Gas turbine trip fault self-recovery system, method, storage medium and program

The self-recovery system automates the recovery of gas turbine trip faults by monitoring and controlling the operation of gas turbines and associated units, enhancing efficiency and safety while minimizing manual intervention and costs.

CN119102891APending Publication Date: 2024-12-10SHENHUA GUOHUA (BEIJING) GAS-FIRED COGENERATION CO LTD
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Patent Information

Application Number
CN202411177665.X
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-08-26
Publication Date
2024-12-10

AI Technical Summary

Technical Problem

Gas turbine tripping failures in two-on-one gas-steam combined cycle units due to equipment aging and complex operating environments lead to unstable operation and high operational risks, requiring labor-intensive manual intervention for fault recovery.

Method used

A self-recovery system and method that includes a state monitoring module to detect trip signals and a control module to automatically adjust the operation of gas turbines, waste heat boilers, and steam turbines, enabling automatic recovery and reducing manual intervention.

Benefits of technology

Enhances operational efficiency and safety while reducing maintenance costs by automating the recovery process, improving the stability and economic performance of gas turbine units.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention relates to a gas turbine tripping fault self-recovery system and method, a storage medium and a program, the program is applied to a two-driving-one operation unit, the two-driving-one operation unit comprises a first gas turbine, a second gas turbine, a first waste heat boiler, a second waste heat boiler and a steam turbine, and the system comprises a state monitoring module and a control module; the state monitoring module is used for monitoring tripping states of the first gas turbine and the second gas turbine, and sending a tripping signal to the control module when the first gas turbine and / or the second gas turbine sends the tripping signal; and the control module is used for controlling operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the tripping signal. The tripping state of the gas turbine in the two-driving-one operation unit can be monitored, operation of the unit is controlled based on the tripping signal sent by the gas turbine, tripping fault self-recovery of the gas turbine is achieved, the operation efficiency and safety of the unit are improved, and the operation and maintenance cost is reduced.
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Description

Technical Field

[0001] The present disclosure relates to the technical field of gas turbine power plants, and in particular to a gas turbine trip fault self-recovery system, method, storage medium and program. Background Art

[0002] In the prior art, during the actual operation of the two-on-one gas-steam combined cycle units in thermal power plants, due to factors such as equipment aging and complex operating environment, gas turbine tripping failures often occur, seriously affecting the stable operation and economic benefits of the units. Traditional fault recovery methods in thermal power plants mostly rely on manual intervention, requiring operators to manually adjust and control according to the fault phenomenon, which is not only time-consuming and labor-intensive, but also involves greater operational risks and uncertainties. With the deepening of the construction of intelligent thermal power plants, the requirements for the automation level and intelligent performance of the units are getting higher and higher. Realizing self-recovery of main and auxiliary system failures or equipment abnormalities of gas turbine units has become a technical problem that urgently needs to be solved. Summary of the invention

[0003] In order to overcome the problems existing in the related art, the present disclosure provides a gas turbine trip fault self-recovery system, method, storage medium and program.

[0004] According to a first aspect of an embodiment of the present disclosure, a gas turbine trip fault self-recovery system is provided, which is applied to a two-to-one operating unit, wherein the two-to-one operating unit includes a first gas turbine, a second gas turbine, a first waste heat boiler, a second waste heat boiler and a steam turbine, and the system includes: a state monitoring module and a control module;

[0005] The state monitoring module is used to monitor the trip state of the first gas turbine and the second gas turbine, and when the first gas turbine and / or the second gas turbine sends a trip signal, send the trip signal to the control module;

[0006] The control module is used to control the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the trip signal.

[0007] Optionally, the control module is further used for:

[0008] When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine is controlled to perform interlock tripping.

[0009] Optionally, the control module comprises: an override control unit;

[0010] The override control unit is used to control the operation states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine to switch to a pressure self-regulation state and a temperature self-regulation state based on the trip signal.

[0011] Optionally,

[0012] The control module is also used to control the operating state of the steam turbine to switch to a one-to-one pressure automatic adjustment state, where the one-to-one is an operating unit combination including a gas turbine, a waste heat boiler and a steam turbine.

[0013] Optionally, the control module is further used for:

[0014] When the first gas turbine sends a trip signal, the high-pressure drum, the medium-pressure drum and the low-pressure drum of the first waste heat boiler are all filled with water at a high level;

[0015] When the high-pressure drum is filled with water at a high position, the high-pressure feed water pump corresponding to the high-pressure drum is controlled to stop running;

[0016] When the high-pressure water supply of the medium-pressure drum is completed, the medium-pressure feed water pump corresponding to the medium-pressure drum is controlled to stop running;

[0017] When the high-level water filling of the low-pressure drum is completed, the low-pressure economizer recirculation pump corresponding to the low-pressure drum is controlled to stop running, and the electric door and regulating valve at the inlet of the low-pressure economizer are closed.

[0018] Optionally, the control module is further used for:

[0019] When the first gas turbine trips and the second gas turbine does not trip, the second waste heat boiler and the steam turbine are controlled to switch to an automatic adjustment state, wherein the automatic adjustment state includes one or more of automatic adjustment of the drum water level, automatic adjustment of the main steam temperature, automatic adjustment of the reheat steam temperature, automatic adjustment of the auxiliary steam pressure, automatic adjustment of the turbine shaft seal pressure and automatic adjustment of the condenser water level.

[0020] According to a second aspect of an embodiment of the present disclosure, a gas turbine trip fault self-recovery method is provided, which is applied to a gas turbine trip fault self-recovery system, and the method comprises:

[0021] Obtaining trip signals of a first gas turbine and a second gas turbine in a two-to-one operating unit;

[0022] Based on the trip signal, the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine in the two-to-one operating unit is controlled.

[0023] Optionally, the method further comprises:

[0024] When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine performs an interlock trip.

[0025] According to a third aspect of an embodiment of the present disclosure, a non-temporary computer-readable storage medium is provided, on which a computer program is stored. When the computer program is executed by a processor, the steps of the gas turbine trip fault self-recovery method described in the second aspect of the embodiment of the present disclosure are implemented.

[0026] According to a fourth aspect of an embodiment of the present disclosure, there is provided an electronic device, including:

[0027] a memory having a computer program stored thereon;

[0028] A processor is used to execute the computer program in the memory to implement the steps of the gas turbine trip fault self-recovery method described in the second aspect of the embodiment of the present disclosure.

[0029] According to a fifth aspect of an embodiment of the present disclosure, a computer program product is provided, comprising a computer program, which, when executed by a processor, implements the steps of the gas turbine trip fault self-recovery method described in the second aspect of an embodiment of the present disclosure.

[0030] In the above technical solution, the state monitoring module is used to monitor the trip state of the first gas turbine and the second gas turbine, and when the first gas turbine and / or the second gas turbine sends a trip signal, the trip signal is sent to the control module; the control module is used to control the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the trip signal. Through the above technical solution, the trip state of the first gas turbine and the second gas turbine is monitored by the state monitoring module, and the operation of the first gas turbine, the second gas turbine, the waste heat boiler, the second waste heat boiler and the steam turbine of the unit can be controlled based on the trip signal sent by the gas turbine, so as to realize the self-recovery of the gas turbine trip fault, improve the operation efficiency and safety of the unit, and reduce the operation and maintenance cost.

[0031] Other features and advantages of the present disclosure will be described in detail in the following detailed description. BRIEF DESCRIPTION OF THE DRAWINGS

[0032] The accompanying drawings are used to provide a further understanding of the present disclosure and constitute a part of the specification. Together with the following specific embodiments, they are used to explain the present disclosure but do not constitute a limitation of the present disclosure. In the accompanying drawings:

[0033] Figure 1 The invention is a block diagram of a gas turbine trip fault self-recovery system according to an exemplary embodiment.

[0034] Figure 2 The invention is a block diagram of another gas turbine trip fault self-recovery system according to an exemplary embodiment.

[0035] Figure 3 The present invention is a flow chart showing a method for self-recovery of a gas turbine trip fault according to an exemplary embodiment.

[0036] Figure 4 The present invention is a block diagram of a gas turbine trip fault self-recovery device according to an exemplary embodiment.

[0037] Figure 5 is a block diagram of an electronic device 500 according to an exemplary embodiment.

[0038] Figure 6 is a block diagram of an electronic device 600 according to an exemplary embodiment. DETAILED DESCRIPTION

[0039] Exemplary embodiments will be described in detail herein, examples of which are shown in the accompanying drawings. When the following description refers to the drawings, the same numbers in different drawings represent the same or similar elements unless otherwise indicated. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present disclosure. Instead, they are merely examples of devices and methods consistent with some aspects of the present disclosure as detailed in the appended claims.

[0040] It is understood that the terms "first", "second", etc. in the present disclosure are used to describe various information, but these information should not be limited to these terms. These terms are only used to distinguish the same type of information from each other, and do not indicate a specific order or importance.

[0041] It is further understood that, although the operations are described in a specific order in the drawings in the embodiments of the present disclosure, it should not be understood as requiring the operations to be performed in the specific order shown or in a serial order, or requiring the execution of all the operations shown to obtain the desired results. In certain environments, multitasking and parallel processing may be advantageous.

[0042] It should be noted that all actions of acquiring signals, information or data in the present disclosure are carried out in compliance with the relevant data protection laws and policies of the country where the device is located and with the authorization given by the owner of the corresponding device.

[0043] The two-to-one gas-steam combined cycle unit is an important component of a modern large-scale thermal power plant. It has the advantages of high efficiency, environmental protection, and flexibility. The unit is equipped with two gas turbines, two gas generators, a steam turbine, and a steam generator. The gas turbine and steam turbine drive the generators to generate electricity, thereby realizing efficient conversion and utilization of energy. The applicant found that during the actual operation of the unit, due to factors such as equipment aging and complex operating environment, gas turbine tripping failures often occur, which seriously affects the stable operation and economic benefits of the unit. Traditional fault recovery methods mostly rely on manual intervention, requiring operators to manually adjust and control according to the fault phenomenon, which is not only time-consuming and labor-intensive, but also has greater operational risks and uncertainties. Therefore, in response to the above problems, the applicant has proposed a gas turbine tripping fault self-recovery system and method. The gas turbine tripping fault self-recovery system and method provided by the present disclosure are described below.

[0044] Figure 1 is a block diagram of a gas turbine trip fault self-recovery system according to an exemplary embodiment. Figure 1 As shown, it is applied to a two-to-one operating unit, the two-to-one operating unit includes a first gas turbine, a second gas turbine, a first waste heat boiler, a second waste heat boiler and a steam turbine, and the gas turbine trip fault self-recovery system 100 includes: a state monitoring module 101 and a control module 102;

[0045] The state monitoring module 101 is used to monitor the trip state of the first gas turbine and the second gas turbine, and when the first gas turbine and / or the second gas turbine sends a trip signal, send the trip signal to the control module 102;

[0046] The control module 102 is used to control the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the trip signal.

[0047] Exemplarily, in a gas turbine trip fault self-recovery system, the state monitoring module 101 monitors the trip status of the first gas turbine and the second gas turbine in the two-to-one operating unit. When the first gas turbine and / or the second gas turbine trips, the state monitoring module obtains a trip signal issued by the first gas turbine and / or the second gas turbine, and sends the trip signal to the control module 102. The control module 102 controls the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the trip signal. For example, when the first gas turbine in the two-to-one operating unit trips and the second gas turbine does not trip, if the auxiliary steam system is the first gas turbine, the auxiliary steam system is automatically switched to the second waste heat boiler cold resteam source, and the pressure regulation system of the auxiliary steam system is switched to an automatic regulation state, which can realize automatic monitoring and recovery functions when a trip fault occurs in the unit gas turbine, thereby improving the unit operation efficiency and safety.

[0048] Through the above technical scheme, the tripping status of the first gas turbine and the second gas turbine is monitored by the status monitoring module, and the operation of the first gas turbine, the second gas turbine, the waste heat boiler, the second waste heat boiler and the steam turbine of the unit can be controlled based on the tripping signal sent by the gas turbine, so as to realize self-recovery of the gas turbine tripping fault, improve the operating efficiency and safety of the unit, and reduce the operation and maintenance cost.

[0049] Optionally, the control module is further used for:

[0050] When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine is controlled to perform interlock tripping.

[0051] Exemplarily, when a tripping fault occurs in the first gas turbine in the two-to-one operating unit, the first gas turbine sends a tripping signal and sends the tripping signal to the control module 102. The control module 102 controls the first waste heat boiler corresponding to the first gas turbine to perform an interlocking trip based on the tripping signal.

[0052] Figure 2 is a block diagram of another gas turbine trip fault self-recovery system according to an exemplary embodiment. Figure 2 As shown, the control module 102 includes: an override control unit 1021;

[0053] The override control unit 1021 is used to control the operating states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine to switch to a pressure self-regulating state and a temperature self-regulating state based on the trip signal.

[0054] Exemplarily, the override control unit 1021 controls the operating states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine to switch to the pressure self-regulation state and the temperature self-regulation state based on the trip signal issued by the first gas turbine and / or the second gas turbine, thereby avoiding the tediousness and instability of manual adjustment and improving the operating efficiency and safety of the power plant.

[0055] Optionally,

[0056] The control module 102 is also used to control the operation state of the steam turbine to switch to a one-to-one pressure automatic adjustment state, where the one-to-one is an operation unit combination including a gas turbine, a waste heat boiler and a steam turbine.

[0057] Optionally, the control module 102 is further configured to:

[0058] When the first gas turbine sends a trip signal, the high-pressure drum, the medium-pressure drum and the low-pressure drum of the first waste heat boiler are all filled with water at a high level;

[0059] When the high-pressure drum is filled with water at a high position, the high-pressure feed water pump corresponding to the high-pressure drum is controlled to stop running;

[0060] When the high-pressure water supply of the medium-pressure drum is completed, the medium-pressure feedwater pump corresponding to the medium-pressure drum is controlled to stop running;

[0061] When the high-level water filling of the low-pressure drum is completed, the low-pressure economizer recirculation pump corresponding to the low-pressure drum is controlled to stop running, and the electric door and regulating valve at the inlet of the low-pressure economizer are closed.

[0062] Optionally, the control module 102 is further configured to:

[0063] When the first gas turbine trips and the second gas turbine does not trip, the second waste heat boiler and the steam turbine are controlled to switch to an automatic adjustment state, which includes one or more of automatic adjustment of drum water level, automatic adjustment of main steam temperature, automatic adjustment of reheat steam temperature, automatic adjustment of auxiliary steam pressure, automatic adjustment of turbine shaft seal pressure and automatic adjustment of condenser water level. When the steam turbine is switched to the automatic adjustment state, the function of switching to manual operation when the deviation between the adjusted quantity of each adjustment system and the set value is large is shielded to keep the system in an automatic state.

[0064] Through the above technical scheme, the tripping status of the first gas turbine and the second gas turbine is monitored by the status monitoring module, and the operation of the first gas turbine, the second gas turbine, the waste heat boiler, the second waste heat boiler and the steam turbine of the unit can be controlled based on the tripping signal sent by the gas turbine, so as to realize self-recovery of the gas turbine tripping fault, improve the operating efficiency and safety of the unit, and reduce the operation and maintenance cost.

[0065] Figure 3FIG. 1 is a flow chart of a method for self-recovery of a gas turbine trip fault according to an exemplary embodiment. Figure 3 As shown, the method is applied to a gas turbine trip fault self-recovery system, and includes:

[0066] In step S11, the trip signals of the first gas turbine and the second gas turbine in the two-to-one operating unit are obtained.

[0067] In step S12, based on the trip signal, the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine in the two-to-one operating unit is controlled.

[0068] Exemplarily, the tripping signals of the first gas turbine and the second gas turbine in the two-to-one operating unit are obtained, and based on the tripping signals, the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine in the two-to-one operating unit is controlled. For example: in the two-to-one unit, the first gas turbine is gas turbine No. 1, the second gas turbine is gas turbine No. 2, the first waste heat boiler is waste heat boiler No. 1, and the second waste heat boiler is waste heat boiler No. 2. When gas turbine No. 1 trips and gas turbine No. 2 is in operation, the waste heat boiler No. 2 corresponding to gas turbine No. 2 is opened first to the low-pressure main steam drain valve of the heating network, and the waste heat boiler No. 2 is opened to the low-pressure main steam valve of the heating network after 2 minutes, and the waste heat boiler No. 1 is closed after opening; when gas turbine No. 2 trips and gas turbine No. 1 is in operation, the waste heat boiler No. 1 is opened to the low-pressure main steam valve of the heating network, and the waste heat boiler No. 2 is closed after opening to the low-pressure main steam valve of the heating network; when gas turbine No. 2 trips and gas turbine No. 1 is in operation, the waste heat boiler No. 1 is opened to the low-pressure main steam valve of the heating network, and the waste heat boiler No. 2 is closed after opening to the low-pressure main steam valve of the heating network.

[0069] Optionally, the method further comprises:

[0070] When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine performs an interlock trip.

[0071] Exemplarily, when a trip fault occurs in the first gas turbine in the two-to-one operating unit, the first gas turbine sends a trip signal, and in response to the trip signal, the first waste heat boiler corresponding to the first gas turbine performs an interlock trip.

[0072] Optionally, the method further comprises:

[0073] Based on the trip signal, the operating states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine are controlled to switch to a pressure self-regulating state and a temperature self-regulating state.

[0074] Optionally, the method further comprises:

[0075] Based on the trip signal, the operating state of the steam turbine is controlled to switch to a one-to-one pressure automatic adjustment state, where the one-to-one is an operating unit combination including a gas turbine, a waste heat boiler and a steam turbine.

[0076] Optionally, the method further comprises:

[0077] When the first gas turbine sends a trip signal, the high-pressure drum, the medium-pressure drum and the low-pressure drum of the first waste heat boiler are all filled with water at a high level;

[0078] When the high-pressure drum is filled with water at a high position, the high-pressure feed water pump corresponding to the high-pressure drum is controlled to stop running;

[0079] When the high-pressure water supply of the medium-pressure drum is completed, the medium-pressure feedwater pump corresponding to the medium-pressure drum is controlled to stop running;

[0080] When the high-level water filling of the low-pressure drum is completed, the low-pressure economizer recirculation pump corresponding to the low-pressure drum is controlled to stop running, and the electric door and regulating valve at the inlet of the low-pressure economizer are closed.

[0081] Optionally, the method further comprises:

[0082] When the first gas turbine trips and the second gas turbine does not trip, the second waste heat boiler and the steam turbine are controlled to switch to an automatic adjustment state, which includes one or more of automatic adjustment of the drum water level, automatic adjustment of the main steam temperature, automatic adjustment of the reheat steam temperature, automatic adjustment of the auxiliary steam pressure, automatic adjustment of the turbine shaft seal pressure and automatic adjustment of the condenser water level.

[0083] Through the above technical scheme, the tripping status of the first gas turbine and the second gas turbine is monitored by the status monitoring module, and the operation of the first gas turbine, the second gas turbine, the waste heat boiler, the second waste heat boiler and the steam turbine of the unit can be controlled based on the tripping signal sent by the gas turbine, so as to realize self-recovery of the gas turbine tripping fault, improve the operating efficiency and safety of the unit, and reduce the operation and maintenance cost.

[0084] Figure 4 is a block diagram of a gas turbine trip fault self-recovery device according to an exemplary embodiment. Figure 4 As shown, the gas turbine trip fault self-recovery device 400 includes: an acquisition module 401 and a unit control module 402;

[0085] An acquisition module 401 is used to acquire a trip signal of a first gas turbine and a second gas turbine in a two-to-one operating unit;

[0086] The unit control module 402 is used to control the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine in the two-to-one operating unit based on the trip signal.

[0087] Optionally, the gas turbine trip fault self-recovery device 400 further includes: an interlock trip module;

[0088] The interlocking tripping module is used to execute interlocking tripping of the first waste heat boiler corresponding to the first gas turbine when the first gas turbine sends a tripping signal.

[0089] Optionally, the unit control module 402 further includes: a first state control module;

[0090] The first state control module is used to control the operation states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine to switch to the pressure self-regulation state and the temperature self-regulation state based on the trip signal.

[0091] Optionally, the unit control module 402 further includes: a second state control module;

[0092] The second state control module is used to control the operating state of the steam turbine to switch to a one-to-one pressure automatic adjustment state based on the trip signal, where the one-to-one is an operating unit combination including a gas turbine, a waste heat boiler and a steam turbine.

[0093] Optionally, the unit control module 402 is further used for:

[0094] When the first gas turbine sends a trip signal, the high-pressure drum, the medium-pressure drum and the low-pressure drum of the first waste heat boiler are all filled with water at a high level;

[0095] When the high-pressure drum is filled with water at a high position, the high-pressure feed water pump corresponding to the high-pressure drum is controlled to stop running;

[0096] When the high-pressure water supply of the medium-pressure drum is completed, the medium-pressure feedwater pump corresponding to the medium-pressure drum is controlled to stop running;

[0097] When the high-level water filling of the low-pressure drum is completed, the low-pressure economizer recirculation pump corresponding to the low-pressure drum is controlled to stop running, and the electric door and regulating valve at the inlet of the low-pressure economizer are closed.

[0098] Optionally, the unit control module 402 is further used for:

[0099] When the first gas turbine trips and the second gas turbine does not trip, the second waste heat boiler and the steam turbine are controlled to switch to an automatic adjustment state, which includes one or more of automatic adjustment of the drum water level, automatic adjustment of the main steam temperature, automatic adjustment of the reheat steam temperature, automatic adjustment of the auxiliary steam pressure, automatic adjustment of the turbine shaft seal pressure and automatic adjustment of the condenser water level.

[0100] Regarding the device in the above embodiment, the specific manner in which each module performs operations has been described in detail in the embodiment of the method, and will not be elaborated here.

[0101] Figure 5 FIG. 5 is a block diagram of an electronic device 500 according to an exemplary embodiment. Figure 5 As shown, the electronic device 500 may include: a processor 501 and a memory 502. The electronic device 500 may also include one or more of a multimedia component 503, an input / output (I / O) interface 504, and a communication component 505.

[0102] The processor 501 is used to control the overall operation of the electronic device 500 to complete all or part of the steps in the above-mentioned gas turbine trip fault self-recovery method. The memory 502 is used to store various types of data to support the operation of the electronic device 500, and these data may include, for example, instructions for any application or method used to operate on the electronic device 500, and application-related data, such as contact data, sent and received messages, pictures, audio, video, etc. The memory 502 can be implemented by any type of volatile or non-volatile storage device or a combination thereof, such as static random access memory (Static Random Access Memory, referred to as SRAM), electrically erasable programmable read-only memory (Electrically Erasable Programmable Read-Only Memory, referred to as EEPROM), erasable programmable read-only memory (Erasable Programmable Read-Only Memory, referred to as EPROM), programmable read-only memory (Programmable Read-Only Memory, referred to as PROM), read-only memory (Read-Only Memory, referred to as ROM), magnetic memory, flash memory, magnetic disk or optical disk. The multimedia component 503 may include a screen and an audio component. The screen may be, for example, a touch screen, and the audio component is used to output and / or input audio signals. For example, the audio component may include a microphone, which is used to receive external audio signals. The received audio signal may be further stored in the memory 502 or sent through the communication component 505. The audio component also includes at least one speaker for outputting audio signals. The I / O interface 504 provides an interface between the processor 501 and other interface modules, and the above-mentioned other interface modules may be keyboards, mice, buttons, etc. These buttons may be virtual buttons or physical buttons. The communication component 505 is used for wired or wireless communication between the electronic device 500 and other devices. Wireless communication, such as Wi-Fi, Bluetooth, Near Field Communication (NFC), 2G, 3G, 4G, NB-IOT, eMTC, or other 4G, etc., or a combination of one or more of them, is not limited here. Therefore, the corresponding communication component 505 may include: Wi-Fi module, Bluetooth module, NFC module, etc.

[0103] In an exemplary embodiment, the electronic device 500 can be implemented by one or more application specific integrated circuits (ASIC), digital signal processors (DSP), digital signal processing devices (DSPD), programmable logic devices (PLD), field programmable gate arrays (FPGA), controllers, microcontrollers, microprocessors or other electronic components to execute the above-mentioned gas turbine trip fault self-recovery method.

[0104] In another exemplary embodiment, a computer-readable storage medium including program instructions is also provided, and when the program instructions are executed by a processor, the steps of the above-mentioned gas turbine trip fault self-recovery method are implemented. For example, the computer-readable storage medium can be the above-mentioned memory 502 including program instructions, and the above-mentioned program instructions can be executed by the processor 501 of the electronic device 500 to complete the above-mentioned gas turbine trip fault self-recovery method.

[0105] Figure 6 6 is a block diagram of an electronic device 600 according to an exemplary embodiment. For example, the electronic device 600 may be provided as a server. Figure 6 The electronic device 600 includes a processor 622, which may be one or more, and a memory 632 for storing a computer program executable by the processor 622. The computer program stored in the memory 632 may include one or more modules, each corresponding to a set of instructions. In addition, the processor 622 may be configured to execute the computer program to perform the above-mentioned gas turbine trip fault self-recovery method.

[0106] In addition, the electronic device 600 may further include a power supply component 626 and a communication component 650, wherein the power supply component 626 may be configured to perform power management of the electronic device 600, and the communication component 650 may be configured to implement communication, for example, wired or wireless communication, of the electronic device 600. In addition, the electronic device 600 may further include an input / output (I / O) interface 658. The electronic device 600 may operate based on an operating system stored in the memory 632.

[0107] In another exemplary embodiment, a computer-readable storage medium including program instructions is also provided, and when the program instructions are executed by a processor, the steps of the above-mentioned gas turbine trip fault self-recovery method are implemented. For example, the non-transitory computer-readable storage medium can be the above-mentioned memory 632 including program instructions, and the above-mentioned program instructions can be executed by the processor 622 of the electronic device 600 to complete the above-mentioned gas turbine trip fault self-recovery method.

[0108] In another exemplary embodiment, a computer program product is also provided. The computer program product includes a computer program executable by a programmable device, and the computer program has a code portion for executing the above-mentioned gas turbine trip fault self-recovery method when executed by the programmable device.

[0109] The preferred embodiments of the present disclosure are described in detail above in conjunction with the accompanying drawings; however, the present disclosure is not limited to the specific details in the above embodiments. Within the technical concept of the present disclosure, a variety of simple modifications can be made to the technical solution of the present disclosure, and these simple modifications all fall within the protection scope of the present disclosure.

[0110] It should also be noted that the various specific technical features described in the above specific embodiments can be combined in any suitable manner without contradiction. In order to avoid unnecessary repetition, the present disclosure will not further describe various possible combinations.

[0111] In addition, various embodiments of the present disclosure may be arbitrarily combined, and as long as they do not violate the concept of the present disclosure, they should also be regarded as the contents disclosed by the present disclosure.

Claims

1. A gas turbine trip fault self-recovery system, It is characterized in that Applied to a two-to-one operating unit, the two-to-one operating unit includes a first gas turbine, a second gas turbine, a first waste heat boiler, a second waste heat boiler and a steam turbine, the system includes: a state monitoring module and a control module; The state monitoring module is used to monitor the trip state of the first gas turbine and the second gas turbine, and when the first gas turbine and / or the second gas turbine sends a trip signal, send the trip signal to the control module; The control module is used to control the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine based on the trip signal.

2. The system according to claim 1, It is characterized in that The control module is also used for: When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine is controlled to perform interlock tripping.

3. The system according to claim 1, It is characterized in that The control module includes: an override control unit; The override control unit is used to control the operation states of the high-pressure, medium-pressure and low-pressure bypasses of the gas turbine to switch to a pressure self-regulation state and a temperature self-regulation state based on the trip signal.

4. The system according to claim 1, It is characterized in that The control module is also used to control the operating state of the steam turbine to switch to a one-to-one pressure automatic adjustment state, where the one-to-one is an operating unit combination including a gas turbine, a waste heat boiler and a steam turbine.

5. The system according to claim 1, It is characterized in that The control module is also used for: When the first gas turbine sends a trip signal, the high-pressure drum, the medium-pressure drum and the low-pressure drum of the first waste heat boiler are all filled with water at a high level; When the high-pressure drum is filled with water at a high position, the high-pressure feed water pump corresponding to the high-pressure drum is controlled to stop running; When the high-pressure water supply of the medium-pressure drum is completed, the medium-pressure feed water pump corresponding to the medium-pressure drum is controlled to stop running; When the high-level water filling of the low-pressure drum is completed, the low-pressure economizer recirculation pump corresponding to the low-pressure drum is controlled to stop running, and the electric door and regulating valve at the inlet of the low-pressure economizer are closed.

6. The system according to claim 1, It is characterized in that The control module is also used for: When the first gas turbine trips and the second gas turbine does not trip, the second waste heat boiler and the steam turbine are controlled to switch to an automatic adjustment state, wherein the automatic adjustment state includes one or more of automatic adjustment of the drum water level, automatic adjustment of the main steam temperature, automatic adjustment of the reheat steam temperature, automatic adjustment of the auxiliary steam pressure, automatic adjustment of the turbine shaft seal pressure and automatic adjustment of the condenser water level.

7. A gas turbine trip fault self-recovery method, It is characterized in that Applied to a gas turbine trip fault self-recovery system, the method comprises: Obtaining trip signals of a first gas turbine and a second gas turbine in a two-to-one operating unit; Based on the trip signal, the operation of the first gas turbine, the second gas turbine, the first waste heat boiler, the second waste heat boiler and the steam turbine in the two-to-one operating unit is controlled.

8. The method according to claim 7, It is characterized in that The method further comprises: When the first gas turbine sends a trip signal, the first waste heat boiler corresponding to the first gas turbine performs an interlock trip.

9. A non-transitory computer-readable storage medium having stored thereon a computer program, It is characterized in that When the computer program is executed by a processor, the steps of the method according to any one of claims 7 to 8 are implemented.

10. An electronic device, It is characterized in that include: a memory having a computer program stored thereon; A processor, configured to execute the computer program in the memory to implement the steps of the method according to any one of claims 7 to 8.

11. A computer program product comprising a computer program, It is characterized in that When the computer program is executed by a processor, the steps of the method according to any one of claims 7 to 8 are implemented.