Heat exchanger having aerodynamic features to improve performance

Patent metadata

Field	Value
Publication number	US-10809009-B2
Application number	US-201715783561-A
Country	US
Kind code	B2
Filing date	Oct 13, 2017
Priority date	Oct 14, 2016
Publication date	Oct 20, 2020
Grant date	Oct 20, 2020

Abstract

A gas-liquid heat exchanger such as a charge air cooler has a core comprising a stack of flat tubes defining liquid coolant flow passages, and a plurality of open-ended gas flow passages between the flat tubes. An endmost gas flow passage is defined between an end plate of the core and an adjacent flat tube, such that the endmost gas flow passage is in contact with only said adjacent one of said flat tubes. A blocking element extends along either the front face or the rear face of the core and at least partly blocking the endmost gas flow passage. Each flat tube may comprise a pair of core plates, at least one including a flap projecting into a gas flow passage and covering a gas bypass channel between the edge of the turbulence-enhancing insert and the sides of a coolant manifold.

First claim

What is claimed is:

1. A gas-liquid heat exchanger comprising a heat exchanger core having a top, a bottom, a pair of sides, an open front face and an open rear face, wherein a gas flow direction is defined through the core from the front face to the rear face, the sides of the core extending parallel to the gas flow direction, and
wherein the core has a height defined between its top and bottom;
wherein the core comprises:
a plurality of flat tubes stacked in parallel relation to one another, each of the flat tubes enclosing a liquid flow passage for circulation of a liquid coolant;
a plurality of gas flow passages, each of which is defined in a space between an adjacent pair of said flat tubes, wherein the gas flow passages are open at the front face and the rear face of the core, and wherein the gas flow passages are provided with turbulence-enhancing inserts;
wherein each of the flat tubes comprises a pair of core plates joined together at their peripheral edges to enclose and define a coolant flow passage;
each of the core plates including a pair of bosses defining coolant manifold openings, wherein the bosses are aligned throughout the height of the core to define coolant inlet and outlet manifolds,
wherein the coolant inlet and outlet manifolds are aligned along the gas flow direction, spaced apart from one another along the gas flow direction, and spaced inwardly from the sides of the core; and
wherein each of the turbulence-enhancing inserts has a first section with a first peripheral edge extending in the gas flow direction and located adjacent to a first side of the inlet and outlet manifolds, and a second section with a second peripheral edge extending in the gas flow direction and located adjacent to an opposite, second side of the inlet and outlet manifolds;
wherein at least one of the core plates in each of the flat tubes includes a flap projecting into one of the gas flow passages, and positioned to cover a gas bypass channel extending lengthwise from the front face to the rear face of the core and extending widthwise between the first peripheral edge of the first section of the turbulence-enhancing insert and the second peripheral edge of the second section of the turbulence-enhancing insert;
wherein the flap is provided in a space between the inlet and outlet manifolds, and extends transversely to the gas flow direction between the first peripheral edge of the first section of the turbulence-enhancing insert and the second peripheral edge of the second section of the turbulence-enhancing insert;
such that the flap is spaced inwardly from the sides of the core and spaced inwardly from the front and rear faces of the core.

2. The gas-liquid heat exchanger of claim 1 , wherein the flap has a free end which engages or is in close proximity to a surface of an adjacent one of said flat tubes.

3. The gas-liquid heat exchanger of claim 1 , wherein each said pair of core plates comprises a first core plate and a second core plate;
wherein the flap is formed in the first core plate, the first core plate further comprising a hole adjacent to the flap, the hole having a periphery with a size and shape corresponding to a size and shape of the flap;
wherein the second core plate includes a flow separation rib separating the bosses and extending transversely to the gas flow direction, wherein the flow separation rib has a sealing surface which is sealed to the first core plate;
wherein the flow separation rib has a widened portion located between the bosses, wherein the sealing surface has sufficient dimensions in the widened portion of the rib so as to surround and sealingly engage the periphery of the hole in the first core plate.

4. The gas-liquid heat exchanger of claim 3 , wherein the widened portion of the flow separation rib includes a trough which is surrounded by the sealing surface, wherein the trough of one said plate pair is in close proximity to or in engagement with the flap of an adjacent one of said plate pairs.

5. The gas-liquid heat exchanger of claim 1 , wherein:
both of the core plates of each said pair includes two of said flaps, each of the core plates further comprising a hole located adjacent to and between said two flaps, the hole having a periphery surrounded by a sealing surface;
wherein the sealing surface surrounding the hole of one said core plate seals to the sealing surface surrounding the hole of the other one of the core plates comprising said pair of plates.

6. The gas-liquid heat exchanger of claim 5 , wherein the flaps each have a height which is substantially the same as a height of the bosses.

7. The gas-liquid heat exchanger of claim 5 , wherein each of the core plates includes a flow separation rib separating the bosses and extending transversely to the gas flow direction, the flow separation rib having a sealing surface, wherein the sealing surface of the flow separation rib of one said core plate is sealed to the sealing surface of the flow separation rib of the other one of the core plates comprising said pair of plates.

8. The gas-liquid heat exchanger of claim 7 , wherein the sealing surface surrounding the hole in each of the core plates is part of the sealing surface of the flow separation rib, and is provided in a widened portion of the flow separation rib located between the bosses.

Assignees

• Dana Canada Corp

Inventors

• Schouten Eric J
• Stevens Cameron L M
• Kenney Benjamin A
• Kinder Lee M

Classifications

• F28D9/0043

  the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another · CPC title

• F28F13/06

  by affecting the pattern of flow of the heat-exchange media {(F28F13/003 takes precedence; static flow control means in header boxes F28F9/026)} · CPC title

• F28F2230/00

  Sealing means · CPC title

• F28F9/22

  Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates · CPC title

• F28D2021/0082

  Charged air coolers · CPC title