LOAD FAULT HANDLING FOR SWITCHED RELUCTANCE OR INDUCTION TYPE MACHINES

• US 20100321968A1
• Filed: 06/18/2009
• Published: 12/23/2010
• Est. Priority Date: 06/18/2009
• Status: Abandoned Application

• Current Assignee: Hamilton Sundstrand Corporation (Rtx Corporation)
• Original Assignee: Hamilton Sundstrand Corporation (Rtx Corporation)
• Inventors: Jones, Stephen R., Romenesko, Charles
• Application Number:
  US12/487,190
• Publication Number:
  US 20100321968A1
• Time in Patent Office: Days
• US Class Current: 363/127
• CPC Class Codes: H02M 1/14 Arrangements for reducing ripples from dc input or output
• CPC Class Codes: H02M 1/32 Means for protecting converters other than automatic disconnection
• CPC Class Codes: H02M 3/155 using semiconductor devices only
• CPC Class Codes: H02P 2101/30 for aircraft
• CPC Class Codes: H02P 25/08 Reluctance motors
• CPC Class Codes: H02P 9/107 for limiting effects of overloads
• CPC Class Codes: H02P 9/48 Arrangements for obtaining a constant output value at varying speed of the generator, e.g. on vehicle H02P9/04 - H02P9/46 take precedence

Abstract

An electrical power generation system includes a power source (102) and power conversion electronics (104) coupled to the power source to rectify phased currents received from the power source and maintain a power conversion voltage used to provide excitation to the power source. The system also includes a power conditioner (108) coupled between the power conversion electronics and a load (108), the power conditioner operating as a filter in a normal operational mode and as a buck converter in an abnormal operational mode.

Claims

1. An electrical power generation system comprising:

a power source (102);

power conversion electronics (104) coupled to the power source to rectify phased currents received from the power source and maintain a power conversion voltage used to provide excitation to the power source; and

a power conditioner (108) coupled between the power conversion electronics and a load (106), the power conditioner operating as a filter in a normal operational mode and as a buck converter in an abnormal operational mode.

2. The system of claim 1, wherein the power source is an induction machine.

3. The system of claim 2, wherein the power conversion electronics include:

an excitation inverter (202) coupled to the induction machine; and

an output capacitor (C1) coupled to an output of the excitation inverter.

4. The system of claim 1, wherein the power source is switched reluctance machine.

5. The system of claim 4, wherein the power conversion electronics include:

an asymmetric half bridge converter coupled to the switched reluctance machine; and

an output capacitor coupled to an output of the half bridge converter.

6. The system of claim 1, wherein the power conditioner includes:

a first transistor (Q7) including a collector coupled to an output of the power conversion electronics;

an inductor (L1) having a first terminal coupled to an emitter of the first transistor; and

a second capacitor (C2) coupled between a second terminal of the inductor and ground.

7. The system of claim 6, wherein the inductor includes windings on both a positive terminal and a negative terminal.

8. The system of claim 6, wherein in the normal operation mode the first transistor allows current to flow from the output of the power conversion electronics to the inductor and in the abnormal operational mode the first transistor disallows current flow for at least a portion of an operating time of the abnormal operational mode.

9. The system of claim 8, wherein the first transistor is repeatedly switched from an open state to a closed state during the operation time of the abnormal operational mode.

10. The system of claim 1, further comprising:

the load (106).

11. The system of claim 1, further comprising:

a controller (110) coupled to the power conversion electronics and the power conditioner.

12. The system of claim 11, wherein the controller receives inputs containing parameters related to a first capacitor contained in the power conversion electronics, the inductor, and a second capacitor coupled in parallel with the load.

13. The system of claim 1, wherein the system is coupled to a prime mover.

14. The system of claim 1, wherein the system is coupled to an airplane.

15. The system of claim 1, wherein the power conditioner operates in the abnormal operational mode in the event of a short in the load.

16. A method of operating a system including a power source, power conversion electronics (104) coupled to the power source (102), and a power conditioner (108) coupled between the power conversion electronics and a load (106), the method comprising:

operating in a first operating mode with the power conditioner operating as pi filter;

determining that a load fault exist at the load; and

switching to a second operating mode with the power conditioner operating as a buck converter in the event that a load fault exists.

17. The method of claim 16, wherein the second operating mode includes selectively opening and closing a switch (Q7) contained in the power conditioner.

18. The method of claim 17, wherein the switch is opened and closed based on at least a voltage of an output capacitor (C1) contained in the power conversion electronics.

19. The method of claim 18, wherein the switch is a transistor.

20. The method of claim 16, wherein the power source is either an induction machine or a switched reluctance machine.