Electrical power system for a vehicle

Patent metadata

Field	Value
Publication number	US-12577906-B2
Application number	US-202418673545-A
Country	US
Kind code	B2
Filing date	May 24, 2024
Priority date	Apr 27, 2022
Publication date	Mar 17, 2026
Grant date	Mar 17, 2026

Abstract

A vehicle includes a gas turbine engine having at least two spools and an associated power system. The power system includes two independent power subsystems, including a first power subsystem for managing power transfer between spools and a second power subsystem for supplying a base power load to the vehicle. The first power subsystem has a first electric machine mechanically coupled with a first spool of the gas turbine engine and a second electric machine mechanically coupled with a second spool. The second electric machine is electrically coupled with the first electric machine such that electrical power is transmittable therebetween. The second power subsystem has a third electric machine mechanically coupled with one of the spools. The third electric machine is electrically coupled with a load positioned offboard the gas turbine engine. The first power subsystem and the second power subsystem are electrically decoupled from one another.

First claim

We claim:

1 . A power system associated with a gas turbine engine mounted to a vehicle, the power system comprising:
a first power subsystem having a first electric machine mechanically coupled with a high pressure spool of the gas turbine engine and a second electric machine mechanically coupled with a low pressure spool of the gas turbine engine, the second electric machine being electrically coupled with the first electric machine such that electrical power is transmittable therebetween; and a second power subsystem having a third electric machine mechanically coupled with the low pressure spool, the third electric machine being electrically coupled with one or more electrical loads positioned offboard the gas turbine engine, and wherein the first power subsystem and the second power subsystem are electrically decoupled from one another.

2 . The power system of claim 1 , wherein the first power subsystem has a first power converter electrically connected to the first electric machine and a second power converter electrically connected to the second electric machine.

3 . The power system of claim 2 , wherein the first power converter and the second power converter are co-located.

4 . The power system of claim 2 , wherein the first power converter and the second power converter are spaced from one another and are electrically coupled by a DC bus.

5 . The power system of claim 2 , wherein the vehicle has a vehicle body and one or more electrical loads, and wherein the vehicle is an aircraft and the vehicle body includes a fuselage and a wing extending from the fuselage, and wherein a nacelle of the gas turbine engine is mounted to the wing via a pylon, the one or more electrical loads being positioned onboard the vehicle body but offboard the nacelle and the pylon.

6 . The power system of claim 5 , wherein the first power converter and the second power converter are positioned onboard the nacelle, the pylon, or both.

7 . The power system of claim 2 , wherein the first power converter and the second power converter are positioned onboard the fuselage.

8 . The power system of claim 7 , wherein a first line electrically connects the first electric machine with the first power converter and a second line electrically connects the second electric machine with the second power converter, a first contactor being disposed along the first line and being positioned onboard the fuselage and a second contactor being disposed along the second line and being positioned onboard the fuselage.

9 . The power system of claim 1 , wherein the vehicle has a vehicle body, and wherein a DC link is positioned between the third electric machine and a main AC bus positioned onboard the vehicle body.

10 . A vehicle, comprising:
a vehicle body; one or more electrical loads positioned onboard the vehicle body; a gas turbine engine mounted to the vehicle body, the gas turbine engine having at least two spools; and a power system, comprising:
a first power subsystem having a first electric machine mechanically coupled with a high pressure spool and a second electric machine mechanically coupled with a low pressure spool, the second electric machine being electrically coupled with the first electric machine such that electrical power is transmittable therebetween; and
a second power subsystem having a third electric machine mechanically coupled with the low pressure spool, the third electric machine being electrically coupled with the one or more electrical loads such that electrical power is transmittable therebetween, and wherein the first power subsystem and the second power subsystem are electrically decoupled from one another.

11 . The vehicle of claim 10 , wherein the first power subsystem has a first power converter electrically connected to the first electric machine and a second power converter electrically connected to the second electric machine.

12 . The vehicle of claim 11 , wherein the first power converter and the second power converter are co-located.

13 . The vehicle of claim 11 , wherein the first power converter and the second power converter are spaced from one another and are electrically coupled by a DC bus.

14 . The vehicle of claim 10 , wherein the vehicle has a vehicle body, and wherein a DC link is positioned between the third electric machine and a main AC bus positioned onboard the vehicle body.

15 . A method of vehicle power transmission, comprising:
transferring, by a first power subsystem, power between high pressure spool and a low pressure spool of a gas turbine engine by transmitting electrical power generated by a first electric machine mechanically coupled with the high pressure spool to a second electric machine mechanically coupled with the low pressure spool; and transmitting, by a second power subsystem, electrical power generated by a third electric machine mechanically coupled with the low pressure spool to one or more loads positioned offboard the gas turbine engine, and
wherein the first power subsystem and the second power subsystem are electrically decoupled from one another.

Assignees

• Gen Electric
• General Electric Deutschland Holding Gmbh

Inventors

• Prabhakaran Satish
• Osama Mohamed

Classifications

• B64D31/18

  for hybrid-electric power plants · CPC title

• B64D27/026

  comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine (Hybrid electric aircraft B64D27/33) · CPC title

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title

• B64D29/02

  associated with wings · CPC title

• B64D27/12

  within, or attached to, wings · CPC title