Electro hydro dynamic cooling for heat sink

1. An Electro Hydro Dynamic (EHD) thruster configured to be electrically isolated from a heat sink and to generate an airflow of ionized air for cooling the heat sink, the EHD thruster comprising:

a first set of electrodes comprising multiple parallel electrodes;

a second set of electrodes comprising multiple parallel electrodes; wherein at least one of the multiple parallel electrodes of the second set of electrodes has a base portion and multiple tip portions extending from the base portion, the base portion is oriented substantially perpendicular to the first set of electrodes and the tip portions extending from the base portion are substantially parallel to the first set of electrodes; and

a supporting structure comprising a containing space formed by side walls for supporting the first and second sets of electrodes disposed inside the containing space.

2. The EHD thruster according to claim 1 , wherein the EHD thruster is configured to generate a push airflow in a first direction through a first part of the heat sink and a pull airflow through a second part of the heat sink.

3. The EHD thruster according to claim 1 , wherein the cooling airflow of the EHD thruster is adjustable by adjusting Direct Currency (DC) voltage feed, based on an estimation of a temperature of a heat source thermally connected to the heat sink.

4. The EHD thruster according to claim 1 , wherein any electrode within the first set of electrodes, or the second set of electrodes is made of metal or dielectric material covered by a metalized surface.

5. The EHD thruster according to claim 1 , wherein the first set of electrodes comprises multiple line electrodes.

6. The EHD thruster according to claim 1 , wherein the multiple tip portions of said at least one of the multiple parallel electrodes in the second set of electrodes are displaced with regard to the first set of electrodes, in a first direction of the airflow.

7. The EHD thruster according to claim 1 , wherein the first set of electrodes comprises at least one bar electrode arranged perpendicular to the second set of electrodes.

8. The EHD thruster according to claim 1 , wherein the supporting structure is open in the first direction towards the first part of the heat sink and is open in a second direction towards the second part of the heat sink, for enabling natural convection cooling of the heat sink when the EHD thruster is switched off.

9. The EHD thruster according to claim 1 , wherein the second set of electrodes is connected to negative voltage and the first set of electrodes is connected to either positive voltage or ground; or wherein the second set of electrodes is connected to positive voltage and the first set of electrodes is connected to either negative voltage or ground.

10. The EHD thruster according to claim 1 , wherein the supporting structure is electrically isolated from the first and second sets of electrodes and is metalized for protecting nearby electronic equipment from electromagnetic interference.

11. The EHD thruster according to claim 1 , wherein the supporting structure comprises at least one grid for enclosing at least one of the groups of (a) the first set of electrodes and (b) the second set of electrodes, while enabling natural convection cooling of the heat sink by allowing the airflow through the supporting structure.

12. The EHD thruster according to claim 1 , wherein the heat sink comprises a first part and a second part, and wherein the heat sink comprises a compartment, and wherein the EHD thruster is adapted to be placed the compartment for providing a push airflow in a first direction through the first part of the heat sink and a pull airflow through the second part of the heat sink.

13. The EHD thruster according to claim 1 , wherein the heat sink comprises a heat base and heat sink fins, wherein the heat sink fins comprises a first fin assembly and a second fin assembly, and wherein the EHD thruster is adapted to be placed on the heat base between the first fin assembly and the second fin assembly.

14. A method in a control unit for controlling airflow generation of an Electro Hydro Dynamic (EHD) thruster configured to be electrically isolated from a heat sink and to generate an airflow of ionized air for cooling the heat sink, the method comprising:

estimating temperature of a heat source thermally connected to the heat sink to be cooled;

comparing the estimated temperature with a threshold limit; and

adjusting the voltage feed level of a Direct Currency (DC) power supply unit to the first and second sets of electrodes, based on the comparison;

wherein the EHD thruster comprises:

a first set of electrodes comprising multiple parallel electrodes;

a second set of electrodes comprising multiple parallel electrodes; wherein at least one of the multiple parallel electrodes of the second set of electrodes has a base portion and multiple tip portions extending from the base portion, the base portion is oriented substantially perpendicular to the first set of electrodes and the tip portions extending from the base portion are substantially parallel to the first set of electrodes; and

a supporting structure comprising a containing space formed by side walls for supporting the first and second sets of electrodes disposed inside the containing space.

15. The method according to claim 14 , wherein the adjustment of the voltage feed level comprises generating pulse width modulation signals in the control unit and transmitting the pulse width modulation signals to the DC power supply unit, which is enabled to accordingly adjust DC current feed to the first and second sets of electrodes of the EHD thruster.

16. The method according to claim 14 , wherein said airflow comprises a pull airflow enabled by the EHD thruster, placed between the first part and the second part of the heat sink, by decreasing local air pressure resulting in a cold airstream through the heat sink.

17. A system comprising an Electro Hydro Dynamic (EHD) thruster and a heat sink, wherein the EHD thruster is configured to be electrically isolated from the heat sink and to generate an airflow of ionized air for cooling the heat sink, wherein the EHD thruster comprises:

a first set of electrodes comprising multiple parallel electrodes;

a second set of electrodes comprising multiple parallel electrodes; wherein at least one of the multiple parallel electrodes of the second set of electrodes has a base portion and multiple tip portions extending from the base portion, the base portion is oriented substantially perpendicular to the first set of electrodes and the tip portions extending from the base portion are substantially parallel to the first set of electrodes; and

a supporting structure comprising a containing space formed by side walls for supporting the first and second sets of electrodes disposed inside the containing space.

18. The system comprising the EHD thruster according to claim 17 , wherein

the heat sink is electrically grounded and comprises a first part and a second part, a compartment for holding the EHD thrusters for providing a push airflow in a first direction through the first part of the heat sink and a pull airflow through the second part of the heat sink.

19. The system according to claim 17 , further comprising a Direct Currency (DC) power supply unit configured for providing a DC current to the first and second sets of electrodes of the EHD thruster.

20. The system according to claim 19 , also comprising a control unit, and wherein the DC power supply unit is configured to convert a DC input to a variable higher voltage DC output, where the level of the higher voltage DC output is controlled by the control unit.

21. The system according to claim 19 , further comprising a short cut detector and wherein the DC power supply unit is configured to disable the voltage feed when a short cut behaviour is detected and to enable the voltage feed of the DC power supply unit when no short cut is detected.

22. The system according to claim 17 , wherein the heat sink comprises a heat base and heat sink fins, wherein the heat sink fins comprises a first fin assembly and a second fin assembly, and wherein the EHD thruster is adapted to be placed on the heat base between the first fin assembly and the second fin assembly.

23. A method for cooling a heat sink comprising:

electrically isolating an Electro Hydro Dynamic (EHD) thruster from the heat sink;

generating, by the EHD thruster, an airflow of ionised air for cooling the heat sink,

wherein the EHD thruster comprises:

a first set of electrodes comprising multiple parallel electrodes;

a second set of electrodes comprising multiple parallel electrodes, wherein at least one of the multiple parallel electrodes of the second set of electrodes has a base portion and multiple tip portions extending from the base portion the base portion is oriented substantially perpendicular to the first set of electrodes and the tip portions extending from the base portion are substantially parallel to the first set of electrodes; and

a supporting structure comprising a containing space formed by side walls for supporting the first and the second sets of electrodes disposed inside the containing space.

24. The method according to claim 23 , further comprising:

estimating a temperature of a heat source thermally connected to the heat sink to be cooled;

comparing the estimated temperature with a threshold limit; and

adjusting the voltage feed level to the first and second sets of electrodes, based on the comparison.

25. The method according to claim 24 wherein the adjustment of the voltage feed level comprises: generating and transmitting pulse width modulation signals to a DC power supply unit, which is enabled to accordingly adjust DC current feed to the first and second sets of electrodes of the EHD thruster.

26. The method according to claim 23 , wherein said airflow comprises a pull airflow enabled by the EHD thruster, placed between the first part and the second part of the heat sink, by decreasing local air pressure resulting in a cold airstream through the heat sink.