Wash timing based on turbine operating parameters

Patent metadata

Field	Value
Publication number	US-9605559-B2
Application number	US-201514611957-A
Country	US
Kind code	B2
Filing date	Feb 2, 2015
Priority date	Feb 2, 2015
Publication date	Mar 28, 2017
Grant date	Mar 28, 2017

Abstract

A system may include a memory storing a turbomachinery degradation model configured to model degradation of a turbine system over time. Further, the system may include a controller communicatively coupled to the memory, which derives a turbomachinery wash timing based on at least one input signal from the turbine system and the turbomachinery degradation model. The turbomachinery degradation model may derive a desired wash point by estimating a modeled power of the turbine system, a modeled heat rate of the turbine system, or both. Furthermore, the controller may use the desired wash point to determine a time for washing components of the turbine system.

First claim

The invention claimed is:

1. A system, comprising:
a memory storing a turbomachinery degradation model configured to model degradation of a turbine system over time; and
a controller communicatively coupled to the memory and configured to derive a turbomachinery wash timing based on at least one input signal from the turbine system and the turbomachinery degradation model, wherein the turbomachinery degradation model is configured to derive a desired wash point by estimating a modeled power of the turbine system, a modeled heat rate of the turbine system, or both, and wherein the controller is configured to use the desired wash point to determine a time for washing components of the turbine system and control the turbine system to operate in a clean mode by controlling an injection of water into the turbine system when the time for washing the components of the turbine system is surpassed, wherein the controller is configured to derive the desired wash point by measuring when a sustained power output of the turbine system no longer maintains a constant output.

2. The system of claim 1 , wherein the controller is configured to maintain a steady output of the turbine system, a steady heat rate of the turbine system, or both over time until the time for washing the components of the turbine system is surpassed.

3. The system of claim 1 , wherein the clean mode comprises driving the turbine system offline for cleaning.

4. The system of claim 1 , wherein the at least one input signal comprises a firing temperature, an inlet guide vane (IGV) angle, a combustor temperature rise, an exhaust temperature, or a combination thereof.

5. The system of claim 1 , wherein the turbomachinery degradation model is configured to derive the wash point by estimating the modeled power and estimating a modeled firing heat of the turbine system.

6. The system of claim 1 , wherein the turbomachinery degradation model is configured to adjust over time based on the at least one input signal from the turbine system.

7. The system of claim 1 , wherein the turbomachinery degradation model comprises a physics-based model, a statistical model, a heuristic model, or a combination thereof.

8. The system of claim 1 , wherein the turbine system comprises a gas turbine, a steam turbine, a hydroturbine, a wind turbine, or a combination thereof.

9. The system of claim 1 , comprising a sensor communicatively coupled to the controller and configured to transmit the at least one input signal, and wherein the at least one input signal is representative of a measured power, a measured heat rate, or a combination thereof.

10. A method, comprising:
storing a turbomachinery degradation model in a memory, wherein the turbomachinery degradation model is configured to model degradation of a turbine system over time;
receiving an input signal from one or more sensors;
receiving a target power;
deriving a wash point using the turbomachinery degradation model and the target power wherein the deriving the wash point comprises measuring when a sustained power output of the turbine system no longer maintains a constant output;
determining whether the turbine system has reached the wash point based on the input signal; and
controlling the turbine system to enter a wash mode.

11. The method of claim 10 , comprising adjusting the turbomachinery degradation model based on the input signal from the one or more sensors.

12. The method of claim 10 , wherein the wash mode comprises an online wash or an offline wash of components of the turbine system.

13. The method of claim 12 , wherein the offline wash comprises removing the turbine system from the baseload and allowing the turbine system to cool.

14. The method of claim 12 , wherein the online wash and the offline wash comprise injecting water into a compressor of the turbine system.

15. A controller, comprising:
at least one processor adapted to execute instructions configured to cause the controller to:
access a turbomachinery degradation model stored in a memory, wherein the turbomachinery degradation model is configured to model degradation of a turbine system over time;
receive an input signal from one or more sensors;
receive a target power;
derive a wash point using the turbomachinery degradation model and the target power wherein the instructions cause the controller to derive the wash point by measuring when a sustained power output of the turbine system no longer maintains a constant output; and
control the turbine system to enter a wash mode at the wash point.

16. The controller of claim 15 , wherein the input signal comprises a firing temperature, an inlet guide vane (IGV) angle, a combustor temperature rise, an exhaust temperature, or a combination thereof.

17. The controller of claim 16 , wherein deriving the wash point comprises adjusting the wash point based on changes in efficiency of the turbine system.

18. The controller of claim 15 , turbine system comprises a turbine engine, wherein the wash mode comprises an online wash where the turbine engine continues operations or an offline wash where the turbine engine is stopped and allowed to cool.

19. The controller of claim 15 , wherein the instructions are configured to adjust the turbomachinery degradation model based on the input signal from the one or more sensors.

Assignees

• Gen Electric

Inventors

• Truesdale Alan Meier
• Ewens David Spencer
• Abrol Sidharth

Classifications

• F02C9/00

  Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants (controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05) · CPC title

• F05D2220/31

  in steam turbines · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title

• F01D25/002 Primary

  Cleaning of turbomachines · CPC title

• F05D2270/303

  Temperature · CPC title