Synthetic jet driven cooling device with increased volumetric flow

Patent metadata

Field	Value
Publication number	US-9976762-B2
Application number	US-201313871353-A
Country	US
Kind code	B2
Filing date	Apr 26, 2013
Priority date	Mar 14, 2013
Publication date	May 22, 2018
Grant date	May 22, 2018

Abstract

A synthetic jet driven cooling device includes at least one synthetic jet actuator to generate and project a series of fluid vortices. A manifold coupled to the synthetic jet actuator(s) receives the fluid vortices and generates a primary air stream. An air amplifier connected to the manifold by a connecting pipe receives the primary air stream. The air amplifier includes an air intake oriented perpendicular to the connecting pipe and an air outlet positioned opposite the air intake, with a venturi section positioned between the air intake and air outlet that has a diameter smaller than the air intake diameter. A low pressure region in a center of the venturi section entrains a surrounding air in through the air intake to generate a secondary air stream that combines with the primary air stream to generate a combined air flow that flows through the venturi and exits the air outlet.

First claim

What is claimed is:

1. A synthetic jet driven cooling device comprising:
at least one synthetic jet actuator configured to generate and project a series of fluid vortices, each of the at least one synthetic jet actuators comprising an orifice through which the series of fluid vortices are projected;
a manifold coupled to the at least one synthetic jet actuator so as to receive the series of fluid vortices from the orifice of the at least synthetic jet actuator, the series of fluid vortices from the at least one synthetic jet actuator generating a primary air stream;
an air amplifier connected to the manifold by way of a connecting pipe so as to receive the primary air stream, the air amplifier comprising:
an air intake positioned at a first end of the air amplifier and having a first diameter, with the air intake being oriented perpendicular to an outlet of the connecting pipe;
an air outlet positioned at a second end of the air amplifier opposite from the first end; and
a venturi section positioned between the air intake and the air outlet and having a second diameter that is less than the first diameter;

wherein a low pressure region in a center of the venturi section entrains a surrounding air in through the air intake to generate a secondary air stream, the secondary air stream combining with the primary air stream to provide a combined air flow that flows through the venturi and exits the air outlet; and
wherein each of the at least one synthetic jet actuators comprises:
a first plate;
a second plate spaced apart from the first plate and arranged parallelly thereto;
a wall coupled to and positioned between the first and second plates to form a chamber and including the orifice therein; and
a piezoelectric actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof, thereby changing a volume within the chamber so that the series of fluid vortices are generated and projected out from the orifice of the wall.

2. The cooling device of claim 1 wherein the outlet of the connecting pipe is coupled to the air amplifier at a throat of the venturi section that tapers the air amplifier down from the first diameter of the air intake to the second diameter of the venturi section.

3. The cooling device of claim 2 wherein, upon exiting the connecting pipe, the primary air stream is caused to flow in proximity to a surface of the venturi section of the air amplifier due to the coanda effect.

4. The cooling device of claim 1 wherein the venturi section of the air amplifier causes a velocity of the primary air stream to increase as it passes therethrough due to the venturi effect, thereby also forming the low pressure region in the center of the venturi section.

5. The cooling device of claim 1 wherein the combined air flow that exits the air outlet of the air amplifier has a higher velocity and volumetric flow rate than the primary air stream generated from the series of fluid vortices from the at least one synthetic jet actuator.

6. The cooling device of claim 5 wherein the volumetric flow rate of the combined air stream is 15 to 20 times greater than that of the primary air stream.

7. The cooling device of claim 1 wherein the air outlet of the air amplifier is positioned adjacent a heat source, such that the combined air flow provides cooling to the heat source.

8. The cooling device of claim 1 wherein the air amplifier comprises a micro-venturi device configured to fit within volume constraints imposed by a microelectronics circuit package that is being cooled.

9. The cooling device of claim 1 wherein the at least one synthetic jet actuator comprises a plurality of synthetic jet actuators arranged in a vertically stacked configuration, with the orifice of each of the plurality of synthetic jet actuators being aligned with other orifices such that the series of fluid vortices projected from each synthetic jet actuator is directed into the manifold.

10. A hybrid coanda-venturi cooling device comprising:
at least one synthetic jet actuator, each of the at least one synthetic jet actuators configured to generate and project a series of fluid vortices out from an orifice thereof;
a manifold coupled to the at least one synthetic jet actuator so as to receive the series of fluid vortices therefrom, the series of fluid vortices from the at least one synthetic jet actuator generating a primary air stream;
an air amplifier connected to the manifold so as to receive the primary air stream, the air amplifier comprising a venturi section having a reduced cross-sectional area as compared to an air intake of the air amplifier;
wherein a coanda effect acting on the primary air stream as it enters the air amplifier and a venturi effect caused by the venturi section of the air amplifier causes a fluid surrounding the air intake to be entrained into the air intake to generate a secondary air stream, the secondary air stream combining with the primary air stream to provide a combined air flow that exits an air outlet of the air amplifier;
wherein the at least one synthetic jet actuator comprises a plurality of synthetic jet actuators arranged in a vertically stacked configuration, with the orifice of each of the plurality of synthetic jet actuators being aligned with other orifices such that the series of fluid vortices projected from each synthetic jet actuator is directed into the manifold; and
wherein each of the at least one synthetic jet actuators comprises:
a first plate;
a second plate spaced apart from the first plate and arranged parallelly thereto;
a wall coupled to and positioned between the first and second plates to form a chamber and including the orifice therein; and
a piezoelectric actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof, thereby changing a volume within the chamber so that the series of fluid vortices are generated and projected out from the orifice of the wall.

11. The cooling device of claim 10 wherein the primary air stream enters the air amplifier in a direction generally perpendicular to the air intake of the air amplifier and at a throat of the venturi section.

12. The cooling device of claim 11 wherein the throat of the venturi section tapers the air amplifier down from a first diameter at the air intake to a second diameter of the venturi section that is less than the first diameter.

13. The cooling device of claim 10 wherein the coanda effect acting on the primary air stream as it enters the air amplifier causes the primary air stream to flow in proximity to a surface of the venturi section of the air amplifier.

14. The cooling device of claim 10 wherein the venturi section of the air amplifier causes a velocity of the primary air stream to increase as it passes therethrough due to the venturi effect, thereby also forming a low pressure region in a center of the venturi section that causes the fluid surrounding the air intake to be entrained into the air intake.

15. The cooling device of claim 10 wherein the combined air flow that exits the air outlet of the air amplifier has a higher velocity and volumetric flow rate than the primary air stream generated from the series of fluid vortices from the at least one synthetic jet actuator.

16. A method of manufacturing a synthetic jet cooling device comprising:
providing one or more synthetic jet actuators each configured to generate and project a series of fluid vortices out from an orifice thereof;
coupling a manifold to the one or more synthetic jet actuators so as to receive the series of fluid vo

Assignees

• Gen Electric

Inventors

• Giammattei Mark Howard
• Weaver Stanton Earl
• Chamarthy Pramod

Classifications

• H10W40/43

  by flowing gases, e.g. forced air cooling · CPC title

• Y10T29/49359

  Cooling apparatus making, e.g., air conditioner, refrigerator · CPC title

• H01L2924/0002

  Electricity · mapped topic

• H01L2924/00

  Electricity · mapped topic

• H01L23/467

  Electricity · mapped topic