Multivariable fuel control and estimator (mfce) for preventing combustor blowout

Patent metadata

Field	Value
Publication number	US-2017328567-A1
Application number	US-201615152182-A
Country	US
Kind code	A1
Filing date	May 11, 2016
Priority date	May 11, 2016
Publication date	Nov 16, 2017
Grant date	—

Abstract

A multivariable fuel control and estimator (MFCE) of a gas turbine engine for preventing combustor blowout is provided. The MFCE includes a first input port that receives controller requests and provide system usage commands, a second input port that receives measured disturbance values, a third input that receives system and component limits, a fourth input port that receives sensed parameters, a fuel system model of the fuel system of the gas turbine engine and an engine model of the engine system that includes the combustor of the gas turbine engine, a processor that generates a control signal for controlling the fuel valve and generates a control signal for controlling the actuator using the fuel system and engine model based on the controller requests, the measured disturbance values, the system and component limits, and the sensed parameters, and an output port that transmits the control signals to the fuel system.

First claim

What is claimed is:

1 . A multivariable fuel control and estimator (MFCE) of a gas turbine engine for preventing combustor blowout, the MFCE comprising:
a first input port that is configured to receive controller requests and provide system usage commands; a second input port that is configured to receive measured disturbance values; a third input that is configured to receive system and component limits; a fourth input port that is configured to receive sensed parameters from a fuel system and an engine system; a fuel system model of the fuel system of the gas turbine engine and an engine model of the engine system that includes the combustor of the gas turbine engine; a processor that generates a control signal for controlling the fuel valve and generates a control signal for controlling the actuator using the fuel system model and the engine model based on the controller requests, the measured disturbance values, the system and component limits, and the sensed parameters; and an output port that transmits the control signals to the fuel system.

2 . The MFCE of claim 1 , wherein the output port is connected to a valve and an actuator of the fuel system, wherein the control signals control the valve and actuator.

3 . The MFCE of claim 1 , wherein the controller requests included in the first input include one or more from a group consisting of a specific fuel amount request, and an actuator position request.

4 . The MFCE of claim 1 , wherein the measured disturbance values include one or more of valve sensor, command signal data, and pump speed.

5 . The MFCE of claim 1 , wherein the system and component limits include one or more of a fuel flow minimum, a fuel flow maximum range, and rate limits.

6 . The MFCE of claim 1 , wherein the sensed parameters include one or more of fuel flow, valve position, and engine sensor readings.

7 . The MFCE of claim 1 , wherein the control signals control the flow rate of the fuel delivered to the combustor by adjusting one or more of an actuator and a valve of the fuel system.

8 . The MFCE of claim 1 , wherein generating the control signals comprises predicting a fluid flow delivered to the combustor using the fuel system model and engine model, adjusting one or more of a valve and actuator values in the fuel system model, recalculating the fluid flow in the fuel system, and repeating until the calculated fluid flow matches a desired fuel flow value delivered to the combustor.

9 . The MFCE of claim 1 , wherein the MFCE minimizes deviation of fuel flow to the combustor.

10 . A gas turbine engine comprising:
an engine system that comprises a combustor that receives and bums fuel; a fuel system that comprises a fuel supply connected to at least one valve and actuator, wherein the fuel system is connected to the engine system and provides fuel to the combustor; and a multivariable fuel control and estimator (MFCE) for preventing combustor blowout, the MFCE comprising:
a first input port configured to receive controller requests and provide system usage commands;
a second input port configured to receive measured disturbance values;
a third input configured to receive system and component limits;
a fourth input port configured to receive sensed parameters from the fuel system and the engine system;
a fuel system model of the fuel system of the gas turbine engine and an engine model of the engine system that includes the combustor of the gas turbine engine;
a processor that generates a control signal for controlling the fuel valve and generates a control signal for controlling the actuator using the fuel system model and the engine model based on the controller requests, the measured disturbance values, the system and component limits, and the sensed parameters; and
an output port that is configured to transmit the control signals to the fuel system.

11 . The gas turbine engine of claim 10 , wherein the output port is connected to a valve and an actuator of the fuel system, wherein the control signals control the valve and actuator.

12 . The gas turbine engine of claim 10 , wherein the controller requests included in the first input include one or more from a group consisting of a specific fuel amount request and an actuator command.

13 . The gas turbine engine of claim 10 , wherein the measured disturbance values include one or more of valve sensor, command signal data, and pump speed.

14 . The gas turbine engine of claim 10 , wherein the system and component limits include one or more of a fuel flow minimum, a fuel flow maximum range, and rate limits.

15 . The gas turbine engine of claim 10 , wherein the sensed parameters include one or more of fuel flow, valve position, and engine sensor readings.

16 . The gas turbine engine of claim 10 , wherein the control signals control the flow rate of fuel delivered to the combustor by adjusting one or more of an actuator and a valve of the fuel system.

17 . The gas turbine engine of claim 10 , wherein generating the control signals comprise predicting a fluid flow in the fuel system using the fuel system model and an engine model, adjusting one or more of a valve and actuator values in the fuel system model, recalculating the fluid flow in the fuel system, and repeating until the calculated fluid flow matches a desired fluid flow value.

18 . A method for preventing combustor blowout using a multivariable fuel control and estimator (MFCE) of a gas turbine engine, the method comprising:
receiving controller requests configured to provide system usage commands; receiving measured disturbance values; receiving system and component limits; receiving measured outputs from a fuel system and an engine system; generating a control signal, using a processor, for controlling a fuel system using a fuel system model and an engine model based on the controller requests, the measured disturbance values, the system and component limits, and the measured outputs; and transmitting the control signals to the fuel system.

Assignees

• United Technologies Corp

Inventors

• Crowley Timothy J
• Selstad Tyler J
• Gelwan David

Classifications

• F23N2231/06

  for flame failures · CPC title

• F23N2241/20

  Gas turbines · CPC title

• F23N5/003

  using detectors sensitive to combustion gas properties (F23N5/02, F23N5/18 - F23N5/26 take precedence) · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F23N1/002

  using electronic means (F23N1/04 - F23N1/10 take precedence) · CPC title