Offshore turbine generator set debugging method, device, equipment and medium

Abstract

The invention relates to the technical field of offshore turbine generator set debugging, and discloses an offshore turbine generator set debugging method, device and equipment and a medium. Compressor corollary equipment and the compressor can be debugged; and debugging the gas turbine corollary equipment. And after the compressor corollary equipment, the compressor and the gas turbine corollary equipment are debugged successfully, gas turbine combined compressor debugging, gas ignition operation debugging and power generation grid-connected debugging are executed in sequence, so that debugging of the offshore turbine generator set is completed. According to the invention, the offshore turbine generator set can be debugged by modules, the debugging quality and reliability are improved, the offshore operation period is shortened, the time cost is saved, and the debugging of the offshore turbine generator set is effectively realized.

Description

Technical Field

[0001] The present invention relates to the technical field of offshore turbine generator set debugging, and in particular to an offshore turbine generator set debugging method, device, equipment and medium. Background Art

[0002] Offshore platforms refer to structures that provide production and living facilities for activities such as drilling, oil production, transportation, observation, navigation and construction at sea. Offshore turbine generator sets are one of the core equipment on offshore platforms, providing power support for various facilities on offshore platforms.

[0003] The normal operation of offshore turbine generator sets is crucial to ensuring the safe and stable production of offshore platforms. Offshore turbine generator sets need to be debugged to promptly discover and resolve potential problems.

[0004] However, the relevant technology cannot effectively realize the debugging of offshore turbine generator sets, which may affect the safe and stable production of offshore platforms. Summary of the invention

[0005] The present invention provides a method, device, equipment and medium for debugging an offshore turbine generator set, which are used to effectively realize the debugging of the offshore turbine generator set.

[0006] In a first aspect, the present invention provides a method for debugging an offshore turbine generator set, comprising:

[0007] Debugging of compressor supporting equipment and compressors; and debugging of gas turbine supporting equipment;

[0008] After the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, gas ignition operation debugging and power generation grid connection debugging are carried out in sequence to complete the debugging of the offshore turbine generator set.

[0009] Optionally, the compressor supporting equipment includes an electrical cabinet and instruments of the compressor; the debugging of the compressor supporting equipment and the compressor includes:

[0010] Powering on the electrical cabinet of the compressor and obtaining parameter measurement values ​​of instruments in the electrical cabinet;

[0011] Determine whether the parameter measurement value is normal and obtain a corresponding determination result;

[0012] When the determination result is normal, performing a single compressor test;

[0013] When the compressor single-machine test passes successfully, perform the compressor remote start and stop debugging.

[0014] Optionally, the gas turbine supporting equipment includes an electrical cabinet, a control cabinet, a control system, a cooling system, an auxiliary system and a starting motor of the gas turbine; the debugging of the gas turbine supporting equipment includes:

[0015] Powering on the electrical cabinet and control cabinet of the gas turbine;

[0016] Downloading the relevant control logic of the gas engine to the gas control system, comparing the data in the control system with the relevant field data to see whether they are the same and obtaining the comparison result;

[0017] When the comparison result is normal, generating and outputting second instruction information to instruct the commissioning personnel to manually commission the cooling system and the auxiliary system in sequence;

[0018] After the manual debugging of the cooling system and the auxiliary system is successfully passed, the starter motor is debugged to complete the debugging of the gas engine supporting equipment.

[0019] Optionally, the gas turbine combined compressor debugging includes gas turbine controlled compressor start and stop debugging, gas turbine interlocked compressor start and stop debugging and instrument assembly performance testing.

[0020] Optionally, perform gas turbine control compressor start and stop commissioning, including:

[0021] Starting the gas engine, and during the operation of the gas engine, controlling the compressor to start and stop according to the operating state of the gas engine;

[0022] Perform gas turbine interlocked compressor start and stop commissioning, including:

[0023] After the start-stop commissioning of the gas engine controlling the compressor is successfully passed, the gas engine and the compressor are jointly operated according to the preset interlocking conditions and operating conditions;

[0024] Perform instrument assembly performance testing including:

[0025] After the start-stop debugging of the gas turbine interlocked compressor is successfully passed, the performance of the instrument assembly is tested by using air as the medium and controlling the gas turbine and the compressor to run jointly.

[0026] Optionally, perform gas ignition operation commissioning, including:

[0027] Generate and output third instruction information to instruct the commissioning personnel to perform manual ignition commissioning on the gas engine;

[0028] After the manual ignition debugging of the gas engine is successfully performed, the automatic program of the gas engine is tested and optimized in turn;

[0029] After the test and optimization of the automatic program are successfully completed, controlling the gas turbine to be connected to the grid and controlling the gas turbine to operate continuously;

[0030] Execute power generation grid connection commissioning, including:

[0031] Execute constant power grid-connected mode debugging, and after successful debugging, perform equal-proportional grid-connected mode debugging.

[0032] Optionally, before testing and optimizing the automatic program of the gas engine in sequence, the method further includes:

[0033] remotely start and stop the gas engine;

[0034] After the manual ignition debugging of the gas engine is successful, the automatic program of the gas engine is tested and optimized in sequence, including:

[0035] After the manual ignition debugging and remote start-stop debugging of the gas engine are successfully performed, the automatic program of the gas engine is tested and optimized in turn.

[0036] In a second aspect, the present invention provides an offshore turbine generator unit commissioning device, comprising:

[0037] A first debugging unit, used for debugging the compressor supporting equipment and the compressor;

[0038] The second debugging unit is used to debug the gas turbine supporting equipment;

[0039] The third debugging unit is used to perform the debugging of the gas turbine combined compressor, the gas ignition operation debugging and the power generation grid connection debugging in sequence after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, so as to complete the debugging of the offshore turbine generator set.

[0040] Optionally, the compressor supporting equipment includes an electrical cabinet and instruments of the compressor; the first debugging unit is further used for:

[0041] Powering on the electrical cabinet of the compressor and obtaining parameter measurement values ​​of instruments in the electrical cabinet;

[0042] Determine whether the parameter measurement value is normal and obtain a corresponding determination result;

[0043] When the determination result is normal, performing a single compressor test;

[0044] When the compressor single-machine test passes successfully, perform the compressor remote start and stop debugging.

[0045] Optionally, the gas turbine supporting equipment includes an electrical cabinet, a control cabinet, a control system, a cooling system, an auxiliary system and a starting motor of the gas turbine; the second debugging unit is also used for:

[0046] Powering on the electrical cabinet and control cabinet of the gas turbine;

[0047] Downloading the relevant control logic of the gas engine to the gas control system, comparing the data in the control system with the relevant field data to see whether they are the same and obtaining the comparison result;

[0048] When the comparison result is normal, generating and outputting second instruction information to instruct the commissioning personnel to manually commission the cooling system and the auxiliary system in sequence;

[0049] After the manual debugging of the cooling system and the auxiliary system is successfully passed, the starter motor is debugged to complete the debugging of the gas engine supporting equipment.

[0050] Optionally, the gas turbine combined compressor debugging includes gas turbine controlled compressor start and stop debugging, gas turbine interlocked compressor start and stop debugging and instrument assembly performance testing.

[0051] Optionally, the third debugging unit is further used for:

[0052] Starting the gas engine, and during the operation of the gas engine, controlling the compressor to start and stop according to the operating state of the gas engine;

[0053] The third debugging unit is also used for:

[0054] After the start-stop commissioning of the gas engine controlling the compressor is successfully passed, the gas engine and the compressor are jointly operated according to the preset interlocking conditions and operating conditions;

[0055] The third debugging unit is also used for:

[0056] After the start-stop debugging of the gas turbine interlocked compressor is successfully passed, the performance of the instrument assembly is tested by using air as the medium and controlling the gas turbine and the compressor to run jointly.

[0057] Optionally, the device further comprises:

[0058] A fourth debugging unit, used for remotely starting and stopping the gas engine before testing and optimizing the automatic program of the gas engine in sequence;

[0059] The third debugging unit is used to test and optimize the automatic program of the gas engine in sequence after the manual ignition debugging and remote start-stop debugging of the gas engine are successfully performed.

[0060] In a third aspect, the present invention provides a computer device, comprising: a memory and a processor, the memory and the processor being communicatively connected to each other, the memory storing computer instructions, and the processor executing the offshore turbine generator set debugging method of the first aspect or any corresponding embodiment thereof by executing the computer instructions.

[0061] In a fourth aspect, the present invention provides a computer-readable storage medium having computer instructions stored thereon, the computer instructions being used to enable a computer to execute the offshore turbine generator set commissioning method of the first aspect or any corresponding embodiment thereof.

[0062] The offshore turbine generator set debugging method, device, equipment and medium provided by the present invention can debug the compressor supporting equipment and the compressor; and debug the gas engine supporting equipment; after the debugging of the compressor supporting equipment, the compressor and the gas engine supporting equipment is successfully passed, the gas engine combined compressor debugging, the gas ignition operation debugging and the power generation grid connection debugging are performed in sequence to complete the debugging of the offshore turbine generator set. The present invention can debug the offshore turbine generator set in modules, improve the reliability of the debugging quality, shorten the offshore operation cycle, save time and cost, and effectively realize the debugging of the offshore turbine generator set. BRIEF DESCRIPTION OF THE DRAWINGS

[0063] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0064] Figure 1 A flow chart of a method for debugging an offshore turbine generator set provided by an embodiment of the present invention;

[0065] Figure 2 A flow chart of another offshore turbine generator set debugging method provided by an embodiment of the present invention;

[0066] Figure 3 A schematic structural diagram of an offshore turbine generator set debugging device provided by an embodiment of the present invention;

[0067] Figure 4 A schematic diagram of the structure of a computer device provided in an embodiment of the present invention. DETAILED DESCRIPTION

[0068] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be clearly and completely described below in conjunction with the drawings of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0069] In order to solve the problem that the relevant technology cannot effectively realize the debugging of offshore turbine generator sets, which may affect the safe and stable production of offshore platforms, this embodiment proposes an offshore turbine generator set debugging method, device, equipment and medium, which can debug the compressor supporting equipment and the compressor; and debug the gas turbine supporting equipment; after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, gas ignition operation debugging and power generation grid debugging are performed in sequence to complete the debugging of the offshore turbine generator set. The present invention can debug the offshore turbine generator set in modules, improve the reliability of debugging quality, shorten the offshore operation cycle, save time and cost, and effectively realize the debugging of the offshore turbine generator set.

[0070] Combine the following Figure 1-Figure 2 The present invention describes the offshore turbine generator set commissioning method.

[0071] like Figure 1 As shown, this embodiment proposes a first offshore turbine generator set commissioning method, which may include the following steps:

[0072] S101. Debug the compressor supporting equipment and compressor.

[0073] It should be noted that, in this embodiment, the offshore turbine generator set can be debugged in modules to improve the reliability of the debugging quality, shorten the offshore operation cycle, and save time and cost.

[0074] Specifically, in this embodiment, the commissioning of the offshore turbine generator set can be divided into the commissioning of the compressor part, the commissioning of the gas turbine part, the gas ignition and automatic operation, and the commissioning of power generation and grid connection.

[0075] Among them, the compressor partial debugging may include debugging the compressor supporting equipment and the compressor.

[0076] Optionally, the compressor supporting equipment includes an electrical cabinet and instruments of the compressor. In this case, step S101 may include:

[0077] Power on the electrical cabinet of the compressor and obtain the parameter measurement values ​​of the instruments in the electrical cabinet;

[0078] Determine whether the parameter measurement value is normal and obtain the corresponding determination result;

[0079] When the result is determined to be normal, perform a single compressor test;

[0080] When the compressor single-machine test passes successfully, perform the compressor remote start and stop debugging.

[0081] The parameter measurement values ​​of the instrument may include the measurement values ​​of parameters such as temperature, pressure, flow and vibration.

[0082] It should be noted that the compressor stand-alone test is performed on the unit itself. After the test is successful, the entire unit is remotely started and stopped.

[0083] S102. Debug the gas turbine supporting equipment.

[0084] Specifically, this embodiment can perform step S102 at the same time as step S101. This embodiment can also perform step S101 first and then perform step S102. Figure 1 Of course, in this embodiment, step S102 may be performed first, and then step S101 may be performed.

[0085] Optionally, the gas turbine supporting equipment includes the gas turbine electrical cabinet, control cabinet, control system, cooling system, auxiliary system and starting motor. In this case, step S102 may include:

[0086] Power on the electrical cabinet and control cabinet of the gas turbine;

[0087] Download the relevant control logic of the gas turbine to the gas control system, compare the data in the control system with the relevant field data to see if they are the same and obtain the comparison results;

[0088] When the comparison result is normal, second instruction information is generated and output to instruct the commissioning personnel to manually commission the cooling system and the auxiliary system in sequence;

[0089] After the manual debugging of the cooling system and auxiliary system is successfully passed, the starting motor is debugged to complete the debugging of the gas turbine supporting equipment.

[0090] Specifically, in this embodiment, after the electrical cabinet and control cabinet of the gas turbine are powered on, the relevant control logic of the gas turbine can be downloaded to the control system of the gas turbine, and then the field data and the control system data can be compared.

[0091] S103. After the debugging of the compressor supporting equipment and the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, the gas ignition operation debugging and the power generation grid connection debugging are performed in sequence to complete the debugging of the offshore turbine generator set.

[0092] Specifically, this embodiment can execute the debugging of the gas turbine combined with the compressor after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, and execute the gas ignition operation debugging after the debugging of the gas turbine combined with the compressor is successfully passed, and then execute the power generation grid connection debugging after the gas ignition operation debugging is successfully passed.

[0093] The offshore turbine generator set debugging method proposed in this embodiment can debug the compressor supporting equipment and the compressor; and debug the gas turbine supporting equipment; after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, the gas ignition operation debugging and the power generation grid debugging are performed in sequence to complete the debugging of the offshore turbine generator set. This embodiment can debug the offshore turbine generator set in modules, improve the reliability of the debugging quality, shorten the offshore operation cycle, save time and cost, and effectively realize the debugging of the offshore turbine generator set.

[0094] based on Figure 1 This embodiment proposes a second offshore turbine generator set debugging method, in which the gas turbine combined compressor debugging includes gas turbine control compressor start and stop debugging, gas turbine interlocked compressor start and stop debugging and instrument assembly performance testing.

[0095] Among them, the start and stop commissioning of the gas turbine control compressor includes:

[0096] Start the gas engine and, during the operation of the gas engine, control the compressor to start and stop according to the operating status of the gas engine.

[0097] Among them, the start and stop commissioning of the gas turbine interlocking compressor includes:

[0098] After the gas turbine control compressor start and stop debugging is successfully passed, the gas turbine and compressor are jointly operated according to the preset interlocking conditions and operating conditions.

[0099] Among them, the instrument assembly performance test is performed, including:

[0100] After the start-stop commissioning of the gas turbine interlocking compressor is successfully passed, use air as the medium and control the gas turbine and compressor to run jointly to test the performance of the instrument assembly.

[0101] Optionally, perform gas ignition operation commissioning, including:

[0102] Generate and output third instruction information to instruct the commissioning personnel to perform manual ignition commissioning on the gas engine;

[0103] After the manual ignition debugging of the gas turbine is successful, the automatic program of the gas turbine is tested and optimized in turn;

[0104] After the testing and optimization of the automatic program is successfully completed, the gas turbine is controlled to be connected to the grid and to operate continuously.

[0105] Optionally, perform power generation grid connection commissioning, including:

[0106] Execute constant power grid-connected mode debugging, and after successful debugging, perform equal-proportional grid-connected mode debugging.

[0107] Optionally, before step S103, the method may further include:

[0108] Remote start and stop debugging of the gas turbine.

[0109] At this time, step S103 may include:

[0110] After the manual ignition debugging and remote start and stop debugging of the gas turbine are successfully carried out, the automatic program of the gas turbine is tested and optimized in turn.

[0111] The offshore turbine generator set debugging method proposed in this embodiment can effectively complete the gas turbine control compressor start and stop debugging, gas turbine interlocked compressor start and stop debugging and instrument assembly performance testing, thereby effectively ensuring the realization of offshore turbine generator set debugging.

[0112] based on Figure 1 ,like Figure 2 The embodiment shown in the figure proposes a third offshore turbine generator set debugging method. In this method, the embodiment can first perform system debugging preparation, and then perform specific debugging after the preparation is completed.

[0113] Specifically, the method can add sub-module debugging to the offshore turbine generator set debugging, which can specifically include the compressor part debugging (i.e. Figure 2 The compressor commissioning in Figure 2 Micro gas turbine debugging), gas ignition and automatic operation and power generation grid connection debugging.

[0114] The compressor debugging may include powering on the compressor electrical cabinet, checking whether the instrument parameters are abnormal, testing the compressor stand-alone, and remotely starting and stopping the compressor.

[0115] Among them, the micro gas turbine debugging may include powering on the gas turbine electrical cabinet and control cabinet, program downloading and data checking, manual debugging of the gas turbine cooling system, manual debugging of the gas turbine auxiliary system, debugging of the gas turbine starting motor and start and stop of the gas turbine control compressor, gas turbine interlocking compressor start and stop and simulating actual working conditions testing, and the performance of the instrument assembly using air in conjunction with the compressor and the gas turbine.

[0116] Among them, gas ignition and automatic operation may include manual ignition, start and stop of the gas turbine, as well as gas turbine automatic program testing, gas turbine automatic program optimization and continuous operation of the gas turbine system.

[0117] The power generation grid connection commissioning may include controlling the gas turbine grid connection operation and the control system running continuously for 72 hours. The specific modes may include constant power grid connection mode and equal proportion grid connection mode.

[0118] Specifically, the method may also include energy station system debugging, which may specifically include remote start and stop of the gas engine, and after the remote start and stop of the gas engine is successfully completed, the gas engine automatic program optimization may be performed.

[0119] It should be noted that, in this embodiment, when a fault is detected during the debugging process, the corresponding fault cause can be determined and corresponding information can be output to instruct the debugging personnel to take corresponding measures to solve the problem according to the information.

[0120] Table 1 Fault cause analysis and recommended information

[0121]

[0122]

[0123]

[0124] The offshore turbine generator set debugging method proposed in this embodiment can debug the offshore turbine generator set in modules to improve the debugging quality and reliability. When a fault is detected during the debugging process, the corresponding fault cause can be determined and corresponding information can be output to instruct the debugging personnel to take corresponding measures to solve the problem according to the information, thereby improving the troubleshooting efficiency and maintenance efficiency, thereby improving the debugging efficiency and ensuring the safe and stable operation of the offshore turbine generator set.

[0125] like Figure 3 As shown, this embodiment proposes that the present invention provides an offshore turbine generator set debugging device, comprising:

[0126] A first debugging unit, used for debugging the compressor supporting equipment and the compressor;

[0127] The second debugging unit is used to debug the gas turbine supporting equipment;

[0128] The third debugging unit is used to perform the debugging of the gas turbine combined compressor, the gas ignition operation debugging and the power generation grid connection debugging in sequence after the debugging of the compressor supporting equipment and the compressor and gas turbine supporting equipment is successfully passed, so as to complete the debugging of the offshore turbine generator set.

[0129] It should be noted that the processing of the first debugging unit, the second debugging unit and the third debugging unit and the beneficial effects thereof can be referred to in Figure 1 Steps S101 to S103 in the above are not described in detail.

[0130] Optionally, the compressor supporting equipment includes an electrical cabinet and instruments of the compressor; the first debugging unit is also used for:

[0131] Power on the electrical cabinet of the compressor and obtain the parameter measurement values ​​of the instruments in the electrical cabinet;

[0132] Determine whether the parameter measurement value is normal and obtain the corresponding determination result;

[0133] When the result is determined to be normal, perform a single compressor test;

[0134] When the compressor single-machine test passes successfully, perform the compressor remote start and stop debugging.

[0135] Optionally, the gas turbine supporting equipment includes the gas turbine electrical cabinet, control cabinet, control system, cooling system, auxiliary system and starting motor; the second debugging unit is also used for:

[0136] Power on the electrical cabinet and control cabinet of the gas turbine;

[0137] Download the relevant control logic of the gas turbine to the gas control system, compare the data in the control system with the relevant field data to see if they are the same and obtain the comparison results;

[0138] When the comparison result is normal, second instruction information is generated and output to instruct the commissioning personnel to manually commission the cooling system and the auxiliary system in sequence;

[0139] After the manual debugging of the cooling system and auxiliary system is successfully passed, the starting motor is debugged to complete the debugging of the gas turbine supporting equipment.

[0140] Optionally, the gas turbine combined compressor commissioning includes gas turbine controlled compressor start and stop commissioning, gas turbine interlocked compressor start and stop commissioning and instrument assembly performance testing.

[0141] Optionally, the third debugging unit is further used for:

[0142] Start the gas engine and, during the operation of the gas engine, control the compressor to start and stop according to the operating status of the gas engine;

[0143] The third debugging unit is also used for:

[0144] After the start and stop commissioning of the gas turbine control compressor is successfully passed, the gas turbine and compressor are jointly operated according to the preset interlocking conditions and operating conditions;

[0145] The third debugging unit is also used for:

[0146] After the start-stop commissioning of the gas turbine interlocking compressor is successfully passed, use air as the medium and control the gas turbine and compressor to run jointly to test the performance of the instrument assembly.

[0147] Optionally, the device further comprises:

[0148] The fourth debugging unit is used to remotely start and stop the gas turbine before testing and optimizing the automatic program of the gas turbine in turn;

[0149] The third debugging unit is used to test and optimize the automatic program of the gas engine in sequence after the manual ignition debugging and remote start and stop debugging of the gas engine are successful.

[0150] The offshore turbine generator set debugging device proposed in this embodiment can debug the compressor supporting equipment and the compressor; and debug the gas turbine supporting equipment; after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, the gas ignition operation debugging and the power generation grid debugging are performed in sequence to complete the debugging of the offshore turbine generator set. This embodiment can debug the offshore turbine generator set in modules, improve the reliability of the debugging quality, shorten the offshore operation cycle, save time and cost, and effectively realize the debugging of the offshore turbine generator set.

[0151] The offshore turbine generator set debugging device in this embodiment is presented in the form of a functional unit, where the unit refers to an ASIC (Application Specific Integrated Circuit) circuit, a processor and memory that executes one or more software or fixed programs, and / or other devices that can provide the above functions.

[0152] The embodiment of the present invention also provides a computer device having the above Figure 3 The offshore turbine generator set commissioning device is shown.

[0153] See also Figure 4, a schematic diagram of the structure of a computer device provided by an optional embodiment of the present invention, the computer device includes: one or more processors 10, a memory 20, and interfaces for connecting various components, including high-speed interfaces and low-speed interfaces. The various components are connected to each other using different buses for communication, and can be installed on a common motherboard or installed in other ways as needed. The processor can process instructions executed in the computer device, including instructions stored in or on the memory to display graphical information of the GUI on an external input / output device (such as a display device coupled to the interface). In some optional embodiments, if necessary, multiple processors and / or multiple buses can be used together with multiple memories and multiple memories. Similarly, multiple computer devices can be connected, and each device provides part of the necessary operations (for example, as a server array, a group of blade servers, or a multi-processor system). Figure 4 A processor 10 is taken as an example.

[0154] The processor 10 may be a central processing unit, a network processor or a combination thereof. The processor 10 may further include a hardware chip. The hardware chip may be a dedicated integrated circuit, a programmable logic device or a combination thereof. The programmable logic device may be a complex programmable logic device, a field programmable gate array, a general purpose array logic or any combination thereof.

[0155] The memory 20 stores instructions executable by at least one processor 10, so that at least one processor 10 executes the method shown in the above embodiment.

[0156] The memory 20 may include a program storage area and a data storage area, wherein the program storage area may store an operating system, an application required for at least one function. The data storage area may store data created according to the use of the computer device, etc. In addition, the memory 20 may include a high-speed random access memory, and may also include a non-transient memory, such as at least one disk storage device, a flash memory device, or other non-transient solid-state storage devices. In some optional embodiments, the memory 20 may optionally include a memory remotely arranged relative to the processor 10, and these remote memories may be connected to the computer device via a network. Examples of the above-mentioned network include, but are not limited to, the Internet, an intranet, a local area network, a mobile communication network, and combinations thereof.

[0157] The memory 20 may include a volatile memory, such as a random access memory. The memory may also include a non-volatile memory, such as a flash memory, a hard disk or a solid state drive. The memory 20 may also include a combination of the above-mentioned types of memory.

[0158] The computer device further comprises a communication interface 30 for the computer device to communicate with other devices or a communication network.

[0159] The embodiment of the present invention also provides a computer-readable storage medium. The method according to the embodiment of the present invention can be implemented in hardware, firmware, or can be implemented as a computer code that can be recorded in a storage medium, or can be implemented as a computer code that is originally stored in a remote storage medium or a non-temporary machine-readable storage medium and will be stored in a local storage medium through a network download, so that the method described herein can be stored in such software processing on a storage medium using a general-purpose computer, a dedicated processor, or programmable or dedicated hardware. Among them, the storage medium can be a magnetic disk, an optical disk, a read-only storage memory, a random access memory, a flash memory, a hard disk or a solid-state hard disk, etc.; further, the storage medium can also include a combination of the above types of memories. It can be understood that a computer, a processor, a microprocessor controller, or programmable hardware includes a storage component that can store or receive software or computer code. When the software or computer code is accessed and executed by a computer, a processor, or hardware, the method shown in the above embodiment is implemented.

[0160] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A method for debugging an offshore turbine generator set, characterized in that: include: Debug the compressor supporting equipment and compressor; And, debug the gas turbine supporting equipment; After the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, the gas turbine combined compressor debugging, gas ignition operation debugging and power generation grid connection debugging are carried out in sequence to complete the debugging of the offshore turbine generator set.

2. The method according to claim 1, characterized in that The compressor supporting equipment includes the electrical cabinet and instruments of the compressor; The debugging of the compressor supporting equipment and the compressor includes: Powering on the electrical cabinet of the compressor and obtaining parameter measurement values ​​of instruments in the electrical cabinet; Determine whether the parameter measurement value is normal and obtain a corresponding determination result; When the determination result is normal, performing a single compressor test; When the compressor single-machine test passes successfully, perform the compressor remote start and stop debugging.

3. The method according to claim 1, characterized in that The gas turbine supporting equipment includes the gas turbine electrical cabinet, control cabinet, control system, cooling system, auxiliary system and starting motor; the debugging of the gas turbine supporting equipment includes: Powering on the electrical cabinet and control cabinet of the gas turbine; Downloading the relevant control logic of the gas engine to the gas control system, comparing the data in the control system with the relevant field data to see whether they are the same and obtaining the comparison result; When the comparison result is normal, generating and outputting second instruction information to instruct the commissioning personnel to manually commission the cooling system and the auxiliary system in sequence; After the manual debugging of the cooling system and the auxiliary system is successfully passed, the starter motor is debugged to complete the debugging of the gas engine supporting equipment.

4. The method according to claim 1, characterized in that: The gas turbine combined compressor debugging includes gas turbine control compressor start and stop debugging, gas turbine interlocking compressor start and stop debugging and instrument assembly performance testing.

5. The method according to claim 4, characterized in that Perform gas turbine control compressor start and stop commissioning, including: Starting the gas engine, and during the operation of the gas engine, controlling the compressor to start and stop according to the operating state of the gas engine; Perform gas turbine interlocked compressor start and stop commissioning, including: After the start-stop commissioning of the gas engine controlling the compressor is successfully passed, the gas engine and the compressor are jointly operated according to the preset interlocking conditions and operating conditions; Perform instrument assembly performance testing including: After the start-stop debugging of the gas turbine interlocked compressor is successfully passed, the performance of the instrument assembly is tested by using air as the medium and controlling the gas turbine and the compressor to run jointly.

6. The method according to claim 1, characterized in that Perform gas ignition operation commissioning, including: Generate and output third instruction information to instruct the commissioning personnel to perform manual ignition commissioning on the gas engine; After the manual ignition debugging of the gas engine is successfully performed, the automatic program of the gas engine is tested and optimized in turn; After the test and optimization of the automatic program are successfully completed, controlling the gas turbine to be connected to the grid and controlling the gas turbine to operate continuously; Execute power generation grid connection commissioning, including: Execute constant power grid-connected mode debugging, and after successful debugging, perform equal-proportional grid-connected mode debugging.

7. The method according to claim 6, characterized in that Before testing and optimizing the automatic program of the combustion engine in sequence, the method further includes: remotely start and stop the gas engine; After the manual ignition debugging of the gas engine is successful, the automatic program of the gas engine is tested and optimized in sequence, including: After the manual ignition debugging and remote start-stop debugging of the gas engine are successfully performed, the automatic program of the gas engine is tested and optimized in turn.

8. An offshore turbine generator unit commissioning device, characterized in that: include: A first debugging unit, used for debugging the compressor supporting equipment and the compressor; The second debugging unit is used to debug the gas turbine supporting equipment; The third debugging unit is used to perform the debugging of the gas turbine combined compressor, the gas ignition operation debugging and the power generation grid connection debugging in sequence after the debugging of the compressor supporting equipment, the compressor and the gas turbine supporting equipment is successfully passed, so as to complete the debugging of the offshore turbine generator set.

9. A computer device, characterized in that: include: A memory and a processor, wherein the memory and the processor are communicatively connected to each other, the memory stores computer instructions, and the processor executes the offshore turbine generator set commissioning method according to any one of claims 1 to 7 by executing the computer instructions.

10. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores computer instructions, and the computer instructions are used to enable a computer to execute the offshore turbine generator set commissioning method according to any one of claims 1 to 7.

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