[특허]2-shaft gas turbine, and the control method of opening degree of inlet guide vane of the gas turbine

MITSUBISHI HITACHI POWER SYSTEMS, LTD.

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특허 상세정보

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2-shaft gas turbine, and the control method of opening degree of inlet guide vane of the gas turbine

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02C-009/20 F02C-009/28 F02C-009/54 F02C-003/10 F02C-009/22
출원번호	US-0417743 (2017-01-27)
등록번호	US-10247109 (2019-04-02)
우선권정보	JP-2016-064976 (2016-03-29)
발명자 / 주소	Myoren, Chihiro Nanataki, Kenji Takahashi, Yasuo Kawamura, Kota
출원인 / 주소	MITSUBISHI HITACHI POWER SYSTEMS, LTD.
대리인 / 주소	Volpe and Koenig, P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 11

초록
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A 2-shaft gas turbine has a controller which controls the opening degree of an air inlet guide vane to adjust the inlet mass flow rate to a compressor. The air inlet guide vane control unit includes a first control unit that adjusts the opening degree of the inlet guide vane to keep the speed of a high pressure turbine shaft constant; a control status confirmation unit that confirms the actual speed and the opening degree of the inlet guide vane; and a low ambient temperature correction unit that reduces the actual speed in a case where the actual speed is equal to or greater than a predetermined threshold value, the opening degree of the inlet guide vane is equal to or greater than a predetermined threshold value, and the ambient temperature is equal to or less than a predetermined threshold value.

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1. A 2-shaft gas turbine comprising: a gas generator that is configured of a compressor that has inlet guide vanes on an air intake side and compresses inflow air, a combustor that generates combustion gas by burning air that is compressed by the compressor and fuel, and a high pressure turbine driven by the combustion gas generated by the combustor; anda low pressure turbine that is driven by gas discharged from the high pressure turbine,wherein a high pressure turbine shaft that connects the compressor to the high pressure turbine, and a low pressure turbine shaft that connects the low pressure turbine to a load are separated shafts, and an inflow air amount to the compressor is adjusted by controlling an opening degree of the inlet guide vane, andwherein as a unit that controls the opening degree of the inlet guide vane, a first control unit that adjusts the opening degree of the inlet guide vane so as to keep an actual speed of the high pressure turbine shaft constant during a high speed rotation of the high pressure turbine shaft; a control status confirmation unit that confirms the actual speed that is kept constant by the first control unit and the opening degree of the inlet guide vane; and a low atmospheric temperature correction unit that reduces the actual speed that is kept constant by the first control unit upon a condition that the actual speed that is kept constant by the first control unit input into the control status confirmation unit is equal to or greater than a predetermined threshold value NO, the opening degree of the inlet guide vane is equal to or greater than a predetermined threshold value □0, and an atmospheric temperature is equal to or less than a predetermined threshold value Ta0 are at least included,wherein the 2-shaft gas turbine is configured of an inlet guide vane control device by which the opening degree of the inlet guide vane is capable of being changed; a fuel control valve that controls a fuel supply amount from a fuel supply source to the combustor; a fuel control unit that controls the fuel control valve using a rotational speed that is detected by a rotational speed detector disposed in the low pressure turbine shaft and operation load data that is obtained from a load; and an inlet guide vane opening degree control unit that is connected to the inlet guide vane control device and controls the opening degree of the inlet guide vane, and includes a gas generator control device that controls an operational status of the 2-shaft gas turbine, andwherein upon a condition that the operational status is determined to be corrected by the control status confirmation unit, in the low atmospheric temperature correction unit, a correction coefficient □ is multiplied to an actual speed N of the gas generator and the opening degree of the inlet guide vane is controlled by sending a signal to the inlet guide vane control device so that the rotational speed is reduced to N′. 2. The 2-shaft gas turbine according to claim 1, wherein the inlet guide vane opening degree control unit includes the first control unit; the control status confirmation unit; the low atmospheric temperature correction unit; a second control unit that calculates a corrected speed using the rotational speed of the gas generator obtained by the rotational speed detector disposed in the high pressure turbine shaft and the atmospheric temperature, and adjusts the opening degree of the inlet guide vane such that a relationship between the corrected speed and the opening degree of the inlet guide vane is uniquely determined irrespective of the atmospheric temperature; an operational status determination unit that determines the operational status of the gas generator in a second operational status configured of actuation and stop status, and a low load operation status, and a first operation status configured of a high load operational status other than the second operational status; and a control selection unit that selects whether any one of the first control unit and the second control unit is used from a determination result of the operational status determination unit, andwherein after the determination of the operational status by the operational status determination unit and the control selection by the control selection unit are completed, the opening degree of the inlet guide vane is controlled through the control status confirmation unit and the low atmospheric temperature correction unit. 3. The 2-shaft gas turbine according to claim 1, wherein the predetermined threshold value N0 of the actual speed kept constant by the first control unit is a rotational speed Ndes during a rated operation defined at the time of design and the predetermined threshold value □0 of the opening degree of the inlet guide vane is an opening degree □des during the rated operation defined at the time of design. 4. The 2-shaft gas turbine according to claim 1, wherein the predetermined threshold value NO of the actual speed kept constant by the first control unit and the predetermined threshold value □0 of the opening degree of the inlet guide vane are less than the rotational speed Ndes during the rated operation and the opening degree □des during the rated operation defined at the time of design. 5. The 2-shaft gas turbine according to claim 2, further comprising: a third control unit that adjusts the opening degree of the inlet guide vane to be kept constant irrespective of the rotational speed of the high pressure turbine shaft upon transition from the control in the second control unit to the control in the first control unit. 6. The 2-shaft gas turbine according to claim 2, wherein the inlet guide vane opening degree control unit includes a low atmospheric temperature additional correction unit that increases the opening degree of the inlet guide vane upon a condition that the atmospheric temperature is equal to or less than the predetermined threshold value Ta0. 7. A control method of an inlet guide vane of a 2-shaft gas turbine including a gas generator that is configured of a compressor that has inlet guide vanes on an air intake side and compresses inflow air, a combustor that generates combustion gas by burning air that is compressed by the compressor and fuel, and a high pressure turbine driven by the combustion gas generated by the combustor; and a low pressure turbine that is driven by gas discharged from the high pressure turbine, in which a high pressure turbine shaft that connects the compressor to the high pressure turbine, and a low pressure turbine shaft that connects the low pressure turbine to a load are separated shafts, and an inflow air amount to the compressor is adjusted by controlling an opening degree of the inlet guide vane, wherein, in the control of the opening degree of the inlet guide vane,as a unit that controls the opening degree of the inlet guide vane, a first control unit; a control status confirmation unit, and a low atmospheric temperature correction unit are included, andin the first control unit, the opening degree of the inlet guide vane is adjusted so as to keep an actual speed of the high pressure turbine shaft constant during a high speed rotation of the high pressure turbine shaft; in the control status confirmation unit, the actual speed that is kept constant by the first control unit and the opening degree of the inlet guide vane are confirmed; and in the low atmospheric temperature correction unit, the opening degree of the inlet guide vane is controlled so as to reduce the actual speed that is kept constant by the first control unit upon a condition that the actual speed that is kept constant by the first control unit input into the control status confirmation unit is equal to or greater than a predetermined threshold value N0, the opening degree of the inlet guide vane is equal to or greater than a predetermined threshold value □0, and an atmospheric temperature is equal to or less than a predetermined threshold value Ta0,wherein the opening degree of the inlet guide vane is changed by the inlet guide vane control device; a fuel supply amount from a fuel supply source to the combustor is controlled by a fuel control valve; an operational status of the 2-shaft gas turbine is controlled by a gas generator control device configured of a fuel control unit that controls the fuel control valve using a rotational speed that is detected by a rotational speed detector disposed in the low pressure turbine shaft and operation load data that is obtained from the load, and an inlet guide vane opening degree control unit that is connected to the inlet guide vane control device and controls the opening degree of the inlet guide vane; a corrected speed is calculated by using the rotational speed of the gas generator obtained by the rotational speed detector disposed in the high pressure turbine shaft and the atmospheric temperature; the opening degree of the inlet guide vane is adjusted in a second control unit such that a relationship between the corrected speed and the opening degree of the inlet guide vane is uniquely determined irrespective of the atmospheric temperature; the operational status of the gas generator is determined by an operational status determination unit in a second operational status configured of actuation, stop status, and a low load operational status, and a first operational status configured of a high load operational status other than the second operational status; and whether any one of the first control unit and the second control unit is used is selected by a control selection unit from a determination result of the operational status determination unit,wherein after the determination of the operational status by the operational status determination unit and the control selection by the control selection unit are completed, the opening degree of the inlet guide vane is controlled through the control status confirmation unit and the low atmospheric temperature correction unit,wherein upon a condition that the operational status is determined to be corrected by the control status confirmation unit, in the low atmospheric temperature correction unit, a correction coefficient □ is multiplied to an actual speed N of the gas generator and the opening degree of the inlet guide vane is controlled by sending a signal to the inlet guide vane control device so that the rotational speed is reduced to N′. 8. The control method of an inlet guide vane of a 2-shaft gas turbine according to claim 7, wherein the predetermined threshold value NO of the actual speed kept constant by the first control unit is a rotational speed Ndes during a rated operation defined at the time of design and the predetermined threshold value □0 of the opening degree of the inlet guide vane is an opening degree □des during the rated operation defined at the time of design. 9. The control method of an inlet guide vane of a 2-shaft gas turbine according to claim 7, wherein the predetermined threshold value NO of the actual speed kept constant by the first control unit and the predetermined threshold value □0 of the opening degree of the inlet guide vane are less than the rotational speed Ndes during the rated operation and the opening degree □des during the rated operation defined at the time of design. 10. The control method of an inlet guide vane of a 2-shaft gas turbine according to claim 7, wherein the predetermined threshold value NO of the actual speed kept constant by the first control unit and the predetermined threshold value □0 of the opening degree of the inlet guide vane are less than the rotational speed Ndes during the rated operation and the opening degree □des during the rated operation defined at the time of design. 11. The control method of an inlet guide vane of a 2-shaft gas turbine according to claim 7, wherein the opening degree of the inlet guide vane is increased by a low atmospheric temperature additional correction unit upon a condition that the atmospheric temperature is equal to or less than the predetermined threshold value Ta0.

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2-shaft gas turbine, and the control method of opening degree of inlet guide vane of the gas turbine

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