Architectures for hybrid-electric propulsion

Patent metadata

Field	Value
Publication number	US-12071256-B2
Application number	US-202218086376-A
Country	US
Kind code	B2
Filing date	Dec 21, 2022
Priority date	Mar 18, 2019
Publication date	Aug 27, 2024
Grant date	Aug 27, 2024

Abstract

A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is configured to receive rotational input power from each of the heat engine shaft and the electric motor shaft and to convert the rotation input power to output power.

First claim

What is claimed is:

1. A hybrid propulsion system comprising:
a heat engine configured to drive a heat engine shaft;
an electric motor configured to drive an electric motor shaft; and
a transmission system connected to receive rotational input power from each of the heat engine shaft and the electric motor shaft, wherein the transmission system is configured to convert the rotational input power to output power;
wherein the heat engine shaft and the electric motor shaft are concentric with a shaft for rotation of a turbocharger component of the heat engine.

2. The system as recited in claim 1 , wherein the transmission system includes:
a turbine gearbox connected between the heat engine shaft and the shaft for driving the turbocharger component of the heat engine at a different rotational speed from the heat engine.

3. The system as recited in claim 1 , wherein the transmission system includes:
a combining gearbox connecting to:
the heat engine shaft;
the electric motor shaft; and
the shaft for driving the turbocharger component of the heat engine, wherein the transmission system is configured to combine the rotational input power from the heat engine and the electric motor for providing rotational output power to an output shaft and to drive the turbocharger component.

4. The system as recited in claim 3 , wherein one and only one of:
the turbocharger component includes a turbine and a compressor that are both on one side of the combining gearbox; or
the turbine and compressor are connected on opposite sides of the combining gearbox.

5. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation and wherein the transmission system includes:
a turbine gearbox connected between the heat engine shaft and the shaft for driving a turbocharger component of the heat engine to drive the turbocharger component at a different rotational speed from the heat engine and the electric motor.

6. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation, and wherein the transmission system includes:
a combining gearbox connecting to:
a common output shaft of the electric motor and the heat engine; and
the shaft for driving the turbocharger component of the heat engine,

wherein the transmission system is configured to combine the rotational input power from the heat engine and electric motor for providing rotational output power to an output shaft and to drive the turbocharger component.

7. The system as recited in claim 6 , wherein one and only one of:
the turbocharger component includes a turbine and a compressor are both on one side of the combining gearbox; or
the turbine and compressor are connected on opposite sides of the combining gearbox.

8. The system as recited in claim 1 , further comprising a turbocharger component driver motor connected to the shaft for driving the turbocharger component of the heat engine to drive the turbocharger component at a different rotational speed ratio from the heat engine and the electric motor.

9. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation and further comprising a turbocharger component driver motor connected to the shaft for driving the turbocharger component of the heat engine to drive the turbocharger component at a different rotational speed ratio from the heat engine and the electric motor.

10. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation and wherein the transmission system includes:
a turbine gearbox connected through a clutch between the heat engine shaft and the shaft for driving the turbocharger component of the heat engine to drive the turbocharger component at a different rotational speed from the heat engine and electric motor when the clutch is engaged, wherein the shaft for driving the turbocharger component is connected to a turbocharger component driver motor to drive the turbocharger independently from the heat engine and the electric motor when the clutch is disengaged.

11. The system as recited in claim 1 , further comprising:
a clutch in the shaft for rotation of the turbocharger component to drive the turbocharger component independently from the heat engine and the electric motor when the clutch is disengaged.

12. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation and further comprising a clutch connected a turbocharger component driver motor connected to the shaft for driving the turbocharger component of the heat engine to drive the turbocharger component with rotational power from the heat engine and electric motor when the clutch is engaged, and to drive the turbocharger component independently from the heat engine and electric motor when the clutch is disengaged.

13. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation, and wherein the transmission system includes:
a combining gearbox connecting to:
a common output shaft of the electric motor and the heat engine; and
the shaft of the turbocharger component of the heat engine,

wherein the transmission system is configured to combine the rotational input power from the heat engine, electric motor, and turbine for providing rotational output power to an output shaft; and
wherein a compressor of the turbocharger component is connected to be driven on the output shaft.

14. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation and wherein the transmission system includes:
a turbine gearbox connected between the heat engine shaft and the shaft of the turbocharger component of the heat engine so a turbine of the turbocharger component can rotate at a different rotational speed from the heat engine and electric motor, wherein a compressor of the turbocharger is connected to a compressor shaft concentric with the common output shaft.

15. The system as recited in claim 1 , wherein the heat engine shaft and the electric motor shaft are connected for common rotation, and wherein the transmission system includes:
a gearbox connecting to:
a common output shaft of the electric motor and the heat engine; and
the shaft of the turbocharger component of the heat engine,

wherein the transmission system is configured to combine the rotational input power from the heat engine and electric motor for providing rotational output power to an output shaft and to drive a turbine and a compressor of the turbocharger component, wherein the gearbox is configured so speed ratio between the common output shaft and the shaft for driving the turbine and the compressor can vary.

16. The system as recited in claim 1 , wherein the turbocharger component comprises a turbine fluidly connected to the heat engine to be driven by exhaust form the heat engine, and a generator connected to be driven by the turbine.

Assignees

• Pratt & Whitney Canada

Inventors

• Latulipe Eric
• Thomassin Jean
• Wang Xiaoqin
• Dubreuil Jean
• Dionne Luc
• Julien Andre

Classifications

• B64D35/024

  of series type · CPC title

• B64D35/025

  of parallel type · CPC title

• B64D35/023

  of series-parallel type · CPC title

• B64D27/357

  using batteries · CPC title

• B64D27/33

  Hybrid electric aircraft · CPC title