GAS TURBINE START ARCHITECTURE

• US 20130031912A1
• Filed: 08/01/2011
• Published: 02/07/2013
• Est. Priority Date: 08/01/2011
• Status: Abandoned Application

• 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: Finney, Adam M., Krenz, Michael
• Application Number:
  US13/195,223
• Publication Number:
  US 20130031912A1
• Time in Patent Office: Days
• US Class Current: 60/778
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F01D 19/00 Starting of machines or engines; Regulating, controlling, or safety means in connection therewith warming-up before starting F01D25/10; turning or inching gear F01D25/34
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A gas turbine starting architecture is used to start a gas turbine engine having at least a first spool. The architecture includes an electric power distribution bus, a motor, a compressor, a pneumatic distribution circuit, an air turbine starter, and a first tower shaft. The motor converts electric power provided by the electric power distribution bus to mechanical power. In turn, the mechanical power provided by the motor is converted to pneumatic power by the compressor for provision to a pneumatic distribution circuit. The air turbine starter converts pneumatic power from the pneumatic distribution circuit to mechanical power is provided via the first tower shaft to the at least one spool on the gas turbine engine.

Claims

1. A gas turbine start architecture for starting a gas turbine engine having at least a first spool, the gas turbine start architecture comprising:

an electric power distribution bus that distributes electric power provided by an electrical power source;

a motor that converts electric power provided by the electric power distribution bus to mechanical power;

a compressor that converts mechanical energy provided by the motor to pneumatic power;

a pneumatic distribution circuit that distributes pneumatic power provided by the compressor;

an air turbine starter that converts pneumatic power provided by the pneumatic distribution circuit to mechanical power; and

a first tower shaft that communicates mechanical energy developed by the air turbine starter to the first spool to start the gas turbine engine.

2. The gas turbine start architecture of claim 1, wherein the first tower shaft is a high-pressure (HP) tower shaft and the first spool is a high-pressure (HP) spool, wherein the HP tower shaft communicates mechanical energy to the HP spool in a gas turbine engine that includes the HP spool and a low-pressure (LP) spool.

3. The gas turbine start architecture of claim 2, further including:

a low-pressure (LP) tower shaft connected to the LP spool of the gas turbine engine, wherein the motor and the compressor are located on the LP tower shaft, wherein mechanical power developed by the motor is communicated via the LP tower shaft to the compressor and to the LP spool.

4. The gas turbine start architecture of claim 3, wherein the motor is a starter/generator that converts electric power to mechanical power during a start mode and converts mechanical energy to electrical energy during a generate mode.

5. The gas turbine start architecture of claim 4, further including:

a clutch connected on the LP tower shaft that selectively decouples the compressor and the starter/generator from the LP spool.

6. The gas turbine start architecture of claim 5, wherein the clutch decouples the LP tower shaft from the LP spool during start operations and couples the LP tower shaft to the LP spool during normal operation to extract energy from the LP spool via the starter/generator.

7. The gas turbine start architecture of claim 1, wherein the electric power distribution bus receives electric power from an auxiliary power unit (APU) and/or an external electric power source.

8. The gas turbine start architecture of claim 1, further including:

a reservoir connected to store pneumatic power provided by the compressor and to supply stored pneumatic power to the air turbine starter.

9. The gas turbine start architecture of claim 1, wherein the pneumatic distribution circuit receives pneumatic power from an external pneumatic source.

10. A gas turbine start architecture for starting a gas turbine engine that includes a low-pressure (LP) spool and a high-pressure (HP) spool, the gas turbine start architecture comprising:

an electric power distribution bus for distributing electrical power generated by an electric power source;

a pneumatic power distribution circuit for distributing pneumatic power;

a low-pressure (LP) tower shaft connected to the LP spool;

a high-pressure (HP) tower shaft connected to the HP spool;

a starter/generator connected to the electric power distribution bus and to the LP tower shaft, wherein the starter/generator converts electric power received from the electric power distribution bus to mechanical power when operating in a starter mode and converts mechanical power provided by the LP tower shaft to electric power when operating in a generator mode;

a compressor connected to the LP tower shaft that converts mechanical power provided by the starter/generator to pneumatic power provided to the pneumatic power distribution circuit; and

an air turbine starter that converts pneumatic power provided via the pneumatic power distribution circuit to mechanical power provided to the HP spool via the HP tower shaft to start the gas turbine engine.

11. The gas turbine starting architecture of claim 10, wherein mechanical energy provided by the starter/generator during start operations is communicated to the LP spool via the LP tower shaft to rotate the LP spool during start operations.

12. The gas turbine starting architecture of claim 10, further including:

a clutch connected to the LP tower shaft to selectively couple and decouple the LP tower shaft from the LP spool, wherein the LP tower shaft is selectively decoupled from the LP spool during starting operations and selectively coupled to the LP spool during normal operations, such that the starter/generator extracts power from the LP spool.

13. The gas turbine starting architecture of claim 10, wherein the electric power distribution circuit is supplied with power from an auxiliary power unit (APU) and/or an external electric power source.

14. The gas turbine starting architecture of claim 10, wherein the pneumatic power distribution circuit receives pneumatic power from an external pneumatic power source.

15. The gas turbine starting architecture of claim 10, further including:

a reservoir connected to store pneumatic power provided by the compressor and to supply stored pneumatic power to the pneumatic power distribution circuit.

16. A method of starting a gas turbine engine, the method comprising:

receiving electric power from an electric power source for distribution via an electric power distribution bus;

providing electric power from the electric power distribution bus to a motor that converts the electric power to mechanical power;

providing mechanical power provided by the motor to a compressor that converts the mechanical power to pneumatic power for distribution via a pneumatic power distribution circuit;

providing pneumatic power from the pneumatic power distribution circuit to an air turbine starter that converts pneumatic power to mechanical power;

communicating mechanical power provided by the air turbine starter to the gas turbine engine for starting the gas turbine engine.

17. The method of claim 16, wherein the motor and the compressor are connected to a low-pressure (LP) tower shaft that is coupled to a LP spool of the gas turbine engine, and the air turbine starter is connected to a high-pressure (HP) tower shaft that is coupled to an HP spool of the gas turbine engine.

18. The method of claim 17, wherein motor is a starter/generator that converts electric power to mechanical power when operating in the starter mode and converts mechanical power to electric power when operating in the generator mode.

19. The method of claim 18, further including:

decoupling the starter/generator and the compressor from the LP spool during start operations to prevent mechanical power provided by the starter/generator from being communicated to the LP spool; and

coupling the starter/generator to the LP spool during normal operations to convert mechanical power provided by the LP spool to electric power for distribution via the electric power distribution bus.