing malfunction · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title