# US 12,006,052 B2 · Electrical power system for a vehicle > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 12,006,052 B2 - Document ID: US12006052B2 - Status: Granted - Kind: B2 - Application number: 17/972,919 - Filed: 2022-10-25 - Published: 2023-11-02 - Granted: 2024-06-11 - Earliest claimed: 2022-04-27 - Assignees: General Electric Company; General Electric Deutschland Holding GmbH - Applicants: General Electric Company; General Electric Deutschland Holding GmbH - Inventors: Satish Prabhakaran; Mohamed Osama - Web page: https://patentgrep.com/patent/US12006052B2 ## CPC - F02C 3/113: with variable power transmission between rotors - B64D 27/12: within, or attached to, wings - B64D 29/02: associated with wings - B64D 31/18: for hybrid-electric power plants - F02C 7/32: Arrangement, mounting, or driving, of auxiliaries - F02K 5/00: Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan - B64D 27/026: {comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine (Hybrid electric aircraft B64D27/33)} - B64D 2221/00: Electric power distribution systems onboard aircraft - F02K 3/06: with front fan - F05D 2220/76: an electrical generator - F05D 2260/40: Transmission of power - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## 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. ## Claims ### 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 first spool of at least two spools of the gas turbine engine and a second electric machine mechanically coupled with a second spool of at least two spools of the gas turbine engine, the second electric machine being electrically coupled with the first electric machine such that electrical power is transmittable therebetween; a second power subsystem having a third electric machine mechanically coupled with the first spool, the third electric machine being electrically coupled with one or more electrical loads positioned offboard the gas turbine engine; and an accessory gearbox indirectly mechanically coupling the first electric machine and the third electric machine to the first spool; wherein the first power subsystem and the second power subsystem are electrically decoupled from one another. ### Claim 2 (depends on 1) The power system of claim 1, wherein the first spool is a high pressure spool and the second spool is a low pressure spool of the gas turbine engine. ### Claim 3 (depends on 1) 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. ### Claim 4 (depends on 3) The power system of claim 3, wherein the first power converter and the second power converter are co-located. ### Claim 5 (depends on 3) The power system of claim 3, wherein the first power converter and the second power converter are spaced from one another and are electrically coupled by a DC bus. ### Claim 6 (depends on 3) A vehicle, comprising: a vehicle body; a gas turbine engine mounted to the vehicle body; one or more electrical loads, the one or more electrical loads being positioned onboard the vehicle body of the vehicle but offboard a nacelle and a pylon of the gas turbine engine, wherein the vehicle is an aircraft and the vehicle body includes a fuselage and a wing extending from the fuselage, and wherein the nacelle of the gas turbine engine is mounted to the wing via the pylon; and the power system of claim 3. ### Claim 7 (depends on 6) The vehicle of claim 6, wherein the first spool is a high pressure spool and the second spool is a low pressure spool of the gas turbine engine, the third electric machine being mechanically coupled with the first spool, and wherein the first power converter and the second power converter are positioned onboard the nacelle, the pylon, or both. ### Claim 8 (depends on 1) The power system of claim 1, wherein the third electric machine is mechanically coupled to one of the first spool and the second spool. ### Claim 9 (depends on 1) The power system of claim 1, further comprising a DC link positioned between the third electric machine and a main AC bus positioned onboard a vehicle body of the vehicle. ### Claim 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 first spool of the at least two spools and a second electric machine mechanically coupled with a second spool of the at least two spools, the second electric machine being electrically coupled with the first electric machine such that electrical power is transmittable therebetween; a second power subsystem having a third electric machine mechanically coupled with the first spool, the third electric machine being electrically coupled with the one or more electrical loads such that electrical power is transmittable therebetween; and an accessory gearbox indirectly mechanically coupling the first electric machine and the third electric machine to the first spool; wherein the first power subsystem and the second power subsystem are electrically decoupled from one another. ### Claim 11 A method of vehicle power transmission, comprising: transferring, by a first power subsystem, power between a first spool and a second spool of at least two spools of a gas turbine engine by transmitting electrical power generated by a first electric machine mechanically coupled with the first spool to a second electric machine mechanically coupled with the second spool; and transmitting, by a second power subsystem, electrical power generated by a third electric machine mechanically coupled with the first spool to one or more loads positioned offboard the gas turbine engine; wherein the first power subsystem and the second power subsystem are electrically decoupled from one another; and wherein an accessory gearbox indirectly mechanically couples the first electric machine and the third electric machine to the first spool.