# US 2021/0172384 A1 · Electric machine assistance for multi-spool turbomachine operation and control

> Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt

- Number: US 2021/0172384 A1
- Document ID: US20210172384A1
- Status: Published application
- Kind: A1
- Application number: 16/705,341
- Filed: 2019-12-06
- Published: 2021-06-10
- Earliest claimed: 2019-12-06
- Assignees: General Electric Company
- Applicants: General Electric Company
- Inventors: Thomas William Brown; Justin Paul Smith; Dominic Barone
- Web page: https://patentgrep.com/patent/US20210172384A1

## CPC

- F02C 9/28: Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence)
- F02C 9/48: Control of fuel supply conjointly with another control of the plant (with nozzle section control F02K1/17)
- F02C 6/20: Adaptations of gas-turbine plants for driving vehicles
- F02C 7/32: Arrangement, mounting, or driving, of auxiliaries
- 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)
- F02K 5/00: Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
- F05D 2220/30: in turbines
- F05D 2220/76: an electrical generator
- 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)
- 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

## Abstract

A multi-spool turbomachine having an electric machine that can be controlled to input power to one of the spools of the turbomachine is provided. In one aspect, the multi-spool turbomachine can be a hybrid electric gas turbine engine for an aircraft. The hybrid electric gas turbine engine can include a first spool, a second spool, and an electric machine operatively coupled with the first spool. In response to an increase in thrust demand, the electric motor receives electrical power from an electrical power source. In turn, the electric machine applies a torque to the first spool, causing the first spool to increase in rotational speed. In this manner, the electric machine can electrically assist the turbomachine to meet the increase in thrust demand.

## Claims

### Claim 1

A vehicle, comprising:
a gas turbine engine, comprising:
a first rotatable component;
a second rotatable component;
an electric machine operatively coupled with the first rotatable component and in communication with an electrical power source, the electric machine being operable to receive electrical power from the electrical power source;
a computing system having one or more processors and one or more memory devices, the one or more memory devices storing instructions that when executed by the one or more processors cause the one or more processors to perform operations, in performing the operations, the one or more processors are configured to:
receive an input indicating a change in a thrust demand to the gas turbine engine; and
in response to the received input indicating the change in the thrust demand to the gas turbine engine, cause the electric machine to change an applied torque on the first rotatable component such that a rotational speed of the first rotatable component is changed.

### Claim 2 (depends on 1)

The vehicle of claim 1, wherein the first rotatable component is a low pressure spool and the second rotatable component is a high pressure spool.

### Claim 3 (depends on 1)

The vehicle of claim 1, wherein the first rotatable component is a high pressure spool and the second rotatable component is a low pressure spool.

### Claim 4 (depends on 1)

The vehicle of claim 1, wherein the change in the thrust demand to the gas turbine engine is a decrease in the thrust demand to the gas turbine engine, and wherein when the one or more processors cause the electric machine to change the applied torque on the first rotatable component, the electric machine decreases the applied torque on the first rotatable component or causes the electric machine to apply a drag torque on the first rotatable component such that the rotational speed of the first rotatable component is decreased.

### Claim 5 (depends on 1)

The vehicle of claim 1, wherein the change in the thrust demand to the gas turbine engine is an increase in the thrust demand to the gas turbine engine, and wherein when the one or more processors cause the electric machine to change the applied torque on the first rotatable component, the electric machine increases the applied torque on the first rotatable component such that the rotational speed of the first rotatable component is increased.

### Claim 6 (depends on 5)

The vehicle of claim 5, wherein in response to the received input indicating the change in the thrust demand to the gas turbine engine, the one or more processors are configured to:
cause, at rate not to exceed a predefined rate, an increase in fuel flow to the gas turbine engine such that the rotational speed of the second rotatable component is increased.

### Claim 7 (depends on 1)

The vehicle of claim 1, wherein the one or more processors are configured to:
determine a thrust demand schedule to meet the thrust demand over time based at least in part on the received input indicating the change in the thrust demand to the gas turbine engine, the thrust demand schedule including a schedule of fuel flow to the gas turbine engine over time and a schedule of electrical current flow to the electric machine over time, and
wherein the one or more processors:
i) control fuel flow to the gas turbine engine over time based at least in part on the determined schedule of fuel flow to the gas turbine engine over time; and
ii) control electrical current flow to the electric machine over time based at least in part on the determined schedule of electrical current flow to the electric machine over time.

### Claim 8 (depends on 7)

The vehicle of claim 7, wherein the one or more processors are configured to:
receive an input indicative of one or more operating conditions of the gas turbine engine, and
wherein the thrust demand schedule is determined by the one or more processors based at least in part on the input indicative of the one or more operating conditions of the gas turbine engine.

### Claim 9 (depends on 8)

The vehicle of claim 8, wherein the one or more operating conditions of the gas turbine engine include at least one of an altitude at which the gas turbine engine is operating, an airspeed of the vehicle, and an ambient temperature outside of the vehicle.

### Claim 10 (depends on 7)

The vehicle of claim 7, wherein the gas turbine engine further comprises a fuel control device operable to control fuel flow to the gas turbine engine, the fuel control device being communicatively coupled with the computing system, and
wherein the vehicle further comprises an electrical current control device operable to control electrical current flow to the electric machine, the electrical current control device being communicatively coupled with the computing system, and
wherein the schedule of fuel flow to the gas turbine engine over time includes one or more fuel flow commands and the schedule of electrical current flow to the electric machine over time includes one or more electrical current commands, and
wherein in controlling fuel flow to the gas turbine over time based at least in part on the determined schedule of fuel flow to the gas turbine engine over time, the one or more processors are configured to cause the fuel control device to control fuel flow to the gas turbine engine based at least in part on the one or more fuel flow control commands, and
wherein in controlling electrical current flow to the electric machine over time based at least in part on the determined schedule of electrical current flow to the electric machine over time, the one or more processors are configured to cause the electrical current control device to control electrical current to the electric machine based at least in part on the one or more electrical current control commands.

### Claim 11 (depends on 7)

The vehicle of claim 7, wherein the one or more processors control fuel flow to the gas turbine engine over time and control electrical current flow to the electric machine over time such that fuel flow to the gas turbine engine is gradually ramped up over time and electrical current flow to the electric machine is ramped down over time.

### Claim 12

A turbomachine for a vehicle, comprising:
a first rotatable component;
a second rotatable component;
an electric machine operatively coupled with the first rotatable component; and
a controller having one or more processors and one or more memory devices, the one or more memory devices storing instructions that when executed by the one or more processors cause the one or more processors to perform operations, in performing the operations, the one or more processors are configured to:
receive an input indicating an increase in thrust demand to the turbomachine; and
in response to the increase in the thrust demand to the turbomachine, cause the electric machine to apply torque to the first rotatable component.

### Claim 13 (depends on 12)

The turbomachine of claim 12, wherein the first rotatable component is a low pressure spool and the second rotatable component is a high pressure spool.

### Claim 14 (depends on 12)

The turbomachine of claim 12, wherein the first rotatable component is a high pressure spool and the second rotatable component is a low pressure spool.

### Claim 15 (depends on 12)

The turbomachine of claim 12, wherein the one or more processors of the controller are configured to:
cause an increase in a fuel flow to the turbomachine such that a rotational speed of the second rotatable component is increased.

### Claim 16 (depends on 15)

The turbomachine of claim 15, wherein the one or more processors of the controller control the increase in the fuel flow to the turbomachine over a first time period and control an electrical current flow to the electric machine over the first time period such that the fuel flow to the turbomachine is gradually increased over the first time period and the electrical current flow to the electric machine is decreased over the first time period.

### Claim 17 (depends on 12)

The turbomachine of claim 12, wherein the one or more processors of the controller are configured to:
receive an input indicative of a constraint descriptive of a fuel input threshold, and
wherein when fuel flow to the turbomachine reaches the fuel input threshold, the increase in thrust demand is met solely by application of torque applied to the first rotatable component by the electric machine.

### Claim 18

A method, comprising:
receiving, by one or more computing devices, an input indicating an increase in thrust demand to a multi-spool turbomachine having a first spool and a second spool;
in response to the received input indicating the increase in thrust demand to the multi-spool turbomachine, causing, by the one or more computing devices, an electric machine operatively coupled with the first spool to increase a rotational speed of the first spool.

### Claim 19 (depends on 18)

The method of claim 18, wherein causing, by the one or more computing devices, the electric machine to increase the rotational speed of the first spool comprises causing, by the one or more computing devices, the electric machine to apply torque to the first spool such that the rotational speed of the first spool increases independent of the second spool.

### Claim 20 (depends on 19)

The method of claim 19, wherein causing, by the one or more computing devices, the electric machine operatively coupled with the first spool to increase the rotational speed of the first spool comprises causing, by the one or more computing devices, the electric machine to increase the rotational speed of the first spool such that the thrust demand is substantially met, and wherein the method further comprises:
causing, by the one or more computing devices, a fuel flow to a combustor of the multi-spool turbomachine, wherein the fuel flow to the combustor increases gradually at over a first time period; and
after causing, by the one or more computing devices, the electric machine to increase the rotational speed of the first spool such that the thrust demand is substantially met, causing, by the one or more computing devices, an electrical current flow to the electric machine to decrease over the first time period.