Secondary protection approach for power switching applications

• US 8,390,972 B2
• Filed: 04/17/2007
• Issued: 03/05/2013
• Est. Priority Date: 04/17/2007
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Simper, Norbert J., Bach, Martin
• Primary Examiner(s): Barnie, Rexford
• Assistant Examiner(s): HOANG, ANN THI
• Application Number:
  US11/736,096
• Publication Number:
  US 20080259914A1
• Time in Patent Office: 2,149 Days
• Field of Search: 361/93.1
• US Class Current: 361/93.1
• CPC Class Codes: H02H 3/05 with means for increasing reliability, e.g. redundancy arrangements for logic circuits H03K19/003
• CPC Class Codes: H02H 3/087 for dc applications

Abstract

An apparatus and method for providing a primary and a secondary protection to a load in a power switching application uses an electronic circuit breaker to selectively permit a flow of current from an input to a load. The circuit breaker comprises a plurality of first switches coupled in parallel, and a plurality of fuses coupled to the plurality of first switches. In a disclosed embodiment, each first switch is coupled to a first fuse and to a second fuse. A controller opens and closes the plurality of first switches by commanding a driver current ON and OFF. The controller is operable to detect a fault condition and to open the plurality of first switches in response to the fault condition by commanding the driver current OFF. If the controller fails to open one of the first switches, one of the fuses coupled to the switch is operable to blow. In addition, the circuit breaker also comprises a charge pump that provides an electric current to a second plurality of switches to prevent the second plurality of switches form shorting the driver current.

Claims

1. An electronic system for providing power to a load, comprising:

a plurality of first switches providing parallel paths from a power source to the load and being operable to control a flow of current from the power source to the load, each of the first switches having an input, an output, and a gate;

a controller, wherein the controller is operable to detect a fault condition and to turn OFF the plurality of first switches to prevent the flow of current from the power source to the load in response to the detected fault condition;

a plurality of first fuses, each first fuse being coupled to an input of an associated one of the plurality of first switches, each of the plurality of first fuses being operable to prevent a flow of current from the power source to the input of its associated switch if a current flowing to the input of its associated switch exceeds a first fuse current threshold; and

a plurality of second fuses, each second fuse being coupled to a gate of an associated one of the plurality of first switches, each of the second plurality of fuses being operable to prevent a flow of current to the gate of its associated switch if the current flowing to the gate of its associated switch exceeds a second fuse current threshold.

2. The system of claim 1, wherein the current flowing to the input of the associated switch exceeds the first fuse current threshold in response to the input of the switch being shorted to the output of the switch.

3. The system of claim 1, wherein the current flowing to the gate of one of the plurality of first switches exceeds a second fuse current threshold in response to the gate of the switch being shorted to the input of the switch.

4. The system of claim 1, wherein each of the plurality of first switches is a MOSFET.

5. The system of claim 1, further comprising:

a driver that provides a driver current to selectively turn the plurality of first switches ON and OFF; and

a charge pump that provides a charge pump current to a second plurality of switches to prevent the second plurality of switches from shorting the driver current, wherein the driver and the charge pump are operated by the controller.

6. The system of claim 5, wherein the second plurality of switches comprises a first switch and a second switch, and an output of the first switch is coupled to a control input of the second switch.

7. The system of claim 6, wherein each of the plurality of first switches are JFETs and the second plurality of switches are transistors.

8. The system of claim 6, wherein the driver amplifies a driver input voltage to provide a driver output voltage that is greater than the driver input voltage, and wherein the driver output voltage is coupled to the control input of each of the plurality of first switches to provide the driver current.

9. The system of claim 1, wherein the load is a component on an aircraft.

10. The system of claim 1, wherein each of the plurality of fuses comprises a bond wire specifically sized and constructed to provide a required fusing characteristic.

11. The system of claim 1, including at least one zener diode oriented to block a flow of current from the power source to the gates of each of the plurality of first switches in a non-fault condition, the at least one zener diode being operable to permit a flow of current from the power source to the gates of each of the plurality of switches in response to a voltage of the power source exceeding a zener diode voltage threshold.

12. The system of claim 11, wherein each of the plurality of second fuses is coupled to a resistor operable to provide a decoupling function to prevent each of the plurality of first switches from oscillating due to an input capacitance of the at least one zener diode.

13. A method of providing fault protection, comprising the steps of:

detecting a fault condition;

opening a plurality of first switches in response to the fault condition;

blowing a first fuse coupled to an input of a one of the plurality of switches in response to said one of the plurality of switches not turning OFF;

blowing a second fuse coupled to a gate of one of the plurality of switches in response to a gate of said one of the plurality of switches being shorted to an input of said one of the plurality of switches;

orienting at least one zener diode to block a flow of current from the power source from flowing to the gates of each of the plurality of first switches in a non-fault condition; and

permitting a flow of current from the power source to the gates of each of the plurality of switches to turn on the plurality of switches in response to a voltage of the power source exceeding a zener diode voltage threshold.

14. The method of claim 13, wherein the step of detecting a fault condition comprises:

measuring a current;

determining if the current exceeds a current threshold.

15. The method of claim 13, wherein the step of opening a plurality of first switches in response to the fault condition further comprises commanding a driver current OFF, wherein the driver current is coupled to a control input of each of the plurality of first switches.

16. The method of claim 15, wherein the step of opening a plurality of first switches in response to the fault condition further comprises the step of commanding a charge pump OFF, wherein turning the charge pump OFF couples the driver current to a ground connection.

17. An electric system for use on a vehicle comprising:

a load;

a first input voltage; and

at least one circuit breaker, wherein the circuit breaker includes;

a plurality of first switches providing parallel paths from a power source to the load and being operable to control a flow of current from the power source to the load, each of the first switches having an input, an output, and a gate;

a controller that is operable to detect a fault condition and to turn OFF the plurality of first switches to prevent the flow of current from the power source to the load in response to the detected fault condition;

a plurality of first fuses, each first fuse being coupled to an input of an associated one of the plurality of first switches, each of the plurality of first fuses being operable to prevent a flow of current from the power source to the input of its associated switch if a current flowing to the input of its associated switch exceeds a first fuse current threshold; and

a plurality of second fuses, each second fuse being coupled to a gate of an associated of the plurality of first switches, each of the second plurality of fuses being operable to prevent a flow of current to the gate of its associated switch if the current flowing to the gate of its associated switch exceeds a second fuse current threshold.

18. The system of claim 17, wherein the vehicle is an aircraft.

19. The system of claim 17, further comprising:

a second input voltage, wherein the circuit breaker further includes;

a driver that provides a driver current to the plurality of first switches to selectively open and close the plurality of first switches, wherein the second input voltage is coupled to the driver; and

charge pump that provides a charge pump current to a second plurality of switches to prevent the second plurality of switches from shorting the driver current, wherein the driver and the charge pump are operated by the controller.

20. The system of claim 17, including at least one zener diode oriented to block a flow of current from the power source to the gates of each of the plurality of first switches in a non-fault condition, the at least one zener diode being operable to permit a flow of current from the power source to the gates of each of the plurality of switches in response to a voltage of the power source exceeding a zener diode voltage threshold.

21. The system of claim 20, wherein each of the plurality of second fuses is coupled to a resistor operable to provide a decoupling function to prevent each of the plurality of first switches from oscillating due to an input capacitance of the at least one zener diode.