Control system for a turbogenerator and method
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorSebastian Nowoisky
Life of this patent
Estimating the term…
Abstract
An open-loop control system for a turbogenerator includes a closed-loop speed control module having: an input; a plurality of closed-loop controllers each configured to output an open-loop control signal based on a speed signal applied to the input; and an output. The closed-loop speed control module is configured to generate an output signal based on the speed signal from one or more of the open-loop control signals of the plurality of closed-loop controllers and to output a same signal at the output.
Claims17
An open-loop control system for a turbogenerator, the open-loop control system comprising:
- a closed-loop speed controller having:
- an input;
- a plurality of closed-loop controllers arranged in parallel, wherein each closed-loop controller of the plurality of closed-loop controllers is set differently, and wherein each closed-loop controller of the plurality of closed-loop controllers is configured to output a different open-loop control signal based on a speed signal applied to the input;
- and
- an output,
- wherein the closed-loop speed controller is configured to select one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers depending on the speed signal and generate an output signal using the selected one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers, and
- wherein the closed-loop speed controller is configured to output the output signal at the output;
- and
- a closed-loop thrust controller configured to receive the output signal of the closed-loop speed controller,
- wherein the closed-loop thrust controller is configured to output an open-loop control signal based on the output signal to adjust a fuel valve to the turbogenerator.
A turbogenerator for an aircraft, the turbogenerator comprising:
- an open-loop control system having:
- a closed-loop speed controller, wherein the closed-loop speed controller comprises:
- an input;
- a plurality of closed-loop controllers arranged in parallel, wherein each closed-loop controller of the plurality of closed-loop controllers is set differently, and wherein each closed-loop controller of the plurality of closed-loop controllers is configured to output a different open-loop control signal based on a speed signal applied to the input;
- and
- an output,
- wherein the closed-loop speed controller is configured to select one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers depending on the speed signal and generate an output signal using the selected one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers, and
- wherein the closed-loop speed controller is configured to output the output signal at the output;
- and
- a closed-loop thrust controller configured to receive the output signal of the closed-loop speed controller,
- wherein the closed-loop thrust controller is configured to output an open-loop control signal based on the output signal to adjust a fuel valve to the turbogenerator.
An aircraft comprising:
- a fuel valve;
- a turbogenerator;
- and
- an electric motor configured to generate thrust and/or lift, wherein the electric motor is electrically coupled to the turbogenerator and supplied with electric current from the turbogenerator,
- wherein the turbogenerator comprises:
- an open-loop control system having:
- a closed-loop speed controller comprising:
- an input;
- a plurality of closed-loop controllers arranged in parallel, wherein each closed-loop controller of the plurality of closed-loop controllers is set differently, and wherein each closed-loop controller of the plurality of closed-loop controllers is configured to output a different open-loop control signal based on a speed signal applied to the input;
- and
- an output,
- wherein the closed-loop speed controller is configured to select one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers depending on the speed signal and generate an output signal using the selected one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers, and
- wherein the closed-loop speed controller is configured to output the output signal at the output;
- and
- a closed-loop thrust controller configured to receive the output signal of the closed-loop speed controller,
- wherein the closed-loop thrust controller is configured to output an open-loop control signal based on the output signal to adjust the fuel valve to the turbogenerator.
A method for open-loop control of a turbogenerator, the method comprising:
- applying a speed signal to an input of a closed-loop speed controller of an open-loop control system of the turbogenerator;
- outputting, by each closed-loop controller of a plurality of closed-loop controllers of the closed-loop speed controller, a different open-loop control signal based on the speed signal applied to the input of the closed-loop speed controller, wherein each closed-loop controller of the plurality of closed-loop controllers is set differently, and wherein closed-loop controllers of the plurality of closed-loop controllers are arranged in parallel;
- selecting, by the closed-loop speed controller, one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers depending on the speed signal;
- generating, by the closed-loop speed controller, an output signal using the selected one or more open-loop control signals of the open-loop control signals of the plurality of closed-loop controllers;
- outputting the output signal at an output of the closed-loop speed controller;
- receiving, by a closed-loop thrust controller, the output signal from the closed-loop speed controller;
- and
- outputting, by the closed-loop thrust controller, an open-loop control signal based on the output signal to adjust a fuel valve to the turbogenerator.
Dependencies are inferred from the claim text.