High-performance heat exchanger with calibrated bypass

Patent metadata

Field	Value
Publication number	US-11976894-B2
Application number	US-202217984710-A
Country	US
Kind code	B2
Filing date	Nov 10, 2022
Priority date	Oct 19, 2020
Publication date	May 7, 2024
Grant date	May 7, 2024

Abstract

A heat exchanger assembly includes a cooling plate with at least one outer heat transfer surface adapted for thermal contact with one or more heat-generating substrates. A fluid flow path extends from an inlet port to an outlet port, with a plurality of cooling zones spaced apart along the fluid flow path, each cooling zone including a heat transfer element such as a corrugated fin sheet in contact with the inner surface of the first plate wall. Manifold spaces are defined proximate to the inlet and outlet ports, and between adjacent cooling zones. One or more bypass flow passages are provided between upstream and downstream ends of at least one cooling zone, to divert a portion of the heat transfer fluid from flowing through the cooling zone. The volume of fluid flow bypassing one or more cooling zones is calibrated to improve temperature uniformity of the heat-generating substrates.

First claim

What is claimed is:

1. A heat exchanger assembly comprising a cooling plate with an outer heat transfer surface adapted for thermal contact with one or more heat-generating substrates, the outer heat transfer surface having an area defined in a first plane, the cooling plate having a thickness defined in a second plane which is perpendicular to the first plane;
the cooling plate comprising:
a first plate wall and a second plate wall spaced apart in the second plane, the first and second plate walls each having an inner surface and an outer surface, wherein the inner surfaces of the first and second plate walls face each other, and wherein the outer heat transfer surface is defined by the outer surface of the first plate wall;
a hollow interior defined between the first and second plate walls;
a fluid flow space defined in the hollow interior;
an inlet port and an outlet port spaced apart in the first plane and in fluid communication with the fluid flow space, wherein a fluid flow path is defined in the fluid flow space from the inlet to the outlet;
a plurality of cooling zones defined along the fluid flow path, wherein the cooling zones are spaced apart from one another along the fluid flow path, each cooling zone having an upstream end for receiving a heat transfer fluid flowing along the fluid flow path and a downstream end for discharging the heat transfer fluid along the fluid flow path, wherein each said cooling zone comprises one or more heat transfer elements which are in contact with the inner surface of the first plate wall;
a plurality of manifold spaces in the hollow interior, including an inlet manifold space proximate to the inlet, an outlet manifold space proximate to the outlet, and at least one intermediate manifold space, each said intermediate manifold space comprising a gap between the downstream end of one said cooling zone and the upstream end of an adjacent said cooling zone;
a bypass flow passage extending between the upstream and downstream ends of one of said cooling zones and adapted to divert a portion of the heat transfer fluid from flowing through the cooling zone, wherein a resistance to fluid flow through the bypass flow passage is lower than a resistance to fluid flow through the cooling zone, due to the presence of said one or more heat transfer elements in the cooling zone, and
wherein the bypass flow passage includes at least one inlet opening for receiving said portion of the heat transfer fluid from one said manifold space at the upstream end of the cooling zone and at least one outlet opening for discharging said portion of the heat transfer fluid into another said manifold space at the downstream end of the cooling zone.

2. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages, and wherein a volume of bypass flow for a first said cooling zone is different from a volume of bypass flow for a second said cooling zone, depending on the amount of cooling required in the first and second cooling zones.

3. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages, and wherein at least one said bypass flow passage is provided for each of the cooling zones except for the cooling zone closest to the outlet opening, such that substantially all the heat transfer fluid flows through the cooling zone closest to the outlet opening.

4. The heat exchanger assembly of claim 1 , wherein at least one of said cooling zones is provided with a plurality of said bypass flow passages.

5. The heat exchanger assembly of claim 1 , wherein each of said heat transfer elements comprises a corrugated fin sheet comprising a plurality of spaced sidewalls extending along the fluid flow path, and comprising top and bottom walls which join adjacent sidewalls together;
wherein the top walls are in direct contact with the inner surface of the first plate wall, and the bottom walls are spaced from the inner surface of the second plate wall; and
wherein the bypass flow passage is defined within a space between the bottom wall of a corrugated fin sheet and the inner surface of the second plate wall.

6. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages;
wherein each of the bypass flow passages has first and second opposite ends, with the at least one inlet opening located at the first end, and the at least one outlet opening located at the opposite second end.

7. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages;
wherein the inner surface of the second plate wall comprises a plurality of grooves, each of which defines one of the bypass flow passages, wherein each of the bypass flow passages has an inlet opening and an outlet opening defined at opposite ends of one of the grooves.

8. The heat exchanger assembly of claim 7 , wherein the second plate wall forms part of an embossed plate, and wherein the grooves comprise rib-like embossments formed in the second plate wall.

9. The heat exchanger assembly of claim 8 , wherein the one or more heat transfer elements in each said cooling zone are in direct contact with portions of the inner surface of the second plate wall surrounding the bypass flow passages.

10. The heat exchanger assembly of claim 7 , further comprising an orifice plate sandwiched between the heat transfer elements and the grooves formed in the inner surface of the second plate wall, wherein the orifice plate includes a plurality of spaced-apart inlet and outlet apertures, wherein each said inlet aperture defines the inlet openings of one or more of said bypass flow passages, and each said outlet aperture defines the outlet openings of one or more of said bypass flow passages.

11. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages, and wherein one or more of the bypass flow passages is angled relative to a longitudinal axis of the cooling plate.

12. The heat exchanger assembly of claim 1 , wherein the cooling plate includes a plurality of said bypass flow passages, and wherein the bypass flow passages are spaced apart from each other.

13. The heat exchanger assembly of claim 1 , wherein the plurality of cooling zones includes a first cooling zone and a second cooling zone separated by one said intermediate manifold space, each of the first and second cooling zones including at least one said bypass flow passage;
wherein each of the bypass flow passages has a first end and an opposite second end, the at least one inlet opening located at the first end, and the at least one outlet opening at the opposite second end; and
wherein the first end of each said bypass flow passage of the first cooling zone is spaced apart from the second end of each said bypass flow passage of the second cooling, across the intermediate manifold space.

Assignees

• Dana Canada Corp

Inventors

• Vanderwees Doug
• Abels Kenneth M A

Classifications

• F28F3/12 Primary

  Elements constructed in the shape of a hollow panel, e.g. with channels {(F28D1/02, F28D1/03 take precedence)} · CPC title

• F28D1/0308 Primary

  the conduits being formed by paired plates touching each other (F28D1/0358 takes precedence) · CPC title

• F28D21/00

  Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00 · CPC title

• F28F3/044

  the deformations being pontual, e.g. dimples · CPC title

• F28F3/027

  with openings, e.g. louvered corrugated fins; Assemblies of corrugated strips · CPC title