METHODS AND APPARATUS FOR ESTIMATING ENGINE THRUST

• US 20070260424A1
• Filed: 05/05/2006
• Published: 11/08/2007
• Est. Priority Date: 05/05/2006
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Brown, Harold, Desai, Premal
• Application Number:
  US11/381,821
• Publication Number:
  US 20070260424A1
• Time in Patent Office: Days
• US Class Current: 702/182
• CPC Class Codes: 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
• CPC Class Codes: F05D 2270/051 Thrust
• CPC Class Codes: F05D 2270/71 synthesized, i.e. parameter computed by a mathematical model

Abstract

A method for estimating engine thrust, wherein the method includes obtaining information about an initial dynamic state of the engine and updating the information about the initial dynamic state of the engine to reflect a second dynamic state of the engine. The method also includes generating engine thrust estimates, wherein the thrust estimates facilitate implementing direct thrust control.

Claims

1. A method for estimating engine thrust, said method comprising:

obtaining information about an initial dynamic state of the engine; and

updating the information about the initial dynamic state of the engine to reflect a second dynamic state of the engine; and

generating engine thrust estimates, wherein the thrust estimates facilitate implementing direct thrust control.

2. A method in accordance with claim 1 further comprising continuously updating the initial dynamic state estimates for a subsequent time step based on the initial dynamic state estimates and expected changes in control inputs.

3. A method in accordance with claim 1 wherein obtaining information about the current state of the engine comprises obtaining information about at least one of an engine system, an actuator, and a sensor.

4. A method in accordance with claim 1 wherein updating the information further comprises updating at least one of a dynamic performance state, a control input, a variable, a component variable, an equipment position error, an equipment sensor output error, a parameter, a performance parameter, a quality parameter, a scalar, an adder, a constraint, an objective function, a limit, an adaptable parameter during steady state operation, and an adaptable parameter during transient operation.

5. A method in accordance with claim 1 wherein updating the information further comprises updating the information using engine thrust as a first system state and high pressure turbine inlet temperature as a second system state.

6. A method in accordance with claim 1 wherein generating engine thrust estimates further comprises generating engine thrust estimates using at least one of a Kalman filter, a linear estimator, a non-linear estimator, a linear state estimator, a non-linear state estimator, a linear parameter estimator, a non-linear parameter estimator, a linear filter, a non-linear filter, a linear tracking filter, a non-linear tracking filter, linear logic, non-linear logic, linear heuristic logic, non-linear heuristic logic, linear knowledge base, and non-linear knowledge base.

7. A method in accordance with claim 6 wherein generating engine thrust estimates further comprises generating engine thrust estimates using engine thrust as a first system state and high pressure turbine inlet temperature as a second system state and obtaining outputs at the first system state linearly independently of the second system state.

8. A method in accordance with claim 7 wherein obtaining outputs at the first system state linearly independently of the second system state further comprises weighting the outputs with respect to at least one of an engine sensor error, a variance of each component engine-to-engine quality variation, and an actuator position error.

9. An apparatus for estimating engine thrust, said apparatus comprising a processor coupled to the engine for receiving input from the plurality of sensors, said processor programmed to:

obtain information from the engine during a first operating condition;

update information from the engine during a second operating condition; and

generate engine thrust estimates utilizing the obtained information and the updated information and implementing direct thrust control.

10. An apparatus in accordance with claim 9 wherein to obtain information from the engine comprises obtaining information about at least one of an engine system, an actuator, and a sensor.

11. An apparatus in accordance with claim 9 wherein to update the information further comprises updating at least one of a dynamic performance state, a control input, a variable, a component variable, an equipment position error, an equipment sensor output error, a parameter, a performance parameter, a quality parameter, a scalar, an adder, a constraint, an objective function, a limit, an adaptable parameter during steady state operation, and an adaptable parameter during transient operation.

12. An apparatus in accordance with claim 9 wherein to update the information further comprises updating the information using engine thrust as a first system state and high pressure turbine inlet temperature as a second system state.

13. An apparatus in accordance with claim 9 wherein to generate engine thrust estimates further comprises generating engine thrust estimates using at least one of a Kalman filter, a linear estimator, a non-linear estimator, a linear state estimator, a non-linear state estimator, a linear parameter estimator, a non-linear parameter estimator, a linear filter, a non-linear filter, a linear tracking filter, a non-linear tracking filter, linear logic, non-linear logic, linear heuristic logic, non-linear heuristic logic, linear knowledge base, and non-linear knowledge base.

14. An apparatus in accordance with claim 9 wherein to generate engine thrust estimates further comprises generating engine thrust estimates using an engine thrust as a first system state and a high pressure turbine inlet temperature as a second system state, and to obtain outputs at the first system state linearly independently of the second system state.

15. An apparatus in accordance with claim 14 wherein to obtain outputs further comprises weighting the outputs with respect to at least one of an engine sensor error, a variance of each component engine-to-engine quality variation, and an actuator position error.

16. A system for controlling a gas turbine engine, said system comprising:

at least one model capable of representing a system behavior; and

at least one thrust estimator capable of estimating engine thrust.

17. A system in accordance with claim 16 wherein said system behavior comprises at least one of a steady-state behavior and a transient behavior.

18. A system in accordance with claim 16 wherein said system is configured to transform a conventional thrust estimator based on low pressure and high pressure rotor speeds to a dynamic thrust estimator based on dynamic states such as engine thrust and high pressure turbine inlet temperature.

19. A system in accordance with claim 18 wherein said dynamic thrust estimator is configured to obtain initial engine sensor measurements, allow direct estimation of the engine dynamic states based on said initial engine sensor measurements, and allow direct thrust control.

20. A system in accordance with claim 19 wherein said dynamic thrust estimator is updated from said initial dynamic state estimates for a subsequent time step based on said initial dynamic state estimates and expected changes in control inputs.