Wash timing based on turbine operating parameters
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-025/00
F01D-021/10
F02C-009/00
F03B-015/00
F03D-007/04
출원번호
US-0611957
(2015-02-02)
등록번호
US-9605559
(2017-03-28)
발명자
/ 주소
Truesdale, Alan Meier
Ewens, David Spencer
Abrol, Sidharth
출원인 / 주소
General Electric Company
대리인 / 주소
Fletcher Yoder, P.C.
인용정보
피인용 횟수 :
16인용 특허 :
13
초록▼
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 fr
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.
대표청구항▼
1. A system, comprising: a memory storing a turbomachinery degradation model configured to model degradation of a turbine system over time; anda controller communicatively coupled to the memory and configured to derive a turbomachinery wash timing based on at least one input signal from the turbine
1. A system, comprising: a memory storing a turbomachinery degradation model configured to model degradation of a turbine system over time; anda 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; andcontrolling 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; andcontrol 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.
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이 특허에 인용된 특허 (13)
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Davis, Jr., Lewis Berkley; Day, Scott Arthur; Jordan, Jr., Harold Lamar; Morgan, Rex Allen, Power output and fuel flow based probabilistic control in gas turbine tuning, related control systems, computer program products and methods.
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Jordan, Jr., Harold Lamar; Davis, Jr., Lewis Berkley; Day, Scott Arthur; Ewens, David Spencer; Morgan, Rex Allen, Probabilistic control in gas turbine tuning for power output-emissions parameters, related control systems, computer program products and methods.
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