Synthetic jet driven cooling device with increased volumetric flow

• US 9,976,762 B2
• Filed: 04/26/2013
• Issued: 05/22/2018
• Est. Priority Date: 03/14/2013
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Giammattei, Mark Howard, Weaver, Stanton Earl, Chamarthy, Pramod
• Primary Examiner(s): McAllister, Steven B
• Assistant Examiner(s): Miller, Samantha
• Application Number:
  US13/871,353
• Publication Number:
  US 20140273796A1
• Time in Patent Office: 1,852 Days
• Field of Search: 454251, 2391022, 165 803
• CPC Class Codes: F04B 23/10 at least one pump being of the reciprocating positive-displacement type
• CPC Class Codes: F04F 5/16 displacing elastic fluids
• CPC Class Codes: F24F 7/007 with forced flow using ducting systems F24F7/06
• CPC Class Codes: H01L 23/467 by flowing gases, e.g. air H01L23/473 takes precedence
• CPC Class Codes: H01L 2924/00 Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
• CPC Class Codes: H01L 2924/0002 Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
• CPC Class Codes: Y10T 29/49359 Cooling apparatus making, e.g., air conditioner, refrigerator

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.

Claims

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 vortices from the orifices of the synthetic jet actuators, the series of fluid vortices from the one or more synthetic jet actuators generating a primary air stream;

connecting an air amplifier to the manifold by way of a connecting pipe so as to receive the primary air stream from the manifold, the air amplifier comprising a venturi section having a reduced cross-sectional area as compared to an air intake of the air amplifier;

wherein connection of the air amplifier to the one or more synthetic jet actuators generates an air flow output from the air amplifier having a higher velocity and volumetric flow rate than the primary air stream generated from the one or more synthetic jet actuators;

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 the air flow output that exits an air outlet of the air amplifier; and

wherein connecting the air amplifier to the manifold comprises connecting an outlet of the connecting pipe to the air amplifier at a throat of the venturi section, with the outlet of the connecting pipe being oriented perpendicular to the air intake of the air amplifier, such that the primary air stream is subject to the coanda effect and venturi effect.

17. The cooling system of claim 16 wherein the one or more synthetic jet actuators comprises a plurality of synthetic jet actuators, and wherein the method further comprises arranging the plurality of synthetic jet actuators into a synthetic jet stack and such that the orifices of the plurality of synthetic jet actuators are aligned.