Systems and methods for reconditioning turbine engines in power generation systems
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-025/00
F01D-005/00
F01D-025/32
출원번호
US-0455965
(2012-04-25)
등록번호
US-9260968
(2016-02-16)
발명자
/ 주소
Dutta, Sandip
Maldonado, Jaime Javier
출원인 / 주소
General Electric Company
대리인 / 주소
Armstrong Teasdale LLP
인용정보
피인용 횟수 :
1인용 특허 :
19
초록▼
A flow control system is provided. The flow control system includes at least one control valve coupled to at least one nozzle of a turbine engine, wherein the control valve is configured to regulate fluid flow in a first direction or a second direction. The first direction is when the fluid is chann
A flow control system is provided. The flow control system includes at least one control valve coupled to at least one nozzle of a turbine engine, wherein the control valve is configured to regulate fluid flow in a first direction or a second direction. The first direction is when the fluid is channeled from a compressor to the nozzle and the second direction is when the fluid is channeled from the nozzle to an exhaust section of the turbine engine. A controller is coupled to the control valve and is configured to control the fluid flow in the first direction during operation of the turbine engine and to change the direction of the fluid flow from the first direction to the second direction to facilitate reconditioning of the turbine engine.
대표청구항▼
1. A flow control system comprising: at least one control valve coupled to at least one nozzle of a turbine section in a turbine engine and operable to change a direction of a fluid flow of a fluid in at least one conduit that extends between the at least one nozzle and said at least one control val
1. A flow control system comprising: at least one control valve coupled to at least one nozzle of a turbine section in a turbine engine and operable to change a direction of a fluid flow of a fluid in at least one conduit that extends between the at least one nozzle and said at least one control valve, wherein in a first direction the fluid is channeled from a compressor through the at least one conduit to the at least one nozzle and wherein in a second direction the fluid is channeled from the at least one nozzle through the at least one conduit to an exhaust section bypassing downstream section of the turbine section of the turbine engine; anda controller coupled to said at least one control valve, said controller configured to:control the fluid flow in the first direction during operation of the turbine engine; andchange the direction of the fluid flow from the first direction to the second direction to facilitate reconditioning of the turbine engine. 2. A flow control system in accordance with claim 1, wherein said at least one control valve comprises a first control valve, a second control valve, and a third control valve, said first control valve is coupled to a first nozzle, said second control valve is coupled to a second nozzle, and said third control valve is coupled to a third nozzle. 3. A flow control system in accordance with claim 1, wherein said at least one conduit includes a plurality of cooling passages defined within the turbine engine. 4. A flow control system in accordance with claim 3, wherein said controller is configured to change the direction of the fluid flow to cause particulates within the plurality of cooling passages to be channeled to the exhaust section. 5. A flow control system in accordance with claim 1, wherein said controller is configured to change the direction of the fluid flow to cause a plurality of particulates within the at least one nozzle to be channeled to the exhaust section. 6. A flow control system in accordance with claim 1, wherein said controller is configured to change the direction of the fluid flow during at least one of a start up of the turbine engine and a shut down of the turbine engine. 7. A flow control system in accordance with claim 1, wherein said controller is configured to change the direction of the fluid flow by transmitting at least one control parameter via at least one signal to said at least one control valve. 8. A power generation system comprising: a turbine engine comprising a turbine, at least one nozzle coupled to said turbine, and an exhaust section coupled to said at least one nozzle; anda flow control system coupled to said turbine engine, said flow control system comprising:at least one control valve coupled to said at least one nozzle and operable to change a direction of a fluid flow of a fluid in at least one conduit that extends between said at least one nozzle and said at least one control valve, wherein in a first direction the fluid is channeled from a compressor through the at least one conduit to said at least one nozzle and wherein in a second direction the fluid is channeled from said at least one nozzle through the at least one conduit to said exhaust section bypassing downstream section of the turbine; anda controller coupled to said at least one control valve, said controller configured to:control the fluid flow in the first direction during operation of said turbine engine; andchange the direction of the fluid flow from the first direction to the second direction to facilitate reconditioning of said turbine engine. 9. A power generation system in accordance with claim 8, wherein said at least one control valve comprises a first control valve, a second control valve, and a third control valve, said at least one nozzle includes a first nozzle coupled to said first control valve, a second nozzle coupled to said second control valve, and a third nozzle coupled to said third control valve. 10. A power generation system in accordance with claim 8, wherein said at least one conduit comprises a plurality of cooling passages defined between said at least one nozzle and said exhaust section, said at least one control valve is configured to regulate the fluid flow within said plurality of cooling passages. 11. A power generation system in accordance with claim 10, wherein said controller is configured to change the direction of the fluid flow to cause particulates within said plurality of cooling passages to be channeled to said exhaust section. 12. A power generation system in accordance with claim 8, wherein said controller is configured to change the direction of the fluid flow from to cause particulates within said at least one nozzle to be channeled to said exhaust section. 13. A power generation system in accordance with claim 8, wherein said controller is configured to change the direction of the fluid flow from during at least one of a start up of said turbine engine and a shut down of said turbine engine. 14. A power generation system in accordance with claim 8, wherein said controller is configured to change the direction of the fluid flow by transmitting at least one control parameter via at least one signal to said at least one control valve. 15. A method for reconditioning a turbine engine in a power generation system, said method comprising: operating at least one control valve that is coupled to at least one nozzle in a turbine section of the turbine engine to change a direction of a fluid flow of a fluid in at least one conduit that extends between the at least one nozzle and the at least one control valve, wherein in a first direction the fluid is channeled from a compressor through the at least one conduit to the at least one nozzle and wherein in a second direction the fluid is channeled from the at least one nozzle through the at least one conduit to an exhaust section bypassing downstream section of the turbine section of the turbine engine;controlling the fluid flow in the first direction during operation of the turbine engine, via a controller that is coupled to the at least one control valve; andchanging the direction of the fluid flow from the first direction to the second direction, via the controller, to facilitate reconditioning of the turbine engine. 16. A method in accordance with claim 15, wherein operating the at least one control valve further comprise operating the at least one control valve to regulate the fluid flow within the at least one conduit that includes a plurality of cooling passages defined between the at least one nozzle and the exhaust section. 17. A method in accordance with claim 16, wherein changing the direction of the fluid flow further comprises changing the direction of the fluid flow such that particulates within the plurality of cooling passages are channeled to the exhaust section. 18. A method in accordance with claim 15, wherein changing the direction of the fluid flow further comprises changing the direction of the fluid flow such that particulates within the at least one nozzle are channeled to the exhaust section. 19. A method in accordance with claim 15, wherein changing the direction of the fluid flow further comprises changing the direction of the fluid flow during at least one of a start up of the turbine engine and a shut down of the turbine engine. 20. A method in accordance with claim 15, wherein changing the direction of the fluid flow further comprises changing the direction of the fluid flow by transmitting at least one control parameter via at least one signal to said at least one control valve.
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