Propulsion system for an aircraft

Patent metadata

Field	Value
Publication number	US-10569759-B2
Application number	US-201715639134-A
Country	US
Kind code	B2
Filing date	Jun 30, 2017
Priority date	Jun 30, 2017
Publication date	Feb 25, 2020
Grant date	Feb 25, 2020

Abstract

A hybrid-electric propulsion system includes a turbomachine, a propulsor coupled to the turbomachine, and an electrical system, the electrical system including an electric machine coupled to the turbomachine. A method for operating a hybrid-electric propulsion system includes operating, by one or more computing devices, the turbomachine in an idle operating condition; receiving, by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine in the idle operating condition; and providing, by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine and increase an acceleration of the turbomachine in response to the received command to accelerate the turbomachine.

First claim

What is claimed is:

1. A method for operating a hybrid-electric propulsion system of an aircraft, the hybrid-electric propulsion system comprising a turbomachine, a propulsor coupled to the turbomachine, and an electrical system, the electrical system comprising an electric machine coupled to the turbomachine, the method comprising:
operating, by one or more computing devices, the turbomachine in an idle operating condition;
receiving, by the one or more computing devices, a command to accelerate the turbomachine while operating the turbomachine in the idle operating condition; and
providing, by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine and increase an acceleration of the turbomachine in response to the received command to accelerate the turbomachine.

2. The method of claim 1 , wherein the hybrid electric propulsion system further comprises an electric energy storage unit, and wherein providing, by the one or more computing devices, electrical power to the electric machine comprises providing, by the one or more computing devices, electrical power to the electric machine from the electric energy storage unit.

3. The method of claim 1 , wherein providing, by the one or more computing devices, electrical power to the electric machine comprises modulating, by the one or more computing devices, an amount of electrical power provided to the electric machine.

4. The method of claim 3 , further comprising:
receiving, by the one or more computing devices, data indicative of a rotational speed parameter of the turbomachine, and wherein modulating, by the one or more computing devices, the amount of electrical power provided to the electric machine comprises modulating, by the one or more computing devices, the amount of electrical power provided to the electric machine based at least in part on the received data indicative of the rotational speed parameter of the turbomachine.

5. The method of claim 4 , wherein the rotational speed parameter of the turbomachine is a rotational speed of one or more components of the turbomachine, or an acceleration of one or more components of the turbomachine.

6. The method of claim 1 , wherein receiving, by the one or more computing devices, the command to accelerate the turbomachine while operating the turbomachine in the idle operating condition comprises receiving, by the one or more computing devices, a command to accelerate the turbomachine to a takeoff power level while operating the turbomachine in the idle operating condition.

7. The method of claim 1 , receiving, by the one or more computing devices, the command to accelerate the turbomachine while operating the turbomachine in the idle operating condition comprises receiving, by the one or more computing devices, a thrust increase command.

8. The method of claim 7 , wherein receiving, by the one or more computing devices, the command to accelerate the turbomachine further comprises determining, by the one or more computing devices, a rate of change of commanded thrust increase, and wherein providing, by the one or more computing devices, electrical power to the electric machine comprises modulating, by the one or more computing devices, an amount of electrical power provided to the electric machine based at least in part on the determined rate of change of commanded thrust increase.

9. The method of claim 1 , further comprising:
terminating, by the one or more computing devices, the provision of electrical power to the electric machine to add power to the turbomachine and increase the acceleration of the turbomachine; and
extracting, by the one or more computing devices, electrical power from the electric machine.

10. The method of claim 9 , wherein the hybrid electric propulsion system further comprises an electric energy storage unit, and wherein extracting, by the one or more computing devices, electrical power from the electric machine comprises extracting, by the one or more computing devices, electrical power from the electric machine to the electric energy storage unit.

11. The method of claim 9 , wherein the hybrid electric propulsion system further comprises an electric energy storage unit, and wherein the propulsor is a first propulsor, wherein the electric machine is a first electric machine, wherein the hybrid electric propulsion system further comprises a second propulsor, wherein the electrical system further comprises a second electric machine coupled to the second propulsor, and wherein extracting, by the one or more computing devices, electrical power from the electric machine comprises extracting, by the one or more computing devices, electrical power from the first electric machine to the electric energy storage unit, the second electric machine, or both.

12. The method of claim 1 , wherein providing, by the one or more computing devices, electrical power to the electric machine to add power to the turbomachine and increase an acceleration of the turbomachine comprises providing, by the one or more computing devices, at least about fifteen horsepower of mechanical power to the turbomachine with the electric machine.

13. A hybrid-electric propulsion system for an aircraft comprising:
a propulsor;
a turbomachine coupled to the propulsor for driving the propulsor and generating thrust;
an electrical system comprising an electric machine and an electric energy storage unit electrically connectable to the electric machine, the electric machine coupled to the turbomachine; and
a controller configured to receive a command to accelerate the turbomachine while operating the turbomachine in the idle operating condition, and further to provide electrical power to the electric machine to add power to the turbomachine and increase an acceleration of the turbomachine in response to the received command to accelerate the turbomachine.

14. The hybrid-electric propulsion system of claim 13 , wherein the electrical system further comprises an electric energy storage unit, and wherein in providing electrical power to the electric machine, the controller is configured to provide electrical power to the electric machine from the electric energy storage unit.

15. The hybrid-electric propulsion system of claim 13 , wherein in providing electrical power to the electric machine, the controller is configured to modulate an amount of electrical power provided to the electric machine.

16. The hybrid-electric propulsion system of claim 15 , wherein the controller is further configured to receive data indicative of a rotational speed parameter of the turbomachine, and wherein in modulating the amount of electrical power provided to the electric machine, the controller is configured to modulate the amount of electrical power provided to the electric machine based at least in part on the received data indicative of the rotational speed parameter of the turbomachine.

17. The hybrid-electric propulsion system of claim 16 , wherein the rotational speed parameter of the turbomachine is a rotational speed of one or more components of the turbomachine, or an acceleration of one or more components of the turbomachine.

18. The hybrid-electric propulsion system of claim 13 , wherein the electric machine is configured to provide at least about fifteen horsepower of mechanical power to the turbomachine when electrical power is provided thereto.

19. The hybrid-electric propulsion system of claim 13 , wherein in receiving the command to accelerate the turbomachine while operating the turbomachine in the idle operati

Assignees

• Gen Electric

Inventors

• Gansler Michael Thomas
• Hon Robert Charles

Classifications

• F02B37/013

  with exhaust-driven pumps arranged in series · CPC title

• B60L50/16

  with provision for separate direct mechanical propulsion · CPC title

• B60K6/22

  characterised by apparatus, components or means specially adapted for HEVs · CPC title

• F05D2270/071

  in particular at idling speed · CPC title

• F05D2270/303

  Temperature · CPC title