WO2001088355A1 - Method for remote monitoring of gas turbine - Google Patents
Method for remote monitoring of gas turbine Download PDFInfo
- Publication number
- WO2001088355A1 WO2001088355A1 PCT/JP2001/004161 JP0104161W WO0188355A1 WO 2001088355 A1 WO2001088355 A1 WO 2001088355A1 JP 0104161 W JP0104161 W JP 0104161W WO 0188355 A1 WO0188355 A1 WO 0188355A1
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- communication mode
- plant
- combustion
- turbine
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/46—Emergency fuel control
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
- G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
- G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
- G01H1/006—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
- G05B23/0286—Modifications to the monitored process, e.g. stopping operation or adapting control
- G05B23/0291—Switching into safety or degraded mode, e.g. protection and supervision after failure
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/01—Protocols
- H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L9/00—Cryptographic mechanisms or cryptographic arrangements for secret or secure communications; Network security protocols
- H04L9/40—Network security protocols
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/301—Pressure
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/30—Control parameters, e.g. input parameters
- F05D2270/303—Temperature
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L69/00—Network arrangements, protocols or services independent of the application payload and not provided for in the other groups of this subclass
- H04L69/30—Definitions, standards or architectural aspects of layered protocol stacks
- H04L69/32—Architecture of open systems interconnection [OSI] 7-layer type protocol stacks, e.g. the interfaces between the data link level and the physical level
- H04L69/322—Intralayer communication protocols among peer entities or protocol data unit [PDU] definitions
- H04L69/329—Intralayer communication protocols among peer entities or protocol data unit [PDU] definitions in the application layer [OSI layer 7]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
- Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
- Y04S40/00—Systems for electrical power generation, transmission, distribution or end-user application management characterised by the use of communication or information technologies, or communication or information technology specific aspects supporting them
- Y04S40/18—Network protocols supporting networked applications, e.g. including control of end-device applications over a network
Definitions
- the present invention relates to a remote monitoring method for a gas turbine installed in a power plant or the like, and in particular, to prevent damage to components caused by resonance with combustion vibration of a turbine.
- compressed air and gas fuel are supplied from a compressor to a combustor, and the pin is rotated using the high-temperature combustion gas generated by combustion in the combustor.
- a rotor blade for compressor and a rotor blade for turbine are provided around the rotation axis of the evening bin, and the rotor blade for turbine rotates by high-temperature combustion gas supplied from the combustor.
- a fuel nozzle for supplying main fuel and a pier port nozzle for supplying pit fuel are provided in the combustor inner cylinder, and air and fuel discharged from the compressor are provided. The fuel is mixed and burned, and the combustion gas flows out of the combustor transition piece to the turbine.
- diluted fuel gas can be used. It is expected that the use of the diluted fuel gas will cause the combustion in the combustor to become unstable, causing a problem that the combustion gas fluid pulsates and the combustion oscillation becomes severe. Similarly, it is necessary to raise the operating temperature to increase efficiency in consideration of energy saving. In this case, it is expected that unstable combustion of the combustor will be increased by burning more fuel.
- Combustion oscillations can be suppressed to some extent by adjusting, for example, the fuel / air distribution ratio (fuel / air ratio), pilot ratio, and bypass valve opening. Therefore, in the initial operation when the gas turbine is installed, it is possible to adjust to such a state that the combustion vibration is suppressed.
- gas turbines that have reduced efficiency and increased operating temperature in recent years After a while, the combustion vibration resumes due to factors such as equipment deterioration, and in the worst case, it resonates with the natural frequency of parts such as bolts and nuts of the combustor and turbine, causing damage to the parts could lead to
- a plant such as a power plant equipped with a gas turbine can be used to monitor the operating parameters of the gas bin and the operating status of the gas bin using a communication line at a remote monitoring station. . Therefore, it is conceivable to monitor the state of the above-mentioned combustion oscillation from a remote monitoring center so that the combustion oscillation does not exceed a certain level.
- a large amount of vibration with a higher frequency is transmitted via the communication line compared to the operating state of the bin. , Must be monitored.
- an object of the present invention is to provide a remote monitoring method capable of monitoring the combustion oscillation state of a combustor of a turbine from a remote monitoring center, and a system using the same.
- Another object of the present invention is to provide a remote monitoring method and a system using the same, which can prevent damage to components due to resonance with combustion vibration of a turbine. Is to provide.
- a further object of the present invention is to provide a remote monitoring method capable of monitoring a predetermined condition causing a turbine trip from a remote monitoring device.
- a first aspect of the present invention relates to a method for burning a combustor in a power plant or the like in which a bin is set from a remote monitoring center to a bin. The vibration state is monitored.
- a low-speed communication mode using an in-net connection or the like, and a line switching method using a telephone line such as ISDN are used as the data transmission mode.
- a line switching method using a telephone line such as ISDN are used as the data transmission mode.
- high-speed communication mode is used as the data transmission mode.
- the Internet is a relatively low-cost form of communication, it is not suitable for transmitting large amounts of data with high accuracy because of its low speed.
- the circuit switching method using ISDN is Since a data communication is established by establishing a communication line between the monitoring center and the monitoring center, a large amount of data can be transmitted with high speed, high accuracy, and high security, but the communication cost is high.
- the combustion vibration data of the combustor is divided into first data acquired in real time and second data composed of representative values within a predetermined period obtained from the first data.
- the second data is transmitted using a low-speed communication mode such as the Internet and monitored by the monitoring center, and if an abnormal state is foreseen as a result of monitoring using the second data,
- the first data is transmitted using a high-speed communication mode such as ISDN, and more detailed combustion vibration data is monitored at the monitoring terminal. If a critical state is foreseen, etc., a command is issued to the site to switch to low-load operation as necessary.
- a combustion vibration data of the combustor is obtained by a frequency spectrum data (first data) of a vibration level obtained by Fourier transform from a vibration waveform sampled in real time; Then, the peak value data (second data) within the predetermined period of the resonance frequency band obtained is divided and transmitted during normal use, and the peak oscillation data is transmitted using the in-net network. In the event of an error, it transmits frequency spectrum data using ISDN. This allows the remote monitoring center to predict the turbine abnormal state by monitoring the peak value data at normal times, and to monitor the frequency spectrum data received by ISDN if there is any indication of an abnormal state. In the evening, immediately before the combustion vibration becomes so violent that the turbine parts are damaged, a command to switch to low-load operation is issued to the site. Try to prevent that from happening.
- a second aspect of the present invention is the first aspect, wherein a sign detection computer for detecting a sign of a critical state is installed in a plant, wherein the peak value data and the turbine It is checked whether or not the combination with the operating parameters of the vehicle is similar to the reference data when a sign of criticality was detected in the past, and an alarm is output in the brand when the sign is detected.
- FIG. 1 is a configuration diagram of an example of a gas turbine according to the present embodiment.
- FIG. 2 is a diagram showing a configuration example of the combustor 5.
- FIG. 3 is a diagram for explaining a remote monitoring method according to the present embodiment.
- FIG. 4 is a diagram showing an example of a frequency spectrum of combustion oscillation.
- FIG. 5 is a diagram showing an example of the peak value of the combustion oscillation level.
- FIG. 6 is a diagram showing an example of a combustion vibration monitoring screen provided in the plant.
- FIG. 7 is a diagram showing an example of a normal monitoring screen in the monitoring center.
- FIG. 8 is a view for explaining the flow of the evening in the first embodiment.
- FIG. 9 is an operation flowchart of the combustion vibration analysis device and the central control device.
- FIG. 10 is a diagram for explaining the flow of the data overnight in the second embodiment.
- FIG. 11 is an operation flowchart of the sign detection device 38.
- FIG. 1 is a configuration diagram of an example of a gas turbine according to the present embodiment.
- the rotating part R / B 3 is supported via a bearing, and the air compressed by the compressor 4 on the left and the fuel gas supplied to the combustor 5 in the center are mixed and burned.
- the combustion gas burned in the vessel 5 and the high temperature expanded combustion gas is supplied to the right turbine, and the thrust of the turbine rotates the turbine blade. Therefore, a plurality of combustors 5 are provided around the road.
- the rotation of the evening bin is used, for example, as power for a generator.
- FIG. 2 is a diagram showing a configuration example of the combustor 5.
- the combustor 5 includes a main nozzle and a pilot port nozzle 10 to which a main fuel premixed with air and a non-premixed pilot fuel are supplied, respectively, and a compressed air mixed with the main fuel. It has a compressed air discharge port 14 supplied from a compressor, a combustor inner tube 11 in which a flame is generated by combustion, a combustor outer tube 12 for sending combustion gas to a bin, and a bypass valve 13.
- combustion vibration has a vibration in a frequency band including the natural frequency of the combustor part, and if the vibration level in the frequency band of the natural frequency exceeds a certain value, the part is expected to be destroyed. Therefore, it is desirable to perform control such as switching to low-load operation before reaching such a combustion oscillation level.
- gas turbines aiming for lower NOx and higher efficiency in the future need to constantly monitor this combustion vibration and control it so that it does not reach a critical state.
- gas turbines may generate shaft vibration as they rotate at high speed. However, it is necessary to constantly monitor such shaft vibration and control it so that it does not exceed the critical value.
- FIG. 3 is a diagram for explaining a remote monitoring method according to the present embodiment.
- FIG. 3 shows a remote plant 20 in which a gas turbine 21 is installed, and a monitoring center 50 connected to the plant via communication lines 16, 18, and 19.
- Various types of computers are connected to the plant 20 via a dedicated network 22.
- a central control device 24 that controls the entire plant and operating parameters such as temperature, pressure, vibration, various control signals, and turbine output (rotation speed) of each part of the gas turbine 21 are acquired. It has a turbine operation control device 26 for performing predetermined operation control.
- a plant operator 48 is stationed in the central operation room where the turbine operation control device 26 and the central control device 24 are installed, and controls the operation of the gas bin.
- the plant 20 has a combustion vibration analyzer 28 that acquires the sensor value S28 from the pressure sensor installed in the combustor of the gas bin 21 and analyzes the combustion vibration, and a combustion vibration monitor for monitoring the combustion vibration.
- a combustion vibration monitoring screen 30 for displaying data is provided.
- a shaft vibration analysis device 32 that obtains a shaft vibration value S32 associated with the rotation of the rotor and analyzes the shaft vibration is provided.
- a data management device 34 for managing the operating parameters obtained by the turbine operation control device 26, the vibration data obtained by the combustion vibration analysis device 28 and the shaft vibration analysis device 32, and a data file 36.
- the sign detection device 38 is a device that automatically detects a sign of a critical state of combustion vibration from combustion vibration data acquired by the combustion vibration analysis device 28, as described later.
- the combustion vibration analyzer 28 acquires a sensor value S28 from a pressure sensor attached to the combustor of the gas turbine 21 in real time.
- the sensor value is A / D converted after noise is removed by filtering.
- the combustion vibration data every two seconds is subjected to Fourier transform to obtain a frequency spectrum of the vibration level.
- peak value data within a predetermined period of time for the vibration level with respect to the natural frequency of the combustor and surrounding components obtained from the frequency spectrum is also obtained.
- the frequency spectrum and the peak value data of the combustion vibration are displayed on the combustion vibration monitoring screen 30.
- FIG. 4 is a diagram showing an example of a combustion oscillation frequency spectrum.
- Horizontal axis Represents the frequency f, and the vertical axis represents the vibration level.
- four natural frequencies,:? 2, 3, and 4 are included in the frequency band.
- the combustion oscillation data shown in Fig. 4 is data obtained in real time, changes at high speed over time, and has a large amount of data.
- FIG. 5 is a diagram showing an example of a peak value of a combustion oscillation level.
- the horizontal axis indicates the sensor provided in the combustor, and the vertical axis indicates the peak value of the vibration level within a predetermined period.
- the example of FIG. 5 shows, for example, a peak value for one minute in a band of natural frequency; l, and indicates that the sensor 3 exceeding the threshold level Vth has a precursor to reach a critical state.
- This peak value is a data that changes every 10 seconds, for example, and has a smaller data amount than the frequency spectrum shown in FIG.
- FIG. 6 is a diagram showing an example of a combustion vibration monitoring screen provided in the plant.
- the example of FIG. 6 shows a case in which the gas turbine has two units. It has areas 72 and 74 for displaying the operating parameters of units A and B, frequency spectrum display areas 76 and 78 for units A and B, and peak value display areas 80 and 82 for units ⁇ and ⁇ . .
- the operating parameters are data used for gas bin operation control
- the frequency spectrum is real-time combustion vibration data
- the peak value is representative within a predetermined period. It is combustion vibration data.
- the operation operator 48 in the plant has a skilled technique, it is possible to monitor the combustion vibration state in addition to the turbine operation control by monitoring this monitoring screen.
- a skilled technician can monitor the monitoring screen when setting up a new plant and set operation control setting values and the like so that the combustion vibration level becomes the lowest level.
- highly skilled technicians must be stationed in order to monitor this monitoring screen and predict that combustion vibration will reach a critical state.
- the monitoring remote from the plant 20 is performed.
- the combustion oscillation state can be monitored. Therefore, the monitoring sensor 50 receives the combustion vibration data via the communication line.
- a communication line it is unsuitable for high-speed and large-volume data transmission, but the communication cost is relatively low, such as Internet connection 16.
- a high-speed communication mode capable of transmitting a large amount of data with high accuracy, for example, a telephone line 18 such as ISDN is also used.
- the IN-UNI-NET 16 is a communication mode in which the IN-UNI-NET server is always connected and performs packet communication of data.
- ISDN 18 is a circuit-switched system that establishes a communication line between a transmitting side and a receiving side during communication. If overnight communication via ISDN is not available as a high-speed communication mode, satellite communication 17 such as INMARSAT (International Mobile Satellite Communications Organization) can also be used.
- INMARSAT International Mobile Satellite Communications Organization
- the peak value data of the combustion vibration data is transmitted to the constant monitoring sensor 50 via the Internet 16 together with the operating parameters of the evening bin.
- an in-net server 40 a file 42 in which combustion vibration data (peak value data) to be transmitted and operating parameters are stored, and a relay device (a 44) are provided.
- a server 54 which is a similar in-night server and stores received data, and a relay device (router) 52 are provided.
- the server 54 of the monitoring center 50 accesses the server 40 in the remote plant to receive the operating parameters and the combustion vibration data (peak value data). .
- the operating parameters and the combustion vibration data (peak value data) that are constantly acquired by the in-net network are displayed on the normal monitoring screen display device 58 in the monitoring center.
- An example of this display screen is shown in FIG.
- the example of FIG. 7 shows the unit parameter common display 70, the operating parameter overnight displays 72 and 74 of the units ⁇ and ⁇ on the combustion vibration monitoring screen 30 in the plant of FIG. 6, and the unit 6.
- ⁇ Peak value display 80, 82 are displayed. These displays are performed on the basis of the operating parameter overnight data constantly received via the internet 16 and the representative value data within a predetermined time in the combustion vibration data.
- the monitoring center 50 receives the above-mentioned data from a plurality of remote brands 20 via the Internet, and displays a screen as shown in FIG. indicate. Then, the combustion vibration of each plant is monitored by a skilled engineer 64 resident in the monitoring center 50. Since the peak value display shows the peak value of the natural frequency band within a predetermined time, the combustion oscillation state cannot be monitored in detail like a real-time frequency spectrum. According to the skilled technician 64, it is sufficient to detect a sign of an abnormal state. Then, when the skilled engineer 64 detects such a sign, the ISDN line 18 is connected to the plant 20 by the relay device 53, and real-time frequency spectrum data is acquired from the plant 20. The data of the frequency spectrum is displayed on the analysis screen display device 60, and the skilled engineer 64 monitors the combustion vibration at the same level as the local plant.
- the power of the gas bin is reduced to the local plant operator by telephone or fax, for example, via telephone line 19. To send instructions. Then, when the combustion oscillation returns to the normal state, the reception of the real-time frequency spectrum is stopped by the ISDN 18, and the reception is returned to only the reception of the peak value data by the infinity net 16.
- the monitoring center 50 receives the peak value data of the combustion vibration, which has a relatively small amount of data, via the Internet 16 which is low speed but has low communication cost in the normal state, and sends the Monitor. If a sign of an abnormal condition is detected, a communication frequency is high, but a large amount of data can be transmitted at high speed. Let the skilled technician 64 monitor in detail.
- FIG. 8 is a diagram showing a data flow in the first embodiment.
- the pressure values from the pressure sensors 29 provided on the inner and outer cylinders of the combustors of the gas burner bin 21 are removed at the filter 86,
- the digital value is converted by the A / D converter 88. Since pressure fluctuations caused by combustion oscillation fluctuate at high frequencies, sampling at high frequencies is necessary accordingly.
- the sensor pressure value S28 converted into digital data is processed into frequency spectrum data and peak value data in the combustion vibration analyzer 28, displayed on the combustion vibration monitor screen 30, and burned by the central controller 24. Vibration data is solved Is analyzed.
- FIG. 9 is an operation flowchart of the combustion vibration analysis device and the central control device.
- the operation in FIG. 8 is shown in FIG.
- an A / D conversion data sampled at a high frequency for the pressure sensor value is input (S100).
- the A / D converted data is subjected to a free-transform (S102).
- the target data of the Fourier transform is, for example, a real-time pressure value every two seconds.
- the Fourier transform can be performed, for example, separately for a high frequency band and a low frequency band. This makes it possible to generate a spectrum having a vibration level in a wide frequency band.
- a peak value of the vibration level is calculated for each band of the natural frequency of the combustor component in the frequency spectrum (S104). Therefore, this peak value is real-time (every 2 seconds) data.
- the alarm setting value (threshold value Vth) set for each band is compared with the calculated peak value (S106). If the peak value exceeds the alarm setting value, an alarm notification is sent to the plant and the monitoring center (S110). ).
- the alarm notification to the monitoring center can be made by communication using the Inuichi Net.
- the central control unit 24 holds the peak value for each band, for example, for a period of one minute (S116), and stores the peak value in the file device 42 of the in-net server 40.
- the operating parameters obtained by the turbine operation control device 26 are also stored in the file device 42.
- the internet server 40 stores the peak value and the operating parameters stored in the file device 42, and the internet 16 Via the monitoring center 50 to the server 54.
- the transmission may be performed once a minute.
- the peak value data for a plurality of combustors can be sent multiple times within a one-minute cycle.
- the transmission mode is determined according to system optimization.
- the monitoring center 50 receives the peak data and the operating parameters via the Internet, and displays the normal monitoring screen display device 58 as shown in FIG. Display.
- This normal monitoring screen is constantly monitored by a skilled technician 64 in the monitoring center.
- the ISDN line 18 was connected to the plant as necessary, while monitoring the peak value display every minute for the combustion vibration of the combustor, and the real-time frequency spectrum data was monitored. Request.
- This case corresponds to, for example, a case where the skilled engineer 64 foresees a sign that the combustion oscillation becomes abnormal due to the deterioration of the peak value.
- the ISDN line 18 is connected to the plant, and requests real-time frequency spectrum data.
- the display as shown in FIG. 6 is performed on the analysis screen display device 60, and the engineer 64 can monitor the combustion vibration in more detail.
- step S112 the central control device 24 in the plant 20 is connected from the monitoring center 50 by the ISDN line 18, and when requested, the frequency spectrum data is transmitted. Is returned to the monitoring center 50 in real time (S120).
- the skilled technician 64 monitors the frequency spectrum of the combustion oscillation in real time, and detects a sign of a critical state, for example, through a telephone fax 62, for example. Contact operator 48 and instruct him to run gas tarpin to reduce load. Accordingly, it is possible to prevent the gas turbine 21 in the plant from being tripped due to the destruction of components in the combustor due to combustion vibration.
- FIG. 10 is a diagram for explaining a data flow in the second embodiment.
- FIG. 11 is an operation flowchart of the sign detection device 38.
- a technician in the monitoring center monitors the peak value of the combustion vibration, and if a sign of an abnormal state is foreseen, receives a frequency spectrum of the combustion vibration through the ISDN line. Perform more detailed monitoring.
- a sign detection device 38 is provided in the plant to detect a sign that combustion vibration reaches a critical state, and to issue an alarm instructing low-load operation in the plant. Or automatically causes the bin operation control device 26 to perform the output reduction operation.
- the monitoring center normally receives the operating parameters and the combustion oscillation peak value data via the in-net network 16 and receives an abnormal condition.
- the frequency spectrum of combustion oscillation is received in real time via the ISDN line.
- the predictive detection device 38 detects that the combination of the peak value of the combustion vibration and the operation parameter causes the combustion vibration to reach an abnormal state or a critical state. Check if a certain correlation has been reached with the evening, and if such a correlation is detected, report an alarm to guide the switch to low-load operation or automatically. Instruct turbine operation control device 26 to switch to low load operation.
- the alarm notification and the information for switching to the low-load operation are also transmitted to the monitoring center 50 via the in-network 16 or the ISDN line 18 if connected.
- FIG. 11 is an operation flowchart of the sign detection device 38.
- the sign detection device inputs the vibration level peak value for each band of the combustion vibration in the file device 36 of the data management device 34 (S130), and at the same time also inputs the operating parameters at that time (SL32).
- the peak value is the maximum value of the natural frequency obtained from the frequency spectrum acquired in real time for one minute for each band.
- the peak value when the combustion vibration reaches an abnormal state or a critical state differs depending on the operating parameters. Therefore, it is necessary to check the combination of the peak value and the operating parameters.
- the sign detection device 38 stores the combination data of the operating parameters and the peak value data when the combustion vibration of the combustor has reached an abnormal state or a critical state in the past. Then, a correlation function between the stored data, the input peak value, and the combination of the operating parameters is calculated (S134). If the calculated correlation coefficient is larger than the alarm value, that is, if it is detected that the combination of the past abnormal state or critical state is similar or approximate (S136), an alarm is displayed. Then, the operator 48 in the plant is instructed to switch to low load operation (S138, S140). Alternatively, the sign detection device 38 may automatically instruct the turbine operation control device 26 to switch to low-load operation.
- the combination of the current peak value data and the combustion parameter is used to determine the combination of the current peak value data and the combustion parameter at the time of the past abnormality. Check whether it is close to As a result, the probability of occurrence of a trip due to combustion vibration can be suppressed more than in the i-th embodiment.
- FIG. 10 shows a modification of the second embodiment.
- a data analysis device 56A is provided in the monitoring center 50, and the past data when the gas bin is in an abnormal state, a critical state, or a trip is recorded in the file device 56B. Then, the data pattern of the past accident is analyzed by the data analyzer 56A and used to prevent future accident recurrence. In particular, the operating parameters that led the monitoring center to switch to low-load operation, the peak value of combustion oscillation, and the frequency spectrum are recorded and analyzed. The data and analysis results thus accumulated are reflected in the set value data in the sign detection device of the plant 20.
- the present invention can also be applied to a turbine using a fuel other than gas.
- real-time data is transmitted over the ISDN line and the representative data within a predetermined period is transmitted over the Internet. This also enables remote monitoring with reduced communication costs.
- the present invention it is possible to effectively monitor the combustion vibration state of the evening bin installed in the plant from a remote monitoring center while suppressing the communication cost. Therefore, even in the evening bin with reduced NOx, it is possible to prevent the combustion vibration from reaching the critical state and tripping.
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Description
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Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP01930204A EP1283339B1 (en) | 2000-05-18 | 2001-05-18 | Method for remote monitoring of gas turbine |
CA002374971A CA2374971C (en) | 2000-05-18 | 2001-05-18 | Remote monitoring method for gas turbines |
DE60133638T DE60133638T2 (de) | 2000-05-18 | 2001-05-18 | Methode zur überwachung einer gasturbine |
US10/031,329 US6721631B2 (en) | 2000-05-18 | 2001-05-18 | Method for remote monitoring of gas turbine |
Applications Claiming Priority (2)
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JP2000-146887 | 2000-05-18 | ||
JP2000146887A JP3810615B2 (ja) | 2000-05-18 | 2000-05-18 | タービンの遠隔制御方法及びシステム |
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WO2001088355A1 true WO2001088355A1 (en) | 2001-11-22 |
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PCT/JP2001/004161 WO2001088355A1 (en) | 2000-05-18 | 2001-05-18 | Method for remote monitoring of gas turbine |
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US (1) | US6721631B2 (ja) |
EP (1) | EP1283339B1 (ja) |
JP (1) | JP3810615B2 (ja) |
CA (1) | CA2374971C (ja) |
DE (1) | DE60133638T2 (ja) |
WO (1) | WO2001088355A1 (ja) |
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EP1331448A2 (en) * | 2002-01-29 | 2003-07-30 | General Electric Company | Fuel control and tuning method for dry low NOx gas turbine engines |
EP1331448A3 (en) * | 2002-01-29 | 2004-10-27 | General Electric Company | Fuel control and tuning method for dry low NOx gas turbine engines |
US8665104B2 (en) | 2011-04-29 | 2014-03-04 | General Electric Company | Systems and methods for protecting rotating machines |
Also Published As
Publication number | Publication date |
---|---|
DE60133638T2 (de) | 2009-05-28 |
EP1283339A4 (en) | 2004-12-01 |
JP3810615B2 (ja) | 2006-08-16 |
EP1283339A1 (en) | 2003-02-12 |
DE60133638D1 (de) | 2008-05-29 |
CA2374971C (en) | 2005-08-30 |
JP2001329861A (ja) | 2001-11-30 |
EP1283339B1 (en) | 2008-04-16 |
US6721631B2 (en) | 2004-04-13 |
US20030014219A1 (en) | 2003-01-16 |
CA2374971A1 (en) | 2001-11-22 |
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