Roof structure and unmanned aerial vehicle command vehicle

Abstract

The utility model discloses a roof structure and an unmanned aerial vehicle command vehicle, and belongs to the technical field of unmanned aerial vehicles. The problem that after the lifting type data chain communication antenna is lifted, the roof of an existing unmanned aerial vehicle command vehicle is open, and consequently the interior of a compartment is in a severe environment is solved. The top cover comprises a top cover main body and a covering unit, the top cover body comprises a top cover capable of being opened and closed and a through hole penetrating through the top cover in the vehicle height direction. The covering unit comprises a covering piece and a telescopic piece which are connected in sequence; the telescopic piece is also connected with the top cover; through stretching and retracting of the telescopic piece, the covering piece rotates around the hinged point where the covering piece is hinged to the top cover, and the through hole is covered. Opening and closing of the roof are achieved through opening and closing of the top cover, and when the roof is in an open state, an access channel is provided for entering and exiting of equipment in a compartment; when the roof is in a closed state, the internal space of the carriage is independent and is prevented from being interfered by the external environment.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a roof structure and an unmanned aerial vehicle command vehicle. Background Art

[0002] As the command center of the unmanned aerial vehicle, the unmanned aerial vehicle command vehicle can quickly set up a command center with its flexible mobility. It receives the real-time dynamics collected by the unmanned aerial vehicle on site through a vehicle-mounted antenna, so as to realize temporary command work, and can synchronously send the collected on-site data to a remote control center in time.

[0003] To realize the signal transmission between the unmanned aerial vehicle command vehicle and the unmanned aerial vehicle, at present, a collapsible data link communication antenna needs to be installed on the roof of the unmanned aerial vehicle command vehicle or a lifting data link communication antenna needs to be installed inside the carriage of the unmanned aerial vehicle command vehicle. Among them, the collapsible data link communication antenna will limit the height of the antenna from the ground, and the communication range of the unmanned aerial vehicle is small. For the unmanned aerial vehicle command vehicle equipped with a lifting antenna, although the communication range of the unmanned aerial vehicle can be increased, during the process of antenna lifting and the working process of the unmanned aerial vehicle command vehicle, the roof has been in an open state. When in harsh environments such as wind, frost, rain and snow, due to the open roof, the inside of the carriage is also in a harsh environment, which is not conducive to the normal progress of command work. Summary of the Utility Model

[0004] In view of the above analysis, the utility model aims to provide a roof structure and an unmanned aerial vehicle command vehicle to solve the problem that after the lifting data link communication antenna is lifted, the roof of the existing unmanned aerial vehicle command vehicle is open, resulting in a harsh environment inside the carriage.

[0005] The purpose of the utility model is mainly achieved through the following technical solutions:

[0006] The utility model provides a roof structure in the first aspect, which includes a top cover main body and a covering unit;

[0007] The top cover main body includes a top cover that can be opened and closed and a through hole that penetrates the top cover along the vehicle height direction;

[0008] The covering unit includes a covering member and a telescopic member connected in sequence;

[0009] The telescopic member is also connected to the top cover;

[0010] Through the telescopic movement of the telescopic member, the covering member rotates around the hinge point where the covering member is connected to the top cover to cover the through hole.

[0011] Further, the top cover includes a first top cover and a second top cover that can be hermetically connected to the first top cover.

[0012] Further, the through hole is a semi-hole arranged on the first top cover, and the notch of the semi-hole faces the side wall of the second top cover.

[0013] Furthermore, the width of the first top cover is greater than that of the second top cover.

[0014] Furthermore, the through hole includes a first half hole arranged on the first top cover and a second half hole arranged on the second top cover;

[0015] After the first top cover and the second top cover are closely attached, the first half hole and the second half hole are butted to form a through hole.

[0016] Furthermore, the covering member includes a top plate and a side plate group connected to the top plate;

[0017] The top plate is connected to the telescopic member;

[0018] The bottom of the side plate group can be hermetically connected to the top cover body.

[0019] Furthermore, the side plate group includes a first side plate;

[0020] The first side plate is hinged to the top cover.

[0021] The second aspect of the present utility model provides a drone command vehicle, including a carriage, a lifting antenna assembly, and a roof structure as described in the first aspect;

[0022] The roof structure is connected above the carriage;

[0023] The lifting antenna assembly includes a lifting rod;

[0024] The fixed end of the lifting rod is connected inside the carriage;

[0025] The telescopic end of the lifting rod extends out of the carriage. After the roof structure is closed, the lifting rod is located in the through hole, and the covering member abuts against the side wall of the lifting rod.

[0026] Furthermore, the carriage includes an antenna cabin;

[0027] The lifting antenna assembly is arranged in the antenna cabin;

[0028] The lifting rod is directly opposite to the through hole.

[0029] Furthermore, it further includes a drone command and control component;

[0030] The carriage further includes a command cabin;

[0031] The drone command and control component is arranged in the command cabin.

[0032] Compared with the prior art, the present utility model can at least achieve one of the following beneficial effects:

[0033] 1. In the present utility model, the opening and closing of the roof structure are realized through the opening and closing of the top cover. When the roof structure is in the open state, it provides an access passage for the entry and exit of equipment inside the carriage; when the roof structure is in the closed state, the interior space of the carriage is in an independent space, protected from external environmental interference.

[0034] 2. In the present utility model, by providing a through hole in the top cover, it provides an extension passage for the lifting rod that extends out of the roof structure when the roof structure is in the closed state.

[0035] 3. In the present utility model, by providing a covering unit, when the lifting rod does not extend out of the carriage, the covering member can cover the through hole, so as to avoid impurities such as rainwater and dust from entering the carriage when the roof structure is in the closed state. The rotation of the covering member is controlled by a telescopic member, so that when the lifting rod is inside the through hole, the covering member does not block the path where the lifting rod is located; also, by the covering member abutting against the lifting rod, part of the gap between the through hole and the lifting rod is blocked, reducing the entry of impurities such as rainwater and dust outside the carriage into the carriage.

[0036] In the present utility model, the above technical solutions can also be combined with each other to achieve more preferred combination schemes. Other features and advantages of the present utility model will be described in the subsequent specification, and some advantages can be made obvious from the specification, or understood by implementing the present utility model. The objectives and other advantages of the present utility model can be realized and obtained through the content specifically pointed out in the embodiments of the specification and the drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] The drawings are only for the purpose of showing specific embodiments, and are not considered to be a limitation of the present utility model. Throughout the drawings, the same reference signs represent the same components.

[0038] Figure 1 It is a schematic structural diagram of a roof structure in a closed state in the present utility model;

[0039] Figure 2 is Figure 1 a schematic structural diagram of the main body of the top cover in;

[0040] Figure 3 It is a schematic structural diagram after the covering unit is connected to the first top cover;

[0041] Figure 4 It is a schematic structural diagram of the covering member;

[0042] Figure 5 It is a schematic structural diagram of an unmanned aerial vehicle command vehicle in the present utility model;

[0043] Figure 6 is Figure 5Schematic top view of the UAV command vehicle when the roof structure is not installed;

[0044] Figure 7 Schematic structure of the UAV command vehicle when the data link communication antenna extends out of the carriage and the roof structure is open;

[0045] Figure 8 Schematic structure of the UAV command vehicle when the data link communication antenna extends out of the carriage and the roof structure is closed.

[0046] Reference numerals:

[0047] 100 - Roof cover main body, 200 - Covering unit; 110 - Roof cover, 120 - Through hole; 111 - First roof cover, 112 - Second roof cover; 210 - Covering member, 220 - Telescopic member, 230 - Fixed block; 211 - Top plate, 212 - Side plate group; 2121 - First side plate, 2122 - Third side plate; 1 - Carriage, 2 - Lifting antenna assembly, 3 - Roof structure, 4 - UAV command and control assembly, 5 - Lighting equipment, 6 - Vehicle head, 7 - Partition, 8 - Ladder, 9 - Air conditioner, 10 - Power supply equipment; 11 - Antenna compartment, 12 - Command compartment; 21 - Lifting rod, 22 - Data link communication antenna; 41 - Console, 42 - Cabinet, 43 - Control panel assembly, 44 - Display screen group; 431 - Panel main body, 432 - Control group; 4321 - Keyboard, 4322 - UAV control joystick; 441 - First display, 442 - Second display. Detailed implementation manners

[0048] The following will specifically describe the preferred embodiments of the present invention with reference to the accompanying drawings. The accompanying drawings form a part of the present invention and are used together with the embodiments of the present invention to explain the principle of the present invention, rather than to limit the scope of the present invention.

[0049] Embodiment 1

[0050] A specific embodiment of the present invention provides a roof structure, as shown in Figure 1 and Figure 2 which includes a roof cover main body 100 and a covering unit 200; the roof cover main body 100 includes an openable and closable roof cover 110 and a through hole 120 penetrating the roof cover 110 in the vehicle height direction; the covering unit 200 includes a covering member 210 and a telescopic member 220 connected in sequence; the telescopic member 220 is also connected to the roof cover 110; through the expansion and contraction of the telescopic member 220, the covering member 210 rotates around the hinge point where the covering member 210 is hinged to the roof cover 110 to cover the through hole 120.

[0051] In this embodiment, the opening and closing of the roof structure is realized by the opening and closing of the top cover 110. When the roof structure is in the open state, it provides an access passage for the entry and exit of equipment inside the carriage; when the roof structure is in the closed state, the interior space of the carriage is an independent space, protected from external environmental interference.

[0052] In this embodiment, a through hole 120 is provided on the top cover 110 to provide an extension passage for the lifting rod that extends out of the roof structure when the roof is in the closed state.

[0053] In this embodiment, by providing a covering unit 200, when the lifting rod does not extend out of the carriage, the covering member 210 can cover the through hole 120 to prevent impurities such as rainwater and dust from entering the carriage when the roof structure is in the closed state. The rotation of the covering member 210 is controlled by the telescopic member 220, so that when the lifting rod 21 is inside the through hole 120, the covering member 210 does not block the path where the lifting rod 21 is located; also, by the covering member 210 abutting against the lifting rod 21, part of the gap between the through hole 120 and the lifting rod 21 is blocked, reducing the entry of impurities such as rainwater and dust outside the carriage into the carriage.

[0054] Furthermore, the top cover 110 includes a first top cover 111 and a second top cover 112 that can be hermetically connected to the first top cover 111, as Figure 2 shown. The first top cover 111 and the second top cover 112 are respectively hinged to the top of the side wall of the carriage, and the opening and closing of the roof structure is completed by the flipping of the first top cover 111 and the second top cover 112.

[0055] Considering the airtightness of the roof structure in the closed state, a through groove is arranged on the second top cover 112; a connecting block matching the through groove is arranged on the first top cover 111, and the connecting block is inserted into the through groove and can be in close contact with the through groove. To facilitate water drainage of the through groove, the through groove is arranged along the length direction of the second top cover 112.

[0056] To facilitate the connection between the connecting end of the first top cover 111 and the through groove, the opening of the through groove is arranged upward.

[0057] Furthermore, considering that the main function of the through hole 120 is to accommodate the lifting rod that extends out of the roof structure when the roof is in the closed state, the top cover main body 100 is provided with a through hole 120 that penetrates the top cover 110 along the vehicle height direction. Among them, the setting method of the through hole 120 mainly includes:

[0058] The first setting of the through hole 120: The through hole 120 is a semi-hole arranged on the first top cover 111, and the notch of the semi-hole faces the side wall of the second top cover 112. After the first top cover 111 and the second top cover 112 are hermetically connected, the through hole 120 and the second top cover 112 are docked to form an extension passage, as Figure 2 and Figure 3As shown in the figure. Among them, considering the centering of the lifting antenna assembly 2 and the convenience of roof structure maintenance, the width of the first top cover 111 is greater than the width of the second top cover 112, so that the through hole 120 can be completely arranged on the first top cover 111.

[0059] The second setting of the through hole 120: The through hole 120 includes a first half hole and a second half hole. The first half hole is arranged on the first top cover 111, and the notch of the first half hole faces the side wall of the second top cover 112. The second half hole is arranged on the second top cover 112, and the notch of the second half hole faces the side wall of the first top cover 111. After the first top cover 111 and the second top cover 112 are closely attached, the first half hole and the second half hole are butted to form the through hole 120. When the through hole 120 is the second setting, it is preferably that the first half hole and the second half hole have the same size, and the first top cover 111 and the second top cover 112 have the same size, which is not only easy for the centering of the lifting antenna assembly 2, but also convenient for the processing and installation of the first top cover 111 and the second top cover 112. When the through hole 120 is the second setting, one or two covering units 200 are provided; when one covering unit 200 is provided, the covering unit 200 is arranged on the side of the first half hole or the second half hole. When two covering units 200 are provided, the two covering units 200 are arranged oppositely and are respectively arranged on the sides of the first half hole and the second half hole, and the two covering units 200 can cover the through hole 120 after combination.

[0060] In this embodiment, a half hole refers to a hole opened at the edge of the top cover and only half of it is left.

[0061] Furthermore, the covering member 210 includes a top plate 211 and a side plate group 212 connected to the top plate 211, as Figure 3 and Figure 4 shown; the top plate 211 is connected to the telescopic member 220; the top plate 211 is controlled by the telescopic member 220 to rotate around the hinge point. The side plate group 212 is hinged to the top cover main body 100 to form a hinge point for the covering member 210 to rotate.

[0062] In this embodiment, the bottom of the side plate group 212 can be hermetically connected to the top cover main body 100. Specifically: when the side plate group 212 is closely attached to the top cover main body 100, the side plate group 212 covers the through hole 120, so as to achieve the airtightness inside the carriage when the roof structure is in the closed state when the lifting antenna assembly 2 does not extend out of the roof structure.

[0063] To ensure the sealing performance when the side plate group 212 is closely attached to the top cover main body 100, a sealing strip is provided at the bottom of the side plate group 212.

[0064] In this embodiment, the cross-sectional shape of the side plate group 212 includes but is not limited to a square, as long as it can completely cover the through hole 120.

[0065] Exemplarily, the structure of the side plate group 212 is described with the cross-sectional shape of the side plate group 212 being square. The side plate group 212 includes a first side plate 2121, a second side plate, a third side plate 2122, and a fourth side plate that are sequentially connected end to end, as Figure 4 shown. Among them, the first side plate 2121 is hingedly connected to the top cover 110. Specifically: the first side plate 2121 is hingedly connected to the first top cover 111. The third side plate 2122 is disposed opposite to the first side plate 2121; the third side plate 2122 can extend into the through groove and be hermetically connected to the through groove. The second side plate and the fourth side plate are disposed opposite to each other and can be in close contact with the upper surface of the first top cover 111.

[0066] In this embodiment, the telescopic member 220 is preferably a pneumatic cylinder, which has a long service life.

[0067] In this embodiment, the covering member 210 further includes a fixing block 230. Through the fixing block 230, the fixed end of the telescopic member 220 is connected to the top cover 110, as Figure 3 shown.

[0068] Embodiment 2

[0069] Another specific embodiment of the present utility model discloses a drone command vehicle, which includes a carriage 1, a lifting antenna assembly 2, and a roof structure 3 as in Embodiment 1, as Figure 5 、 Figure 7 and Figure 8 shown; the roof structure 3 is connected above the carriage 1; the lifting antenna assembly 2 includes a lifting rod 21; the fixed end of the lifting rod 21 is connected inside the carriage 1; the telescopic end of the lifting rod 21 extends out of the carriage 1. After the roof structure 3 is closed, the lifting rod 21 is located in the through hole 120, and the covering member 210 abuts against the side wall of the lifting rod 21.

[0070] In this embodiment, the opening of the roof structure 3 provides an access channel for the lifting antenna assembly 2 to enter and exit the carriage 1, that is, when the first top cover 111 and the second top cover 112 are flipped and opened, the lifting antenna assembly 2 extends out of the carriage 1 from the exit after the roof structure 3 is opened, as Figure 7 shown. When it reaches the position, the first top cover 111 and the second top cover 112 are flipped and closed, the roof structure 3 is in a closed state, the lifting rod 21 is located in the through hole 120, as Figure 8 shown, the first top cover 111 and the second top cover 112 are in close contact, so that the internal environment of the carriage 1 is independent of the external environment and is not interfered by the external environment.

[0071] Compared with the existing UAV command vehicle with an inverted data link communication antenna installed on the roof, the antenna in the lifting antenna assembly 2 of this embodiment is installed in the car 1 and is lifted vertically. Because it is not installed on the roof and is not limited by the size of the inverted antenna, the height of the lifting rod 21 can be adjusted as needed, and the control range of the antenna can be adjusted, so that the UAV command vehicle of this embodiment can remotely control the UAV within a range of 150km.

[0072] Compared with the existing UAV command vehicle equipped with a liftable data link communication antenna, in this embodiment, after the antenna is extended out of the roof structure 3, the roof structure 3 can be closed, so that the internal environment of the vehicle is independent of the external environment and free from interference from the external environment, thereby improving the environmental adaptability of the UAV command vehicle.

[0073] Furthermore, the lifting antenna assembly 2 includes a lifting rod 21 and a data link communication antenna 22. Figure 7 and Figure 8 As shown, the telescopic end of the lifting rod 21 is connected to the data link communication antenna 22, and the fixed end of the lifting rod 21 is fixedly connected to the bottom plate of the carriage 1. The lifting height of the data link communication antenna 22 is controlled by the lifting rod 21.

[0074] In this embodiment, considering that the data link communication antenna 22 extends out of the compartment 1, in order to avoid the data link communication antenna 22 blocking the closing of the first top cover 111 and the second top cover 112, the distance that the data link communication antenna 22 extends out of the roof structure 3 is greater than or equal to the width of the first top cover 111. Specifically: when the first top cover 111 and the second top cover 112 are not opened or are fully opened, the lifting function of the lifting antenna assembly 2 is in a closed state and cannot be operated; when the first top cover 111 and the second top cover 112 are fully opened, the lifting rod 21 can be started, and the data link communication antenna 22 can be raised to a specified height before the first top cover 111 and the second top cover 112 can be flipped and closed. Among them, opening to the full extent means that the opening between the first top cover 111 and the second top cover 112 can allow the data link communication antenna 22 to pass smoothly. The data link communication antenna 22 is raised to a specified height, which means that the position of the data link communication antenna 22 and the lifting rod 21 will not block the flipping and closing of the first top cover 111 and the second top cover 112.

[0075] In this embodiment, the remote link is established through the data link communication antenna 22, which can not only remotely monitor and control the UAV, but also establish a connection with a remote control center.

[0076] Furthermore, the drone command vehicle in this embodiment further includes a drone command control component 4, a lighting device 5 and a power supply device 10 arranged in the vehicle compartment 1, such as Figure 5 and Figure 6 shown.

[0077] In this embodiment, the UAV command and control component 4 includes a console 41, a cabinet 42, a control panel component 43, and a display screen group 44, as Figure 5 shown; the cabinet 42 is arranged below the console 41, the control panel component 43 is connected to the side wall of the console 41, the control panel component 43 includes a panel main body 431 and a control group 432 arranged on the panel main body 431, and the control group 432 includes a keyboard 4321 and a UAV control joystick 4322, as Figure 6 shown. The display screen group 44 is arranged above the console 41, and the display screen group 44 includes a first display 441 and a second display 442, as Figure 5 shown, wherein, two first displays 441 are arranged side by side, the second display 442 is arranged above the first display 441, and four second displays 442 are arranged. The UAV command and control component 4 realizes the flight control of the UAV, specifically including completing the UAV route setting, flight data supervision, and real-time data processing, etc. Video conferencing can also be realized through the data link communication antenna 22 and the display screen group 44. Among them, preferably two groups of control groups are arranged, the cabinet 42 includes a 7U cabinet, and three cabinets are arranged side by side. The first display 441 is preferably a 23.8-inch display. The second display 442 is preferably a 10.1-inch display.

[0078] In this embodiment, the UAV command vehicle in this embodiment further includes seats arranged in the carriage 1, and the seats are arranged close to the control panel component 43 to facilitate the operator to work on the control panel component 43 in a sitting position. One seat corresponds to one UAV control station, and each UAV control station realizes the control of one UAV through one first display 441, two second displays 442, a set of keyboard 4321, and a set of UAV control joystick 4322.

[0079] In this embodiment, the lighting device 5 includes a lighting lamp and an emergency lamp arranged on the top of the carriage.

[0080] In this embodiment, the power supply device 10 includes a generator, preferably an ultrasonic generator.

[0081] Furthermore, in this embodiment, the UAV command vehicle further includes a vehicle head 6 connected to the carriage 1, wherein the carriage 1 includes an antenna cabin 11 and a command cabin 12 arranged from the rear of the vehicle to the vehicle head 6, as Figure 5 and Figure 6 shown.

[0082] In this embodiment, the vehicle head 6 includes a driving and seating area.

[0083] In this embodiment, the UAV command vehicle further includes a partition 7, as Figure 5As shown in the figure, in order to make the driving and riding area and the command cabin 12 have relatively independent spaces, a partition 7 is provided between the driving and riding area and the carriage 1.

[0084] In this embodiment, the roof structure 3 is arranged above the antenna cabin 11, the lift-type antenna assembly 2 is arranged in the antenna cabin 11, and the lift rod 21 is directly opposite to the through hole 120 to facilitate the extension of the antenna in the lift-type antenna assembly 2. The power supply device 10 is arranged in the antenna cabin 11 to make the command cabin 12 have a larger usable space.

[0085] In this embodiment, the lighting device 5 is installed on the top of the command cabin 12.

[0086] Furthermore, in this embodiment, the UAV command vehicle further includes a ladder 8. As Figure 5 shown, the ladder 8 is arranged on the side wall of the rear of the vehicle, and the roof can be climbed through the ladder 8.

[0087] Furthermore, in order to facilitate the operation personnel to rest and adjust the environment inside the carriage, the UAV command vehicle in this embodiment further includes a sofa, a shading curtain and an air conditioner 9. As Figure 5 shown, the shading curtain is arranged at the window of the carriage and is used to block the window. The sofa is arranged in the command cabin 12. The air conditioner 9 is installed on the top of the command cabin 12.

[0088] The above is only the preferred specific embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any changes or substitutions that can be easily thought of by those skilled in the art within the technical scope disclosed by the present utility model should be covered within the protection scope of the present utility model.

Claims

1. A roof structure, characterized in that: It comprises a top cover body (100) and a covering unit (200); The top cover body (100) comprises a top cover (110) that can be opened and closed and a through hole (120) that penetrates the top cover (110) along the vehicle height direction; The covering unit (200) comprises a covering member (210) and a telescopic member (220) which are connected in sequence; The telescopic member (220) is also connected to the top cover (110); Through the extension and retraction of the telescopic member (220), the covering member (210) rotates around a hinge point connecting the covering member (210) and the top cover (110) to cover the through hole (120).

2. The roof structure according to claim 1, characterized in that: The top cover (110) comprises a first top cover (111) and a second top cover (112) capable of being tightly connected to the first top cover (111).

3. The roof structure according to claim 2, characterized in that: The through hole (120) is a half hole arranged on the first top cover (111), and a notch of the half hole is arranged toward the side wall of the second top cover (112).

4. The roof structure according to claim 3, characterized in that: The width of the first top cover (111) is greater than the width of the second top cover (112).

5. The roof structure according to claim 2, characterized in that: The through hole (120) comprises a first half hole arranged on the first top cover (111) and a second half hole arranged on the second top cover (112); After the first top cover (111) and the second top cover (112) are in close contact, the first half hole and the second half hole are butted against each other to form the through hole (120).

6. The roof structure according to claim 1, characterized in that: The covering member (210) comprises a top plate (211) and a side plate group (212) connected to the top plate (211); The top plate (211) is connected to the telescopic member (220); The bottom of the side plate group (212) can be tightly connected to the top cover body (100).

7. The roof structure according to claim 6, characterized in that: The side plate group (212) comprises a first side plate (2121); The first side panel (2121) is hingedly connected to the top cover (110).

8. A UAV command vehicle, characterized in that: It comprises a vehicle compartment (1), a lifting antenna assembly (2) and a roof structure as claimed in any one of claims 1 to 7; The roof structure is connected above the vehicle compartment (1); The lifting antenna assembly (2) comprises a lifting rod (21); The fixed end of the lifting rod (21) is connected inside the carriage (1); The telescopic end of the lifting rod (21) extends out from the vehicle compartment (1); after the roof structure is closed, the lifting rod (21) is located in the through hole (120), and the covering member (210) abuts against the side wall of the lifting rod (21).

9. The UAV command vehicle according to claim 8, characterized in that: The carriage (1) comprises an antenna cabin (11); The lifting antenna assembly (2) is arranged in the antenna cabin (11); The lifting rod (21) is directly opposite to the through hole (120).

10. The UAV command vehicle according to claim 8, characterized in that: Also included is a UAV command and control component (4); The carriage (1) further comprises a command cabin (12); The UAV command and control component (4) is arranged in the command cabin (12).

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