Gas turbine generator set

Abstract

The utility model discloses a gas turbine generator set, and relates to the field of power generation equipment. A gas turbine generator set comprises a gas turbine, a generator, a fan set, a first vehicle body and a second vehicle body. The first vehicle body is provided with a gas turbine ventilation cabin and a power generator ventilation cabin, the gas turbine is arranged in the gas turbine ventilation cabin, the power generator is arranged in the power generator ventilation cabin, the second vehicle body is provided with a ventilation air inlet cabin and a gas turbine air inlet cabin, at least part of the fan set is arranged in the ventilation air inlet cabin, and at least part of the fan set is arranged in the power generator ventilation cabin. The fan set is provided with a second air outlet and a third air outlet, the gas turbine air inlet cabin is communicated with an air inlet of the gas turbine through a first air pipe, the second air outlet is communicated with the gas turbine ventilation cabin through a second air pipe, and the third air outlet is communicated with the generator ventilation cabin through a third air pipe. The problems that a vehicle body is large in load, large in width size and the like can be solved at least.

Description

Technical Field

[0001] This application belongs to the technical field of power generation equipment, specifically relating to a gas turbine generator set. Background Technology

[0002] The gas turbine generator set in the relevant technology includes a gas turbine, a generator and other devices, and these devices are all installed on the same vehicle body, which results in a large load on the vehicle body, making the design and manufacturing requirements of the vehicle body more stringent. In addition, in order to support all the devices of the gas turbine generator set at the same time, the width of the vehicle body needs to be very large, which cannot meet the road transport regulations. Utility Model Content

[0003] The purpose of this application is to provide a gas turbine generator set that can solve problems such as heavy vehicle load and large width.

[0004] To solve the above-mentioned technical problems, this application is implemented as follows:

[0005] This application provides a gas turbine generator set, including: a gas turbine, a generator, a wind turbine unit, a first vehicle body, and a second vehicle body;

[0006] The first vehicle body is equipped with a gas turbine ventilation compartment and a generator ventilation compartment. The gas turbine is located in the gas turbine ventilation compartment, and the generator is located in the generator ventilation compartment.

[0007] The second vehicle body is provided with a ventilation air intake compartment and a gas turbine air intake compartment. At least part of the wind turbine unit is located in the ventilation air intake compartment. The wind turbine unit has a second air outlet and a third air outlet. The gas turbine air intake compartment is connected to the air inlet of the gas turbine through a first air pipe. The second air outlet is connected to the gas turbine ventilation compartment through a second air pipe. The third air outlet is connected to the generator ventilation compartment through a third air pipe.

[0008] In this embodiment, the gas turbine, generator, and other devices are carried on a first vehicle body, while the wind turbine and other devices are carried on a second vehicle body, achieving a dual-vehicle mounting system. This reduces the load on each vehicle body, lowers the design and manufacturing requirements, and also allows for a smaller vehicle width to comply with road transport regulations. Furthermore, when the gas turbine generator set is operating, gas needs to be supplied to the gas turbine, and ventilation is required for both the gas turbine and the generator. Based on this, the first vehicle body in this embodiment is provided with a gas turbine ventilation compartment and a generator ventilation compartment, and the second vehicle body can be provided with a ventilation intake compartment and a gas turbine intake compartment. Thus, the fan unit can connect the gas turbine intake compartment and the gas turbine intake port through a first air pipe to supply gas to the gas turbine, ensuring its normal operation. The fan unit can also connect the second outlet and the gas turbine ventilation compartment through a second air pipe to introduce gas into the gas turbine ventilation compartment, thereby ventilating the area around the gas turbine and achieving a cooling effect. Furthermore, the fan unit can connect the third outlet and the generator ventilation compartment through a third air pipe to introduce gas into the generator ventilation compartment, thereby ventilating the area around the generator and achieving a cooling effect. Attached Figure Description

[0009] Figure 1 This is a schematic diagram of the first and second vehicle bodies disclosed in the embodiments of this application;

[0010] Figure 2 This is a first schematic diagram of the first vehicle body disclosed in the embodiments of this application;

[0011] Figure 3 This is a second schematic diagram of the first vehicle body disclosed in the embodiments of this application;

[0012] Figure 4 This is a first schematic diagram of the second vehicle body disclosed in an embodiment of this application;

[0013] Figure 5 This is a second schematic diagram of the second vehicle body disclosed in the embodiments of this application;

[0014] Figure 6 This is a third schematic diagram of the second vehicle body disclosed in the embodiments of this application;

[0015] Figure 7 This is a schematic diagram of the structure of the first vehicle body disclosed in an embodiment of this application;

[0016] Figure 8 This is a schematic diagram of the lubrication path, gas turbine, generator, gearbox, first heat dissipation assembly, and second heat dissipation assembly disclosed in the embodiments of this application.

[0017] Explanation of reference numerals in the attached figures:

[0018] 01-Gas turbine;

[0019] 02-Generator;

[0020] 03-Gearbox;

[0021] 04-Lubrication path;

[0022] 05-First vehicle body; 051-Gas turbine ventilation compartment; 052-Generator ventilation compartment; 053-Non-high voltage engine compartment; 054-High voltage engine compartment;

[0023] 06-Second vehicle body; 061-Air intake compartment; 061a-Ventilation air intake compartment; 061b-Gas turbine air intake compartment; 0611-Block; 0611a-First accommodating space; 0611b-Second accommodating space; 0612-Gas turbine air intake filter; 0613-Generator air intake filter; 0614-Air intake filter; 0615-Air outlet filter; 0616-Gas turbine air outlet filter; 0617-Generator air outlet filter; 062-Transformer compartment;

[0024] 07-Wind turbine unit; 071-First wind turbine; 072-Second wind turbine;

[0025] 081 - First trachea; 082 - Second trachea; 083 - Third trachea;

[0026] 11-Fuel tank;

[0027] 121 - First oil pump; 122 - Second oil pump;

[0028] 13-First oil circuit;

[0029] 14-Second oil line;

[0030] 15-Thermostat;

[0031] 161 - First control valve; 162 - Second control valve;

[0032] 20 - First heat dissipation component;

[0033] 30 - Second heat dissipation component. Detailed Implementation

[0034] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0035] The terms "first," "second," etc., used in the specification and claims of this application are used to distinguish similar objects and not to describe a specific order or sequence. It should be understood that such use of data can be interchanged where appropriate so that embodiments of this application can be implemented in orders other than those illustrated or described herein, and the objects distinguished by "first," "second," etc., are generally of the same class and the number of objects is not limited; for example, a first object can be one or more. Furthermore, in the specification and claims, "and / or" indicates at least one of the connected objects, and the character " / " generally indicates that the preceding and following objects are in an "or" relationship.

[0036] The embodiments of this application will be described in detail below with reference to the accompanying drawings and specific examples and application scenarios.

[0037] refer to Figures 1 to 8 This application discloses a gas turbine generator set, which includes a gas turbine 01, a generator 02, a wind turbine 07, a first vehicle body 05, and a second vehicle body 06. The gas turbine 01 is the power component, providing power to the generator 02 to drive its operation and generate electricity. The generator 02 converts kinetic energy into electrical energy to output electrical energy. The wind turbine 07 supplies gas to the gas turbine 01 and the generator 02 to meet their respective operating requirements.

[0038] refer to Figure 2 and Figure 3 The first vehicle body 05 may be equipped with a gas turbine ventilation compartment 051 and a generator ventilation compartment 052, wherein the gas turbine 01 is located in the gas turbine ventilation compartment 051 and the generator 02 is located in the generator ventilation compartment 052. Based on this, the first vehicle body 05 can support the gas turbine 01 and the generator 02, and the gas turbine 01 can be ventilated through the gas turbine ventilation compartment 051 and the generator 02 can be ventilated through the generator ventilation compartment 052.

[0039] The second vehicle body 06 may be equipped with a ventilation intake compartment 061a and a gas turbine intake compartment 061b. At least a portion of the wind turbine assembly 07 is located in the ventilation intake compartment 061a, so that the second vehicle body 06 can support at least a portion of the wind turbine assembly 07. The wind turbine assembly 07 may have a second air outlet and a third air outlet. The gas turbine intake compartment 061b is connected to the air inlet of the gas turbine 01 via a first air pipe 081, the second air outlet is connected to the gas turbine ventilation compartment 051 via a second air pipe 082, and the third air outlet is connected to the generator ventilation compartment 052 via a third air pipe 083.

[0040] Based on the above configuration, gas can sequentially enter the gas turbine 01 through the gas turbine inlet compartment 061b, the first gas pipe 081, and the gas turbine 01 inlet to ensure gas supply and guarantee the gas required for the operation of the gas turbine 01. The gas generated by the fan unit 07 can sequentially enter the gas turbine ventilation compartment 051 through the second outlet and the second gas pipe 082 to ventilate the gas turbine ventilation compartment 051 and meet the heat dissipation requirements of the gas turbine 01 in the gas turbine ventilation compartment 051. The gas generated by the fan unit 07 can also sequentially enter the generator ventilation compartment 052 through the third outlet and the third gas pipe 083 to ventilate the generator ventilation compartment 052 and meet the heat dissipation requirements of the generator 02 in the generator ventilation compartment 052.

[0041] In this embodiment, the gas turbine 01, generator 02 and other devices are carried by the first vehicle body 05, and the wind turbine 07 and other devices are carried by the second vehicle body 06, thereby realizing the dual-vehicle loading method of the first vehicle body 05 and the second vehicle body 06. This can reduce the load of each vehicle body, reduce the design and manufacturing requirements of the vehicle body, and also reduce the width of the vehicle body to comply with road transport regulations.

[0042] refer to Figure 5 and Figure 6 In some embodiments, the second vehicle body 06 may be provided with an air intake compartment 061, and the fan unit 07 may be located in the air intake compartment 061, so as to accommodate and install the fan unit 07 through the air intake compartment 061. The air intake compartment 061 may be a whole or may include multiple independent sub-compartments, which may be selected according to the actual working conditions.

[0043] In some embodiments, the main air intake compartment 061 can be divided into a ventilation air intake compartment 061a and a gas turbine air intake compartment 061b. The gas turbine air intake compartment 061b may have an exhaust filter port 0615, and the ventilation air intake compartment 061a may have a gas turbine exhaust filter port 0616 and a generator exhaust filter port 0617. The exhaust filter port 0615 is connected to a first air pipe 081, the gas turbine exhaust filter port 0616 is connected to a second exhaust port and a second air pipe 082, and the generator exhaust filter port 0617 is connected to a third exhaust port and a third air pipe 083.

[0044] Based on the above configuration, the exhaust filter 0615, the first air pipe 081, and the gas turbine 01 can be connected in sequence to supply air to the gas turbine 01; the second exhaust port, the gas turbine exhaust filter 0616, the second air pipe 082, and the gas turbine ventilation compartment 051 can be connected in sequence to dissipate heat from the gas turbine 01; and the third exhaust port, the generator exhaust filter 0617, the third air pipe 083, and the generator ventilation compartment 052 can be connected in sequence to dissipate heat from the generator 02.

[0045] Optionally, the first air pipe 081, the second air pipe 082, and the third air pipe 083 can all be flexible tubes that can deform to adapt to the relative positions of the first vehicle body 05 and the second vehicle body 06.

[0046] Continue to refer to Figure 6 In some embodiments, the ventilation intake chamber 061a is provided with a partition 0611, which can divide the ventilation intake chamber 061a into a first accommodating space 0611a and a second accommodating space 0611b arranged vertically.

[0047] Additionally, the fan unit 07 may include a first fan 071 and a second fan 072. The first fan 071 is located in the first accommodating space 0611a and has a second air outlet; the second fan 072 is located in the second accommodating space 0611b and has a third air outlet.

[0048] Based on the above configuration, gas can be supplied to the gas turbine ventilation compartment 051 through the second outlet and the second air pipe 082 under the action of the first fan 071, thereby ventilating the gas turbine 01; and gas can be supplied to the generator ventilation compartment 052 through the third outlet and the third air pipe 083 under the action of the second fan 072, thereby ventilating the generator 02. Furthermore, arranging the first fan 071 and the second fan 072 vertically allows for full utilization of the space in the height direction of the second vehicle body 06, which is beneficial for reducing the length of the second vehicle body 06.

[0049] In some embodiments, the fan unit 07 may further include a third fan disposed within the gas turbine inlet compartment 061b, the third fan having a first outlet connected to a first gas pipe 081. Based on this arrangement, under the action of the third fan, gas is supplied to the gas turbine 01 through the first outlet and the first gas pipe 081, thereby achieving gas supply to the gas turbine 01.

[0050] refer to Figure 2 and Figure 8 In some embodiments, the gas turbine generator set may further include a lubrication path 04, at least a portion of which is located on the first vehicle body 05, for supplying lubricating oil to the gas turbine 01 and the generator 02 to achieve lubrication and cooling of the gas turbine 01 and the generator 02.

[0051] Considering that components such as gas turbine 01 and generator 02 can generate heat during operation, and that the lubricating oil absorbs some of the heat as it passes through these components, the lubricating oil can achieve a cooling effect on these components. At the same time, the temperature of the lubricating oil that absorbs heat is increased.

[0052] To achieve heat dissipation of the lubricating oil, such as Figure 8 As shown, the lubrication path 04 may further include a first heat dissipation assembly 20, which is disposed on the second vehicle body 06 and connected to the lubrication path 04, so that the lubricating oil transmitted by the lubrication path 04 enters the first heat dissipation assembly 20 and is cooled by the first heat dissipation assembly 20. Based on this configuration, the heat in the lubricating oil is dissipated by the first heat dissipation assembly 20 to obtain lubricating oil with a lower temperature, thereby allowing continued lubrication and cooling of components such as the gas turbine 01 and the generator 02. Optionally, the first heat dissipation assembly 20 may include a first radiator.

[0053] Considering that the gas inlet of the gas turbine generator set is prone to icing under some low-temperature conditions, the ice layer will reduce the cross-sectional area of ​​the gas inlet, affecting the normal gas supply of the gas turbine generator set, which will have an adverse impact on the normal operation of the gas turbine generator set.

[0054] Based on the above, in this embodiment of the application, the first heat dissipation component 20 can be installed at the gas inlet of the gas turbine generator set, so as to dissipate heat to the area where the gas inlet is located through the first heat dissipation component 20, thereby raising the temperature of the area and effectively alleviating the problem of icing at the gas inlet.

[0055] refer to Figure 5 and Figure 6 In some embodiments, the gas turbine generator set's air inlet may include an air inlet filter 0614 located in the gas turbine air inlet compartment 061b, a gas turbine air inlet filter 0612 located in the ventilation air inlet compartment 061a, and a generator air inlet filter 0613 located in the ventilation air inlet compartment 061a. The first heat dissipation component 20 is located at the air inlet filter 0614, the gas turbine air inlet filter 0612, and the generator air inlet filter 0613. Specifically, the gas can enter the gas turbine intake compartment 061b through the air inlet filter 0614, facilitating its subsequent delivery to the gas turbine 01 and ensuring the necessary gas supply for its operation. The gas can also enter the ventilation intake compartment 061a through the gas turbine intake filter 0612, allowing for ventilation of the surrounding environment and providing some cooling to the gas turbine 01. Finally, the gas can enter the ventilation intake compartment 061a through the generator intake filter 0613, facilitating ventilation of the surrounding environment and providing some cooling to the generator 02.

[0056] In this embodiment, by placing the first heat dissipation component 20 at the air inlet filter 0614, the gas turbine air inlet filter 0612, and the generator air inlet filter 0613, the heat from the lubricating oil with a certain temperature transferred to the first heat dissipation component 20 via the heat dissipation path 10 can be diffused to the air inlet filter 0614, the gas turbine air inlet filter 0612, and the generator air inlet filter 0613 respectively. This effectively prevents air from merging at the air inlet filter 0614, the gas turbine air inlet filter 0612, and the generator air inlet filter 0613, ensuring normal air intake and ventilation of the gas turbine 01 and normal ventilation of the generator 02.

[0057] Continue to refer to Figure 8 In some embodiments, the lubrication path 04 may include an oil tank 11, a first oil pump 121, a second oil pump 122, a first oil passage 13, and a second oil passage 14. The inlet ends of the first oil passage 13 and the second oil passage 14 are respectively connected to the outlet of the oil tank 11, the outlet end of the first oil passage 13 is connected to the inlet of the oil tank 11, and the outlet end of the second oil passage 14 is connected to the first oil passage 13. At least a portion of the first oil passage 13 extends to the second vehicle body 06 and is connected to the first cooling assembly 20. Components such as the gas turbine 01 and the generator 02 can be respectively connected to the first oil passage 13, and are all located downstream of the junction of the second oil passage 14 and the first oil passage 13. Furthermore, the first oil pump 121 is located on the first vehicle body 05 and connected to the first oil passage 13, and the second oil pump 122 is located on the first vehicle body 05 and connected to the second oil passage 14.

[0058] Based on the above configuration, under the action of the first oil pump 121, the lubricating oil in the oil tank 11 can enter the first oil passage 13 and flow from the inlet end to the outlet end of the first oil passage 13; under the action of the second oil pump 122, the lubricating oil in the oil tank 11 can enter the second oil passage 14 and flow into the first oil passage 13 through the outlet end of the second oil passage 14. Therefore, lubricating oil can be supplied to components such as the gas turbine 01 and the generator 02 through the first oil passage 13, achieving lubrication of these components and also providing a cooling effect.

[0059] It should be noted that the first oil pump 121 can be the main oil pump, and the second oil pump 122 can be an auxiliary oil pump or an emergency oil pump. Under normal circumstances, the first oil pump 121 can be started to supply lubricating oil to components such as the gas turbine 01 and the generator 02 through the first oil circuit 13, thereby achieving lubrication and cooling for the three components respectively. When the first oil pump 121 fails, the second oil pump 122 can be started to deliver lubricating oil to the first oil circuit 13 through the second oil circuit 14, and then supply lubricating oil to components such as the gas turbine 01 and the generator 02 through the first oil circuit 13, thereby achieving lubrication and cooling for both components respectively.

[0060] Of course, in other embodiments, in order to increase the supply flow of lubricating oil, the first oil pump 121 and the second oil pump 122 can also work together. In this case, the lubricating oil pumped by the first oil pump 121 and the lubricating oil pumped by the second oil pump 122 can merge in the first oil passage 13 and flow together to the gas turbine 01 and the generator 02 and other components, so as to lubricate and cool them respectively.

[0061] To further improve the cooling effect on the lubricating oil, the gas turbine generator set may also include a second cooling component 30, so that the second cooling component 30 and the first cooling component 20 work together to achieve the cooling effect on the lubricating oil and improve the cooling efficiency.

[0062] The second heat dissipation component 30 can be disposed on the second vehicle body 06, and a portion of the lubrication path 04 extends to the second vehicle body 06 and connects to the second heat dissipation component 30. Based on this, lubricating oil that absorbs heat can be supplied to the second heat dissipation component 30 through the lubrication path 04, and the second heat dissipation component 30 can dissipate some of the heat from the lubricating oil, achieving a heat dissipation effect on the lubricating oil and effectively preventing the lubricating oil from overheating and deteriorating, as well as affecting the cooling effect on components such as the gas turbine 01 and the generator 02. Optionally, the second heat dissipation component 30 may include a second radiator.

[0063] Optionally, the second heat dissipation component 30 and the first heat dissipation component 20 can be connected in parallel.

[0064] Optionally, the first oil circuit 13 may include two branch oil circuits, one of which is connected to the first heat dissipation component 20 and the other is connected to the second heat dissipation component 30. One branch oil circuit is provided with a first control valve 161 and the other branch oil circuit is provided with a second control valve 162, so as to control the lubricating oil flowing into the first heat dissipation component 20 and the second heat dissipation component 30 through the cooperation of the first control valve 161 and the second control valve 162.

[0065] In addition, the oil outlets of the two branch oil circuits can be connected to thermostats 15 to adjust the lubricating oil in the first heat dissipation assembly 20 and the second heat dissipation assembly 30 according to the thermostats 15.

[0066] To achieve power transmission, the gas turbine generator set may also include a gearbox 03, which is located on the first vehicle body 05 and is connected to the gas turbine 01 and the generator 02. In this way, during the operation of the gas turbine 01, the gearbox 03 can be driven to move, and the gearbox 03 can drive the generator 02 to operate, so as to generate electricity through the operation of the generator 02.

[0067] Optionally, gearbox 03 can be a gear-type reduction gearbox, etc.

[0068] Furthermore, the gearbox 03 can also be connected to the lubrication path 04 to supply lubricating oil to the gearbox 03 through the lubrication path 04 and to cool the gearbox 03.

[0069] refer to Figure 2 and Figure 3 In some embodiments, the first vehicle body 05 may also include a non-high-voltage engine compartment 053 and a high-voltage engine compartment 054 arranged along the length of the first vehicle body 05. The non-high-voltage engine compartment 053 may contain medium-voltage electrical cabinets and low-voltage electrical cabinets, while the high-voltage engine compartment 054 may contain high-voltage electrical cabinets. This arrangement separates the high-voltage electrical cabinets from the low-voltage and medium-voltage electrical cabinets, thereby preventing electrical injuries to maintenance personnel during operation. For example, the non-high-voltage engine compartment 053 and the high-voltage engine compartment 054 may be spaced apart along the length of the first vehicle body 05.

[0070] It should be noted that the voltage of the high-voltage electrical cabinet is higher than that of the medium-voltage electrical cabinet, and the voltage of the medium-voltage electrical cabinet is higher than that of the low-voltage electrical cabinet. The high-voltage electrical cabinet, medium-voltage electrical cabinet and low-voltage electrical cabinet in the embodiments of this application are intended to indicate the relative voltage between each electrical cabinet, and do not represent that the voltage of each electrical cabinet is absolutely high voltage, medium voltage and low voltage respectively.

[0071] In some embodiments, the voltage corresponding to the high-voltage electrical cabinet can be higher than 35KV, the voltage corresponding to the medium-voltage electrical cabinet can be higher than 1KV and lower than 35KV, and the voltage corresponding to the low-voltage electrical cabinet can be lower than 1KV. Of course, other forms are also possible, and no specific limitation is made here.

[0072] In addition, such as Figure 5 and Figure 6As shown, the second vehicle body 06 may also be provided with a transformer compartment 062, which may be equipped with a transformer cabinet. The transformer cabinet is connected to at least one of the low-voltage electrical cabinet, medium-voltage electrical cabinet and high-voltage electrical cabinet via cables to realize the transmission of electrical energy and signals.

[0073] refer to Figure 7 In some embodiments, the first vehicle body 05 may employ a load-bearing frame, which is at least composed of non-carbon steel beams and carbon steel beams. Based on this configuration, the load-bearing capacity of the first vehicle body 05 can be improved using a load-bearing frame, and it also helps to reduce the weight of the load-bearing frame, lowering the risk of overweight. Compared to welded carbon steel frames in related technologies, it has the advantage of lightweight design while maintaining load-bearing capacity.

[0074] The embodiments of this application have been described above with reference to the accompanying drawings. However, this application is not limited to the specific embodiments described above. The specific embodiments described above are merely illustrative and not restrictive. Those skilled in the art can make many other forms under the guidance of this application without departing from the spirit and scope of the claims, and all of these forms are within the protection scope of this application.

Claims

1. A gas turbine generator set, characterized in that, include: Gas turbine (01), generator (02), wind turbine (07), first car body (05), and second car body (06); The first vehicle body (05) is provided with a gas turbine ventilation compartment (051) and a generator ventilation compartment (052). The gas turbine (01) is located in the gas turbine ventilation compartment (051), and the generator (02) is located in the generator ventilation compartment (052). The second vehicle body (06) is provided with a ventilation intake compartment (061a) and a gas turbine intake compartment (061b). At least a portion of the fan unit (07) is located in the ventilation intake compartment (061a). The fan unit (07) has a second air outlet and a third air outlet. The gas turbine intake compartment (061b) is connected to the air inlet of the gas turbine (01) through a first air pipe (081). The second air outlet is connected to the gas turbine ventilation compartment (051) through a second air pipe (082). The third air outlet is connected to the generator ventilation compartment (052) through a third air pipe (083).

2. The gas turbine generator set according to claim 1, characterized in that, The gas turbine intake compartment (061b) has an exhaust filter port (0615), the ventilation intake compartment (061a) has a gas turbine exhaust filter port (0616) and a generator exhaust filter port (0617), the exhaust filter port (0615) is connected to the first air pipe (081), the gas turbine exhaust filter port (0616) is connected to the second exhaust port and the second air pipe (082), and the generator exhaust filter port (0617) is connected to the third exhaust port and the third air pipe (083).

3. The gas turbine generator set according to claim 2, characterized in that, The ventilation intake chamber (061a) is provided with a partition (0611), which divides the ventilation intake chamber (061a) into a first accommodating space (0611a) and a second accommodating space (0611b) arranged vertically. The fan unit (07) includes a first fan (071) and a second fan (072). The first fan (071) is located in the first accommodating space (0611a) and has a second air outlet. The second fan (072) is located in the second accommodating space (0611b) and has the third air outlet.

4. The gas turbine generator set according to claim 2, characterized in that, The wind turbine unit (07) also includes a third wind turbine located in the gas turbine intake compartment (061b), the third wind turbine having a first air outlet connected to the first air pipe.

5. The gas turbine generator set according to any one of claims 2 to 4, characterized in that, The gas turbine generator set also includes a lubrication path (04) and a first heat dissipation component (20). At least a portion of the lubrication path (04) is provided in the first vehicle body (05) for supplying lubricating oil to the gas turbine (01) and the generator (02); The first heat dissipation component (20) is disposed on the second vehicle body (06) and located at the gas inlet of the gas turbine generator set. The first heat dissipation component (20) is connected to the lubrication path (04) so ​​that the lubricating oil transmitted by the lubrication path (04) enters the first heat dissipation component (20) and dissipates heat to the gas inlet of the gas turbine generator set via the first heat dissipation component (20).

6. The gas turbine generator set according to claim 5, characterized in that, The gas turbine generator set includes an air inlet filter (0614) located in the gas turbine air inlet compartment (061b) and a gas turbine air inlet filter (0612) and a generator air inlet filter (0613) located in the ventilation air inlet compartment (061a). The first heat dissipation component (20) is respectively located at the air inlet filter (0614), the gas turbine air inlet filter (0612) and the generator air inlet filter (0613).

7. The gas turbine generator set according to claim 5, characterized in that, The lubrication path (04) includes an oil tank (11), a first oil pump (121), a second oil pump (122), a first oil passage (13), and a second oil passage (14); The oil inlet of the first oil passage (13) and the second oil passage (14) are respectively connected to the oil outlet of the oil tank (11). The oil outlet of the first oil passage (13) is connected to the oil inlet of the oil tank (11). The oil outlet of the second oil passage (14) is connected to the first oil passage (13). At least a portion of the first oil passage (13) extends to the second vehicle body (06) and is connected to the first heat dissipation component (20). The first oil pump (121) is located on the first vehicle body (05) and connected to the first oil circuit (13); The second oil pump (122) is located on the first vehicle body (05) and connected to the second oil circuit (14); The gas turbine (01) and the generator (02) are respectively connected to the first oil circuit (13), and are both located in the downstream area of ​​the junction of the second oil circuit (14) and the first oil circuit (13).

8. The gas turbine generator set according to any one of claims 2 to 4, characterized in that, The gas turbine generator set also includes a lubrication path (04) and a second heat dissipation component (30). The second heat dissipation component (30) is disposed on the second vehicle body (06); The lubrication path (04) extends partially to the second vehicle body (06) and is connected to the second heat dissipation assembly (30).

9. The gas turbine generator set according to claim 5, characterized in that, The gas turbine generator set also includes a gearbox (03), which is located on the first vehicle body (05) and is connected in a transmission manner between the gas turbine (01) and the generator (02); The lubrication path (04) is also used to supply lubricating oil to the gearbox (03).

10. The gas turbine generator set according to claim 1, characterized in that, The first vehicle body (05) is also provided with a non-high voltage engine compartment (053) and a high voltage engine compartment (054) arranged along the length direction of the first vehicle body (05). The non-high voltage engine compartment (053) is provided with a medium voltage electrical cabinet and a low voltage electrical cabinet, and the high voltage engine compartment (054) is provided with a high voltage electrical cabinet. The second vehicle body (06) is also provided with a transformer compartment (062), which is equipped with a transformer cabinet. The transformer cabinet is connected to at least one of the low-voltage electrical cabinet, the medium-voltage electrical cabinet and the high-voltage electrical cabinet via a cable.

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