Power generation system having compressor creating excess gas flow for supplemental gas turbine system
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01K-023/10
F02C-006/02
F02C-006/00
F02C-006/18
F02C-009/18
F02C-003/10
F02C-006/08
출원번호
US-0662836
(2015-03-19)
등록번호
US-9863285
(2018-01-09)
발명자
/ 주소
Ekanayake, Sanji
Freeman, Thomas John
Memmer, John David
Rehg, Timothy Joseph
Scipio, Alston Ilford
출원인 / 주소
General Electric Company
대리인 / 주소
Cusick, Ernest G.
인용정보
피인용 횟수 :
0인용 특허 :
15
초록▼
A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combu
A power generation system may include a generator; a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor and a combustor to which air from the integral compressor and fuel are supplied, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow. A first control valve system controls flow of the excess air flow along an excess air flow path to a supplemental gas turbine system. The excess air flow may be combusted with a fuel and supplied to the supplemental gas turbine system. An eductor may be positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional gas.
대표청구항▼
1. A power generation system, comprising: a generator;a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor, a combustor to which air from the integral compressor and fuel are supplied, and a first rotatable shaft coupled to the
1. A power generation system, comprising: a generator;a gas turbine system for powering the generator, the gas turbine system including a turbine component, an integral compressor, a combustor to which air from the integral compressor and fuel are supplied, and a first rotatable shaft coupled to the gas turbine system, the combustor arranged to supply hot combustion gases to the turbine component, and the integral compressor having a flow capacity greater than an intake capacity of at least one of the combustor and the turbine component, creating an excess air flow;a supplemental gas turbine system including a second rotatable shaft and a supplemental combustor arranged to supply hot combustion gases of the supplemental combustor to a supplemental turbine component thereof, the supplemental turbine component operatively coupled to a supplemental generator;a first control valve system controlling flow of the excess air flow along an excess air flow path; andan eductor positioned in the excess air flow path for using the excess air flow as a motive force to augment the excess air flow with additional gas, the educator creating an augmented excess gas flow,wherein the excess air flow path feeds the augmented excess gas flow directly to the intake of the supplemental combustor, and the supplemental combustor combusts the augmented excess gas flow with the fuel to create the hot combustion gases of the supplemental combustor for the supplemental turbine component;wherein an exhaust of the turbine component feeds a heat recovery steam generator (HRSG) for creating steam for a steam turbine system, the steam turbine system including a third rotatable shaft; andwherein the first, second, and third rotatable shafts are not within one another. 2. The power generation system of claim 1, wherein the HRSG also feeds steam to a co-generation steam load. 3. The power generation system of claim 1, wherein the first control valve system includes a compressor discharge control valve controlling a first portion of the excess air flow taken from a discharge of the integral compressor, and an upstream control valve controlling a second portion of the excess air flow taken from a stage of the integral compressor upstream from the discharge. 4. The power generation system of claim 3, further comprising at least one sensor for measuring a flow rate of each portion of the excess air flow, each sensor operably coupled to a respective control valve. 5. The power generation system of claim 1, wherein the eductor includes a suction side flow path, and further comprising a second control valve system in the suction side flow path controlling a flow of the additional gas into the eductor. 6. The power generation system of claim 5, wherein the suction side flow path is fluidly coupled to an inlet filter of the integral compressor. 7. The power generation system of claim 1, further comprising a sensor for measuring a flow rate of the additional gas in a suction side flow path of the eductor, the sensor operably coupled to the second control valve system. 8. The power generation system of claim 1, wherein a suction side flow path of the eductor is fluidly coupled to an inlet filter of the integral compressor. 9. The power generation system of claim 1, wherein the generator that is different than the supplement generator. 10. The power generation system of claim 1, wherein the additional gas includes ambient air. 11. The power generation system of claim 1, wherein the additional gas includes a process gas. 12. The power generation system of claim 1, wherein the additional gas includes a synthesis gas. 13. The power generation system of claim 1, wherein the additional gas includes exhaust from an engine.
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이 특허에 인용된 특허 (15)
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Frutschi Hansulrich (Riniken CHX), Method for regulating a power plant containing a gas turbine assembly and apparatus for the performance of the aforesaid.
Ekanayake, Sanji; Scipio, Alston Ilford; Davis, Dale J.; Pastrana, Ryan Margate, Systems and methods for de-icing a gas turbine engine inlet screen and dehumidifying inlet air filters.
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