Hybrid turbogenerator and associated method

• US 8,957,539 B1
• Filed: 10/16/2012
• Issued: 02/17/2015
• Est. Priority Date: 10/16/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ralston, Mark Dixon
• Primary Examiner(s): ZARROLI, MICHAEL C
• Application Number:
  US13/652,980
• Time in Patent Office: 854 Days
• Field of Search: 290/52, 607/72
• US Class Current: 290/52
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F02C 9/20 by throttling; by adjusting vanes
• CPC Class Codes: F05D 2220/50 for auxiliary power units (APU's)
• CPC Class Codes: F05D 2220/76 an electrical generator

Abstract

A hybrid turbogenerator and a method of operation are provided to configure a gas turbine engine. In the context of a method, a hybrid turbogenerator including a gas turbine engine coupled to an electric motor-generator alternates between a standby mode and a charging mode. In the standby mode, the method at least partially closes one or more inlet guide vane(s) to limit air flow through a compressor and into a turbine. In the standby mode, the method provides power to both a power bus and the electric motor-generator from an energy storage device. In the charging mode, the method at least partially opens the inlet guide vane(s) to increase air flow through the compressor and into the turbine relative to the standby mode. In the charging mode, the method provides electric power from the electric motor-generator to both the power bus and the energy storage device.

Claims

1. A method of operating a hybrid turbogenerator including a gas turbine engine coupled to an electric motor-generator, the method comprising:

alternating between a standby mode and a charging mode,

wherein during operation in the standby mode, the method further comprises;

at least partially closing one or more inlet guide vanes to limit air flow through a compressor and to a turbine of the gas turbine engine; and

providing electric power to both a power bus and the electric motor-generator from an energy storage device; and

wherein during operation in the charging mode, the method further comprises;

at least partially opening the one or more inlet guide vanes to increase air flow through the compressor and to the turbine of the gas turbine engine relative to the standby mode; and

providing electric power from the electric motor-generator to both the power bus and the energy storage device.

2. A method according to claim 1 further comprising recovering heat from an exhaust gas flow from the gas turbine engine and transferring the heat to a discharge flow from the compressor.

3. A method according to claim 1 wherein alternating between the standby mode and the charging mode comprises monitoring a charge stored by the energy storage device and controlling operation in the standby mode and the charging mode based upon the charge stored by the energy storage device.

4. A method according to claim 1 wherein at least partially closing the one or more inlet guide vanes during the standby mode comprises closing the one or more inlet guide vanes so as to limit air flow therethrough to less than a predefined percentage of the air flow through the one or more inlet guide vanes during the charging mode.

5. A method according to claim 1 further comprising providing an intermittent supply of bleed air from the compressor with more bleed air supplied during the charging mode than during the standby mode.

6. A hybrid turbogenerator comprising:

a gas turbine engine comprising a compressor, a combustor and a turbine;

an electric motor-generator rotationally coupled to the gas turbine engine;

an energy storage device;

one or more inlet guide vanes positioned to at least partially control air flow through the compressor and to the turbine of the gas turbine engine; and

a controller configured to cause operation of the hybrid turbogenerator to alternate between a standby mode and a charging mode,

wherein, during operation in the standby mode, the controller is configured to;

at least partially close one or more inlet guide vanes to limit air flow through the compressor and to the turbine of the gas turbine engine; and

provide electric power to both a power bus and the electric motor-generator from the energy storage device; and

wherein, during operation in the charging mode, the controller is configured to;

at least partially open the one or more inlet guide vanes to increase air flow through the compressor and to the turbine of the gas turbine engine relative to the standby mode; and

provide electric power from the electric motor-generator to both the power bus and the energy storage device.

7. A hybrid turbogenerator according to claim 6 further comprising a recuperator configured to recover heat from an exhaust gas flow from the gas turbine engine and to transfer the heat to a discharge flow from the compressor.

8. A hybrid turbogenerator according to claim 6 wherein the controller is further configured to monitor a charge stored by the energy storage device and to control operation in the standby mode and the charging mode based upon the charge stored by the energy storage device.

9. A hybrid turbogenerator according to claim 6 wherein the energy storage device comprises a capacitor bank.

10. A hybrid turbogenerator according to claim 6 wherein the controller is configured to at least partially close the one or more inlet guide vanes during the standby mode so as to limit air flow therethrough to less than a predefined percentage of the air flow through the one or more inlet guide vanes during the charging mode.

11. A method of operating a hybrid turbogenerator including a gas turbine engine coupled to an electric motor-generator, the method comprising:

alternating between a standby mode and a charging mode,

wherein during operation in the standby mode, the method further comprises;

controllably positioning a plurality of valves so as to direct air flow through a turbine and then to a compressor of the gas turbine engine; and

providing electric power to a power bus from an energy storage device; and

wherein during operation in the charging mode, the method further comprises;

controllably positioning the plurality of valves so as to redirect air flow to the compressor and then to the turbine of the gas turbine engine; and

providing electric power from the electric motor-generator to both the power bus and the energy storage device.

12. A method according to claim 11 wherein during operation in the standby mode the method further comprises intercooling gas flowing between the turbine and the compressor.

13. A method according to claim 11 wherein during operation in the charging mode the method further comprises recovering heat from an exhaust gas flow from the gas turbine engine and transferring the heat to a discharge flow from the compressor.

14. A method according to claim 11 wherein controllably positioning the plurality of valves during operation in the standby mode comprises controllably positioning the plurality of valves so as to direct air flow through a recuperator for preheating to a burner for combustion to the turbine for expansion and then to the compressor for compression prior to being exhausted.

15. A method according to claim 11 wherein alternating between the standby mode and the charging mode comprises monitoring a charge stored by the energy storage device and controlling operation in the standby mode and the charging mode based upon the charge stored by the energy storage device.

16. A hybrid turbogenerator comprising:

a gas turbine engine comprising a compressor and a turbine;

an electric motor-generator rotationally coupled to the gas turbine engine;

an energy storage device;

a plurality of valves configured to direct air flow through the gas turbine engine; and

a controller configured to cause operation of the hybrid turbogenerator to alternate between a standby mode and a charging mode,

wherein, during operation in the standby mode, the controller is configured to;

controllably position the plurality of valves so as to direct air flow through the turbine and then to the compressor of the gas turbine engine; and

provide electric power to a power bus from the energy storage device; and

wherein, during operation in the charging mode, the controller is configured to;

controllably position the plurality of valves so as to redirect air flow to the compressor and then to the turbine of the gas turbine engine; and

provide electric power from the electric motor-generator to both the power bus and the energy storage device.

17. A hybrid turbogenerator according to claim 16 further comprising an intercooler configured, during operation in the standby mode, to cool gas flowing between the turbine and the compressor.

18. A hybrid turbogenerator according to claim 16 further comprising a recuperator configured, during operation in the charging mode, to recover heat from an exhaust gas flow from the gas turbine engine and to transfer the heat to a discharge flow from the compressor.

19. A hybrid turbogenerator according to claim 16 wherein the controller, during operation in the standby mode, is further configured to controllably position the plurality of valves so as to direct air flow through a recuperator for preheating to a burner for combustion to the turbine for expansion and then to the compressor for compression prior to being exhausted.

20. A hybrid turbogenerator according to claim 16 wherein the controller is further configured to monitor a charge stored by the energy storage device and to control operation in the standby mode and the charging mode based upon the charge stored by the energy storage device.