Gas turbine system and method for controlling the same
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H02P-007/66
H02P-009/04
F02N-011/04
B60L-011/02
출원번호
US-0102598
(2002-03-18)
우선권정보
JP-0226040 (2001-07-26)
발명자
/ 주소
Ichinose, Masaya
Futami, Motoo
Arita, Hiroshi
출원인 / 주소
Hitachi, Ltd.
대리인 / 주소
Hogan & Hartson, LLP
인용정보
피인용 횟수 :
10인용 특허 :
6
초록▼
In a gas turbine system having first power converter converting power system N AC voltage to DC voltage, second power converter converting the DC voltage into AC voltage, generator connected to second power converter's AC output and rotated by turbine and turbine controller outputting a revolution s
In a gas turbine system having first power converter converting power system N AC voltage to DC voltage, second power converter converting the DC voltage into AC voltage, generator connected to second power converter's AC output and rotated by turbine and turbine controller outputting a revolution speed command value omg* according to a fuel flow rate of the turbine, a detector for detects a revolution speed omg of the generator, another detector detects Vdc of the first converter, a speed regulator generats a DC voltage command value according to a difference between omg and omg*, a switchover unit selects either a preset DC voltage command value Vref or the DC voltage command value according to the revolution speed omg and a voltage regulator and a controller control first power converter conversion output according to a control signal for making Vdc coincide with Vdc*.
대표청구항▼
1. A gas turbine system including: first power conversion means for converting an AC voltage of a power system to a DC voltage; second power conversion means for converting the DC voltage output from said first power conversion means into an AC voltage; a generator connected to an AC output side of
1. A gas turbine system including: first power conversion means for converting an AC voltage of a power system to a DC voltage; second power conversion means for converting the DC voltage output from said first power conversion means into an AC voltage; a generator connected to an AC output side of said second power conversion means and driven and rotated by a gas turbine; and turbine control means for outputting a revolution speed command value depending upon a fuel flow rate of said gas turbine, said gas turbine system comprising:revolution speed detection means for detecting a revolution speed of said generator;DC voltage detection means for detecting a voltage of a DC side of said first power conversion means;DC voltage command value generation means for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and the revolution speed command value output by said turbine control means;DC voltage command value selection means for selecting either a preset DC voltage command value or the DC voltage command value generated by said DC voltage command value generation means in accordance with the revolution speed detected by said DC voltage detection means; andfirst control means for controlling a conversion output of said first power conversion means in accordance with a control signal for making the DC voltage detected by said DC voltage detection means coincide with the DC voltage command value selected by said DC voltage command value selection means. 2. The gas turbine system according to claim 1, comprising:DC current command value generation means for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and the revolution speed command value output by said turbine control means;running command selection means for selecting either a PWM running command or a diode running command in accordance with the revolution speed detected by said revolution speed detection means; andsecond control means for controlling a conversion output of said second power conversion means in accordance with the DC voltage command value and the running command selected by said running command selection means. 3. The gas turbine system according to claim 2, whereinsaid running command selection means selects diode rectification running when the detected revolution speed is at least a revolution speed at which such a DC voltage that control on the power system is possible is obtained, andsaid running command selection means selects PWM running when the detected revolution speed is less than the revolution speed at which such a DC voltage that control on the power system is possible is obtained. 4. A power conversion apparatus including: first power conversion means for converting an AC voltage of a power system to a DC voltage; and second power conversion means for converting the DC voltage output from said first power conversion means into an AC voltage, a generator driven and rotated by a gas turbine being connected to an AC output side of said second power conversion means,said power conversion apparatus comprising:revolution speed detection means for detecting a revolution speed of said generator;DC voltage detection means for detecting a voltage of a DC side of said first power conversion means;DC voltage command value generation means for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and a revolution speed command value depending upon a fuel flow rate of said gas turbine;DC voltage command value selection means for selecting either a preset DC voltage command value or the DC voltage command value generated by said DC voltage command value generation means in accordance with the revolution speed detected by said DC voltage detection means; andfirst control m eans for controlling a conversion output of said first power conversion means in accordance with a control signal for making the DC voltage detected by said DC voltage detection means coincide with the DC voltage command value selected by said DC voltage command value selection means. 5. The power conversion apparatus according to claim 4, comprising:DC current command value generation means for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and the revolution speed command value depending upon the fuel flow rate of said gas turbine;running command selection means for selecting either a PWM running command or a diode running command in accordance with the revolution speed detected by said revolution speed detection means; andsecond control means for controlling a conversion output of said second power conversion means in accordance with the DC voltage command value and the running command selected by said running command selection means. 6. The power conversion apparatus according to claim 5, whereinsaid running command selection means selects diode rectification running when the revolution speed detected by said revolution speed detection means is at least a revolution speed at which such a DC voltage that control on the power system is possible is obtained, andsaid running command selection means selects PWM running when the revolution speed detected by said revolution speed detection means is less than the revolution speed at which such a DC voltage that control on the power system is possible is obtained. 7. A control method of a gas turbine system including: first power conversion means for converting an AC voltage of a power system to a DC voltage; second power conversion means for converting the DC voltage output from said first power conversion means into an AC voltage; a generator connected to an AC output side of said second power conversion means and driven and rotated by a gas turbine; and turbine control means for outputting a revolution speed command value depending upon a fuel flow rate of said gas turbine, said gas turbine system control method comprising the steps of:providing revolution speed detection means for detecting a revolution speed of said generator, and DC voltage detection means for detecting a voltage of a DC side of said first power conversion means;generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and the revolution speed command value output by said turbine control means;selecting either a preset DC voltage command value or the generated DC voltage command value in accordance with the revolution speed detected by said DC voltage detection means; andcontrolling a conversion output of said first power conversion means in accordance with a control signal for making the DC voltage detected by said DC voltage detection means coincide with the selected DC voltage command value. 8. The gas turbine system control method according to claim 7, comprising the steps of:generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detection means and the revolution speed command value output by said turbine control means;selecting either a PWM running command or a diode running command in accordance with the revolution speed detected by said revolution speed detection means; andcontrolling a conversion output of said second power conversion means in accordance with the DC voltage command value and the selected running command. 9. The gas turbine system control method according to claim 8, whereindiode rectification running is selected when the detected revolution speed is at least a revolution speed at which such a DC voltage that control on the power system is possible is obtained, andPWM running is selected when the detected revolution sp eed is less than the revolution speed at which such a DC voltage that control on the power system is possible is obtained. 10. The gas turbine system control method according to claim 8, whereinat time of the PWM running, the DC voltage of said first power conversion means is controlled to become a low value in a range of the DC voltage at which control is possible, andswitchover to the diode rectification running is conducted in a region where the revolution speed of said generator is high. 11. The gas turbine system control method according to claim 9, whereinat time of the PWM running, the DC voltage of said first power conversion means is controlled to become a low value in a range of the DC voltage at which control is possible, andswitchover to the diode rectification running is conducted in a region where the revolution speed of said generator is high. 12. A gas turbine system including: first power converter for converting an AC voltage of a power system to a DC voltage; second power converter for converting the DC voltage output from said first power converter into an AC voltage; a generator connected to an AC output side of said second power converter and driven and rotated by a gas turbine; and turbine controller for outputting a revolution speed command value depending upon a fuel flow rate of said gas turbine, said gas turbine system comprising:revolution speed detector for detecting a revolution speed of said generator;DC voltage detector for detecting a voltage of a DC side of said first power convertor;DC voltage command value generator for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detector and the revolution speed command value output by said turbine controller;DC voltage command value selector for selecting either a preset DC voltage command value or the DC voltage command value generated by said DC voltage command value generator in accordance with the revolution speed detected by said DC voltage detector; andfirst controller for controlling a conversion output of said first power converter in accordance with a control signal for making the DC voltage detected by said DC voltage detector coincide with the DC voltage command value selected by said DC voltage command value selector. 13. The gas turbine system according to claim 12, comprising:DC current command value generating unit for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detector and the revolution speed command value output by said turbine controller;running command selection means for selecting either a PWM running command or a diode running command in accordance with the revolution speed detected by said revolution speed detector; andsecond controller for controlling a conversion output of said second power converter in accordance with the DC voltage command value and the running command selected by said running command selector. 14. The gas turbine system according to claim 13, whereinsaid running command selector selects diode rectification running when the detected revolution speed is at least a revolution speed at which such a DC voltage that control on the power system is possible is obtained, andsaid running command selector selects PWM running when the detected revolution speed is less than the revolution speed at which such a DC voltage that control on the power system is possible is obtained. 15. A power conversion apparatus including: first power converter for converting an AC voltage of a power system to a DC voltage; and second power converter for converting the DC voltage output from said first power converter into an AC voltage, a generator driven and rotated by a gas turbine being connected to an AC output side of said second power converter,said power conversion apparatus comprising:revolution speed detector for detecting a revolution speed of said generato r;DC voltage detector for detecting a voltage of a DC side of said first power converter;DC voltage command value generating unit for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detecter and a revolution speed command value depending upon a fuel flow rate of said gas turbine;DC voltage command value selector for selecting either a preset DC voltage command value or the DC voltage command value generated by said DC voltage command value generating unit in accordance with the revolution speed detected by said DC voltage detector; andfirst controller for controlling a conversion output of said first power convertor in accordance with a control signal for making the DC voltage detected by said DC voltage detector coincide with the DC voltage command value selected by said DC voltage command value selector. 16. The power conversion apparatus according to claim 15, comprising:DC current command value generating unit for generating a DC voltage command value in accordance with a difference between the revolution speed detected by said revolution speed detector and the revolution speed command value depending upon the fuel flow rate of said gas turbine;running command selector for selecting either a PWM running command or a diode running command in accordance with the revolution speed detected by said revolution speed detector; andsecond controller for controlling a conversion output of said second power converter in accordance with the DC voltage command value and the running command selected by said running command selector. 17. The power conversion apparatus according to claim 16, whereinsaid running command selector selects diode rectification running when the revolution speed detected by said revolution speed detector is at least a revolution speed at which such a DC voltage that control on the power system is possible is obtained, andsaid running command selector selects PWM running when the revolution speed detected by said revolution speed detector is less than the revolution speed at which such a DC voltage that control on the power system is possible is obtained.
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