Low drag skin heat exchanger

Patent metadata

Field	Value
Publication number	US-10059435-B2
Application number	US-201514959366-A
Country	US
Kind code	B2
Filing date	Dec 4, 2015
Priority date	Dec 4, 2014
Publication date	Aug 28, 2018
Grant date	Aug 28, 2018

Abstract

A heat exchanger including a heat exchange panel having an exterior surface that forms an exterior surface portion of the vehicle (e.g. an aircraft), and including one or more vortex generators protruding from the exterior surface. The heat exchange panel has at least a portion made of a thermally conductive material. The one or more vortex generators are configured to direct airflow to particular areas on the aircraft, which may then prevent large scale airflow separation to synergistically enhance heat removal from the heat exchange panel and reduce drag of air flowing over the exterior surface.

First claim

What is claimed is:

1. A vehicle including:
a heat exchange panel having an exterior surface forming an exterior surface portion of the vehicle, the exterior surface having at least a portion made of a thermally conductive material; and
one or more vortex generators protruding from the exterior surface and configured to prevent separation of flow to reduce drag of air flowing over the exterior surface of the heat exchange panel as the vehicle travels in a forward direction.

2. The vehicle of claim 1 , wherein the exterior surface is thermally connected to a heat generating device.

3. The vehicle of claim 2 , wherein the exterior surface and the heat generating device are connected through one or more fluid carrying conduits.

4. The vehicle of claim 2 , wherein the heat generating device includes a fuel cell emergency power system that is thermally connected to the exterior surface.

5. The vehicle of claim 1 , wherein the vehicle is an aircraft.

6. The aircraft of claim 5 , wherein the one or more vortex generators are disposed along a fuselage of the aircraft.

7. The aircraft of claim 5 , wherein the one or more vortex generators are disposed at a junction of an empennage upsweep and a main body of the aircraft.

8. A heat exchanger for a vehicle, the heat exchanger comprising:
a panel having an exterior surface and an internal flow path for flow of a heat exchange fluid that transfers heat to a thermally conductive portion of the exterior surface, and
one or more vortex generators protruding from the exterior surface of the panel to reduce drag.

9. The heat exchanger of claim 8 , wherein the panel is configured for mounting to an aircraft at the exterior of the aircraft.

10. The heat exchanger of claim 9 , wherein the panel has an exterior wall forming the exterior surface, and a plurality of fins extend from an inner surface of the exterior wall into the internal flow path.

11. The heat exchanger of claim 8 , wherein the panel has a fluid inlet and a fluid outlet for receiving and returning the heat exchange fluid that extracts heat from a heat generating device.

12. The heat exchanger of claim 8 , further including one or more internal flow passages in at least one of the one or more vortex generators, wherein each internal flow passage is fluidly connected to the internal flow path.

13. The heat exchanger of claim 8 , further including one or more additional internal flow paths for directing fluid flowing within the panel.

14. The heat exchanger of claim 13 , wherein the one or more additional flow paths extend between the exterior surface and an interior surface of the panel.

15. The heat exchanger of claim 13 , wherein the one or more additional flow paths are fluidly connected with an inlet and an outlet of the panel.

16. An aircraft including the heat exchanger of any one of claim 8 , wherein the one or more vortex generators are disposed along a fuselage of the aircraft.

17. A heat exchanger including:
a heat exchange panel having an exterior surface forming an exterior surface portion of a vehicle, the exterior surface having at least a portion made of a thermally conductive material; and
one or more vortex generators protruding from the exterior surface and configured to prevent separation of flow to reduce drag of air flowing over the exterior surface of the heat exchange panel.

18. The heat exchanger of claim 17 , wherein the heat exchange panel has an exterior wall forming the exterior surface, and a plurality of fins extend from an inner surface of the exterior wall into an internal flow passage.

19. An aircraft including the heat exchanger of claim 17 , wherein the one or more vortex generators are disposed along a fuselage of the aircraft.

20. The heat exchanger of claim 17 , wherein each of the vortex generators has a sloped profile to reduce drag.

Assignees

• Parker Hannifin Corp

Inventors

• Daggett David Lee
• Utendorf Randy
• Lawson Irwin

Classifications

• B64D33/10

  Radiator arrangement · CPC title

• Y02T90/36

  Cross-Sectional Technologies · mapped topic

• B64D2041/005

  Fuel cells · CPC title

• B64C23/005 Primary

  by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds · CPC title

• Y02T50/162

  Cross-Sectional Technologies · mapped topic