ELECTRICALLY COUPLED COUNTER-ROTATION FOR GAS TURBINE COMPRESSORS

• US 20160160867A1
• Filed: 09/10/2015
• Published: 06/09/2016
• Est. Priority Date: 03/15/2013
• Status: Abandoned Application

• Current Assignee: Embry-Riddle Aeronautical University Incorporated
• Original Assignee: Embry-Riddle Aeronautical University Incorporated
• Inventors: Gehlot, Vinod
• Application Number:
  US14/849,941
• Publication Number:
  US 20160160867A1
• Time in Patent Office: Days
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F02C 3/067 having counter-rotating rotors F02C3/073 takes precedence
• CPC Class Codes: F02C 7/36 Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user F02C3/107 - F02C3/13 and F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H
• CPC Class Codes: F04D 25/06 the pump being electrically driven F04D25/08 takes precedence
• CPC Class Codes: F04D 27/004 by varying driving speed
• CPC Class Codes: F04D 27/02 Surge control surge detection F04D27/001
• CPC Class Codes: F04D 29/325 for axial flow fans blade mountings F04D29/34, blades F04D29/38
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2220/76 an electrical generator
• CPC Class Codes: F05D 2240/24 for turbines
• CPC Class Codes: F05D 2240/35 Combustors or associated equipment
• CPC Class Codes: F05D 2240/60 Shafts
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A system and method for implementing stage-by-stage counter rotation in a multi-stage axial compressor of a gas turbine engine. The system includes an electrical power generator and an electric motor. A turbine-driven shaft connected to an armature of the electrical generator drives a first plurality of compressor blades. The electrical generator armature induces changing magnetic flux in the stator coils of the electrical generator which generates electrical power that is sent to a power control module. The power control module controls the electrical motor and excites the coils in the electric motor stator which drives the electric motor armature. The electric motor armature drives a second shaft which drives a second plurality of compressor blades in an opposite direction to the first plurality of compressor blades.

Claims

1. A system for providing stage-by-stage counter rotation in a multi-stage axial compressor of a gas turbine engine using electrical coupling comprising:

an electric power generator mounted in an engine core on a gas turbine engine shaft for driving a first plurality of compressor blades;

an electric motor mounted in the engine core on a second shaft for driving a second plurality of compressor blades in an opposite direction from a direction of the first plurality of compressor blades, wherein the first plurality of compressor blades and the second plurality of compressor blades alternate in the compressor on a stage-by-stage basis; and

a power control module for receiving electrical power from the electrical

generator and controlling operation of the electric motor.

2. The system for providing stage-by-stage counter rotation of claim 1 wherein the electric power generator comprises a generator armature coupled to the turbine shaft and a generator stator coupled to the second shaft, the second shaft rotating in an opposite direction from the rotation of the turbine shaft.

3. The system for providing stage-by-stage counter rotation of claim 1 wherein the electric motor comprises a motor stator and a motor armature, the motor armature coupled to the second shaft which drives the second plurality of compressor blades in an opposite direction from the first plurality of compressor blades.

4. The system for providing stage-by-stage counter rotation of claim 1 wherein the rotating armature of the electrical power generator induces a changing magnetic flux in a plurality of stator coils of the generator to generate electrical power.

5. The system for providing stage-by-stage counter rotation of claim 1 wherein the power control module receives electrical power generated by the electrical generator.

6. The system for providing stage-by-stage counter rotation of claim 1 wherein the power control module includes a plurality of power electronics which controls the electric motor and enables electrical power offtake.

7. The system for providing stage-by-stage counter rotation of claim 1 further comprising a full-authority digital engine control which controls operation of the power control module.

8. The system for providing stage-by-stage counter rotation of claim 1 wherein the power control module excites a plurality of coils in the motor stator which drives the motor armature.

9. A system for providing stage-by-stage counter rotation in a multi-stage axial compressor of gas turbine engine comprising:

an electrical power generator mounted in an engine core and including a stator and an armature;

an electric motor mounted in the engine core and including a stator and an armature;

a turbine-driven shaft for driving a first plurality of compressor blades and electrically coupled to the electric generator armature, the electric generator armature inducing a changing magnetic flux in a plurality of stator coils of the generator stator;

a power control module for receiving electrical power from the electrical

generator and controlling the electric motor by exciting a plurality of stator coils in the electric motor to drive the electric motor armature; and

a second shaft driven by the electric motor armature, the second shaft

driving a second plurality of compressor blades in an opposite direction from a direction of the first plurality of compressor blades.

10. The system for providing stage-by-stage counter rotation of claim 9 wherein the stator and armature of the electrical generator are coupled to separate counter-rotating shafts.

11. The system for providing stage-by-stage counter rotation of claim 9 wherein the electric generator stator is coupled to the turbine shaft and the electric generator armature is coupled to the second shaft, the second shaft rotating in an opposite direction from the turbine shaft.

12. The system for providing stage-by-stage counter rotation of claim 9 wherein the changing magnetic flux in the plurality of generator stator coils generates electrical power that is provided to the power control module to control the electric motor and enable aircraft takeoff under electrical power.

13. The system for providing stage-by-stage counter rotation of claim 9 wherein the first plurality of compressor blades and the second plurality of compressor blades alternate in the compressor on a stage-by-stage basis.

14. The system for providing stage-by-stage counter rotation of claim 9 wherein the first plurality of compressor blades are connected to a counter-rotating module casing which is connected to a plurality of engine struts, the casing providing electrical connections to the power control module.

15. The system for providing stage-by-stage counter rotation of claim 9 wherein the second plurality of compressor blades are connected to a counter-rotating compressor drum.

16. The system for providing stage-by-stage counter rotation of claim 9 wherein the electrically coupled counter-rotating shaft system drives onboard avionics and electrically-operated equipment.

17. The system for providing stage-by-stage counter rotation of claim 13 wherein there is no mechanical contact between the turbine shaft and second shaft, the separate shafts providing contra-rotation of the alternating first plurality of compressor blades and the second plurality of compressor blades.

18. The system for providing stage-by-stage counter rotation of claim 13 wherein electrical coupling enables the power control module to provide an adaptable and precise control of revolutions per minute (rpm) of the contra-rotating shafts.

19. A system for providing stage-by-stage counter rotation of compressor blades mounted on separate shafts in a multi-stage axial compressor of a gas turbine engine comprising:

a first plurality of compressor blades driven by a turbine shaft;

a second plurality of compressor blades driven by a second shaft in a direction opposite to the direction of the turbine shaft;

an electrical generator mounted in an engine core for driving the first plurality of compressor blades and providing electrical power to a power control module; and

an electric motor mounted in an engine core for receiving electrical power from the power control module and driving the second plurality of compressor blades in a direction opposite from a direction of the first plurality of compressor blades.

20. The system for providing stage-by-stage counter rotation of claim 19 wherein the electrical generator includes a rotating armature that induces a changing magnetic flux in a plurality of stator coils of the generator to generate electrical power that is provided to the power control module.

21. The system for providing stage-by-stage counter rotation of claim 19 wherein the power control module excites a plurality of coils in a motor stator which drives a motor armature coupled to the second shaft to rotate the second plurality of compressor blades in an opposite direction from the first plurality of compressor blades.

22. The system for providing stage-by-stage counter rotation of claim 19 wherein the first plurality of compressor blades and the second plurality of compressor blades alternate in the compressor on a stage-by-stage basis.