SYSTEM AND METHOD FOR COOLING COMPONENTS OF A SURGICAL NAVIGATION SYSTEM

• US 20110137152A1
• Filed: 12/03/2009
• Published: 06/09/2011
• Est. Priority Date: 12/03/2009
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Li, Dun Alex
• Application Number:
  US12/630,551
• Publication Number:
  US 20110137152A1
• Time in Patent Office: Days
• US Class Current: 600/424
• CPC Class Codes: A61B 2560/0242 adapted to measure environmental factors, e.g. temperature, pollution
• CPC Class Codes: A61B 5/062 using magnetic field

Abstract

In one embodiment, a surgical navigation system is provided with a transmitter assembly that includes at least one coil for creating an electromagnetic field in the vicinity of a surgical operation. The surgical navigation system also includes a cooling unit thermally coupled to the transmitter assembly for dissipating heat generated by the transmitter assembly and a receiver assembly that includes at least one coil configured to generate signals induced by the field. The surgical navigation system further includes electronic circuitry coupled to and communicating with the transmitter assembly and the receiver assembly for calculating at least a position of the receiver coil.

Claims

1. A surgical navigation system comprising:

a transmitter assembly comprising at least one coil for creating an electromagnetic field in the vicinity of a surgical operation;

a cooling unit thermally coupled to the transmitter assembly for dissipating heat generated by the transmitter assembly;

a receiver assembly comprising at least one coil configured to generate signals induced by the field; and

electronic circuitry coupled to and communicating with the transmitter assembly and the receiver assembly for calculating at least a position of the receiver coil.

2. The surgical navigation system of claim 1, wherein the cooling unit comprises a plurality of semiconductor thermocouples.

3. The surgical navigation system of claim 2, wherein the semiconductor thermocouples are powered by a controller to generate both an endothermic end and an exothermic end on each of the semiconductor thermocouples.

4. The surgical navigation system of claim 3, wherein the endothermic ends of the semiconductor thermocouples are connected to the transmitter assembly and the exothermic ends of the semiconductor thermocouples are connected to a heat sink.

5. The surgical navigation system of claim 1, wherein the cooling unit comprises a heat sink that is air cooled or water-cooled.

6. The surgical navigation system of claim 1, further comprising a temperature sensor.

7. The surgical navigation system of claim 6, wherein the temperature sensor is electronically coupled to and communicating with a controller configured for regulating the temperature of the transmitter assembly.

8. The surgical navigation system of claim 7, wherein the controller is configured to regulate the temperature of the transmitter assembly independent of user input.

9. The surgical navigation system of claim 6, wherein the temperature sensor is coupled to circuitry comprising an output device configured to indicate the temperature of the transmitter assembly.

10. The surgical navigation system of claim 1, wherein the transmitter coil and the receiver coil are both operable to generate and sense an electromagnetic field.

11. The surgical navigation system of claim 1, wherein the transmitter assembly is coupled to a surgical table.

12. The surgical navigation system of claim 11, wherein the transmitter assembly is secured within the surgical table beneath a patient support.

13. The surgical navigation system of claim 11, wherein heat generated by the transmitter assembly is dissipated away from the transmitter assembly to outer edges of the surgical table.

14. The surgical navigation system of claim 1, wherein the transmitter assembly comprises a first layer that includes the at least one coil and a second layer that includes the cooling unit.

15. The surgical navigation system of claim 1, wherein the transmitter assembly comprises an electromagnetic shielding layer.

16. A surgical navigation system comprising:

an imaging system operable to acquire image data;

a display configured to display an image acquired via the imaging system;

an electromagnetic tracking system comprising;

at least one transmitter assembly located beneath an imaged subject and configured to generate an electromagnetic field;

at least one receiver assembly configured to generate signals induced by the electromagnetic field; and

electronics coupled to and communicating with the transmitter assembly and the receiver assembly for calculating at least a position of the receiver assembly; and

a cooling system thermally coupled to the transmitter assembly to dissipate heat generated by the transmitter assembly.

17. The surgical navigation system of claim 16, comprising a controller coupled to the cooling system and configured to regulate operation of the cooling system.

18. The surgical navigation system of claim 17, wherein the cooling system comprises a temperature sensor, and wherein the controller is coupled to the temperature sensor and controls operation of the cooling system in a closed-loop manner.

19. The surgical navigation system of claim 16, wherein the cooling system comprises a plurality of semiconductor thermocouples and a controller coupled to the plurality of semiconductor thermocouples to drive each of the semiconductor thermocouples to extract heat from the at least one transmitter assembly.

20. The surgical navigation system of claim 16, wherein the transmitter assembly comprises a temperature sensor electronically coupled to and communicating with the controller, and wherein the controller is configured for regulating the temperature of the transmitter assembly.

21. The surgical navigation system of claim 20, wherein the controller is coupled to a temperature indicator, and wherein the display is configured to indicate a status of the transmitter assembly temperature.

22. The surgical navigation system of claim 16, wherein the controller is configured to reduce the temperature of the transmitter assembly independent of user input.

23. A method of cooling a transmitter assembly of a surgical navigation system, the method comprising:

measuring a temperature of a transmitter assembly;

communicating the temperature of the transmitter assembly to a controller; and

activating a cooling system to dissipate heat generated by the transmitter assembly and to reduce the temperature of the transmitter assembly.

24. The method of claim 23, wherein the cooling system is activated by the controller and/or a user.

25. The method of claim 23, wherein the cooling system comprises a plurality of semiconductor thermocouples and a controller coupled to the plurality of semiconductor thermocouples, and wherein activating the cooling system comprises operating the controller to drive the semiconductor thermocouples to extract heat from the transmitter assembly.