Mobile unmanned aerial vehicle airport convenient to deploy quickly

Abstract

According to the mobile unmanned aerial vehicle airport convenient to deploy rapidly, a box body is arranged at the top of a vehicle body in a turnover mode, a traction arm is arranged on the side wall of the box body, a parking platform is composed of a top plate of the box body, four turnover plates and four splice plates, the turnover plates are arranged on the side wall of the box body in a turnover mode, and when the parking platform is unfolded, the turnover plates are horizontally arranged; the splice plates are detachably connected between the adjacent turnover plates; when the parking platform is folded, the splice plate is detached, and the turnover plate is vertically arranged; and the locking mechanism is arranged between the box body and the vehicle body. Through the structure of the vehicle body and the turnover box body, on one hand, the box body can be dragged by a tractor under the assistance of the vehicle body, and on the other hand, the parking platform can be in a horizontal state, so that take-off and landing of the unmanned aerial vehicle are facilitated, and an airport can quickly adapt to different terrain requirements along a railway; the mobile characteristic breaks through the power and terrain limitation of a fixed airport, can dynamically adjust the position according to the inspection requirements, reduces the invalid round-trip time of the unmanned aerial vehicle, and improves the effective inspection coverage rate.

Description

Technical Field

[0001] This application belongs to the field of unmanned aerial vehicle (UAV) technology, and more specifically, relates to a mobile UAV airport that is easy to deploy quickly. Background Technology

[0002] In the field of intelligent inspection of heavy-haul railways, drone swarm technology can significantly improve the inspection coverage and efficiency in large-scale scenarios through multi-drone collaborative operations. However, existing swarm systems mostly rely on fixed drone airports, whose deployment locations are limited by power supply and terrain conditions, making it difficult to dynamically adapt to the complex and ever-changing operational needs along railway lines. Especially in high-risk areas such as freight yards and high slopes, the static nature of fixed airports means that the drone's flight radius cannot fully cover the target area, requiring frequent returns to change batteries, resulting in an effective inspection time of less than 40%. Utility Model Content

[0003] The purpose of this application is to provide a mobile drone airport that is easy to deploy quickly, so as to extend the effective cruise time of drones.

[0004] To achieve the above objectives, the technical solution adopted in this application is as follows: A mobile unmanned aerial vehicle (UAV) airport that is easy to deploy quickly is provided, comprising a vehicle body, a container, a landing platform, and a locking mechanism. The container is rotatably mounted on top of the vehicle body, and a traction arm is provided on the side wall of the container for connecting to a towing vehicle. The landing platform consists of a top plate of the container, four rotatable plates, and four connecting plates. The rotatable plates are rotatably mounted on the side wall of the container. When the landing platform is deployed, the rotatable plates are horizontally arranged, and the connecting plates are detachably connected between adjacent rotatable plates. When the landing platform is retracted, the connecting plates are disassembled, and the rotatable plates are vertically arranged. The locking mechanism is located between the container and the vehicle body. When the locking mechanism is locked, the container is fixed relative to the vehicle body.

[0005] In one possible implementation, when the flip plate is arranged horizontally, a support rod is provided between the flip plate and the box body. One end of the support rod is detachably connected to the flip plate, and the other end of the support rod is detachably connected to the side wall of the box body.

[0006] In one possible implementation, the support rod has a first connecting shaft and a second connecting shaft at both ends, and the bottom of the flip plate has two first support blocks arranged at intervals. The first support blocks have a first support groove, and the opening of the first support groove is located on the side wall of the first support block away from the box body. The first support shaft is inserted into the first support groove. The side wall of the box body has two second support blocks arranged at intervals. The second support blocks have a second support groove, and the opening of the second support groove is located on the side wall of the second support block away from the box body. The second support shaft is inserted into the second support groove.

[0007] In one possible implementation, the first support block has a first support hole, and a bolt is screwed into the first support hole to hold the first support shaft in the first support groove; the second support block has a second support hole, and a bolt is screwed into the second support hole to hold the second support shaft in the second support groove.

[0008] In one possible implementation, two flip blocks are spaced apart near the top of each side wall of the housing. Each flip block has a flip hole. A pair of opposite side walls of the flip plate have flip shafts. The flip plate corresponds one-to-one with each set of flip blocks, and the flip shafts are inserted into the corresponding flip holes. The top surface of the flip plate has four splicing slots. One end of some of the splicing slots is flush with the left side wall of the flip plate, and one end of the remaining splicing slots is flush with the right side wall of the flip plate. The bottom surface of each splicing slot has a first threaded hole. Multiple splicing blocks are provided on two adjacent side walls of the splicing plate. Each splicing block corresponds one-to-one with a splicing slot. A splicing block on one side wall of the splicing plate is inserted into the corresponding splicing slot of one of the two adjacent flip plates, and a splicing block on the other side wall of the splicing plate is inserted into the corresponding splicing slot of the other of the two adjacent flip plates. Each splicing block has a second threaded hole. When the stop platform is unfolded, bolts are screwed into the corresponding first and second threaded holes.

[0009] In one possible implementation, the side wall of the housing is provided with four insertion holes, each corresponding to a splicing plate. The insertion holes are strip-shaped holes. When the stop platform is retracted, the disassembled splicing plate is inserted into the corresponding insertion hole, and a portion of the splicing plate is located outside the housing. The two sides of the housing are provided with fixing rods, and the two ends of the fixing rope are respectively fixed to the fixing rods. The fixing rope passes through the second threaded hole of the splicing plate to fix the splicing plate.

[0010] In one possible implementation, when the flip-up panels are arranged parallel to the side wall of the housing, cable ties are attached to the outer side of each flip-up panel.

[0011] In one possible implementation, the bottom of the box is provided with two first mounting plates, and a first adjusting shaft is provided between the first mounting plates. The top of the vehicle body is provided with two second mounting plates spaced apart, and the first adjusting shaft passes through the second mounting plates.

[0012] In one possible implementation, the locking mechanism includes two third mounting plates, a first locking shaft, a mounting rod, an adjusting rod, two fourth mounting plates, a mounting tube, and an adjusting tube. The two third mounting plates are spaced apart at the bottom of the housing; the first locking shaft is rotatably disposed between the two third mounting plates; the top end of the mounting rod is disposed on the first locking shaft; the adjusting rod is coaxially arranged with the mounting rod and rotatably disposed on the mounting rod; the two fourth mounting plates are spaced apart at the top of the vehicle body; the second locking shaft is rotatably disposed between the two fourth mounting plates; the bottom end of the mounting tube is disposed on the second locking shaft; the adjusting tube is coaxially arranged with the mounting tube and rotatably disposed on the mounting tube; a portion of the adjusting rod is screwed into the adjusting tube.

[0013] In one possible implementation, the vehicle body is provided with four support plates, which are located at the four corners of the vehicle body. Each support plate has a support hole, and a balance bar is screwed into the support hole. The balance bar can abut against the bottom surface or release from the bottom surface due to rotation.

[0014] The advantages of the mobile drone airport provided in this application, which facilitates rapid deployment, are as follows: Compared with the prior art, this application, through its vehicle body and flip-up container structure, allows the container to be towed by a tractor with the assistance of the vehicle body, realizing the mobile deployment of the drone airport. On the other hand, the container can be flipped up, ensuring that the top landing platform is always in a horizontal state, thus facilitating the take-off and landing of drones. At the same time, combined with the design of deployable / retractable landing platforms, the landing platforms can be retracted when moving and deployed when in use, enabling the airport to quickly adapt to different terrain requirements along railway lines. The mobile nature overcomes the power and terrain limitations of fixed airports, and the location can be dynamically adjusted according to inspection needs, reducing the ineffective round-trip time of drones and improving the effective inspection coverage. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this application, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 A schematic diagram of the structure of a mobile drone airport landing pad, which is designed for rapid deployment, at one angle according to an embodiment of this application.

[0017] Figure 2 A schematic diagram of the landing pad of the mobile drone airport, which is designed for rapid deployment according to an embodiment of this application, when deployed from another angle;

[0018] Figure 3 for Figure 2 Enlarged view of part A;

[0019] Figure 4 for Figure 2 Enlarged view of part B;

[0020] Figure 5 for Figure 2 Enlarged view of part C;

[0021] Figure 6 This is a schematic diagram of the structure of a mobile drone airport, which is designed for rapid deployment and is shown in the embodiment of this application, when the landing pad is retracted.

[0022] The labels for the attached figures are as follows:

[0023] 1. Vehicle body; 2. Box body; 3. Stop platform; 4. Locking mechanism;

[0024] 101. Top plate; 102. Tilting block; 103. Insertion hole; 104. Fixing rod; 105. Rolling strip; 106. Fixing rope; 107. First mounting plate; 108. First adjusting shaft; 109. Second mounting plate; 110. Support plate; 111. Balance bar;

[0025] 201. Traction arm;

[0026] 301. Flip plate; 302. Splicing plate; 303. Support rod; 304. First connecting shaft; 305. Second connecting shaft; 306. First support block; 307. First support groove; 308. Second support block; 309. Second support groove; 310. Flip shaft; 311. Splicing groove; 312. First threaded hole; 313. Splicing block;

[0027] 401. Third mounting plate; 402. First locking shaft; 403. Mounting rod; 404. Adjusting rod; 405. Fourth mounting plate; 406. Mounting tube; 407. Second locking shaft; 408. Adjusting tube. Detailed Implementation

[0028] To make the technical problems, technical solutions, and beneficial effects to be solved by this application clearer, the following detailed description is provided in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative and are not intended to limit the scope of this application.

[0029] It should be further noted that the accompanying drawings and embodiments of this application mainly describe the concept of this application. Based on this concept, some specific forms and arrangements of connection relationships, positional relationships, power mechanisms, power supply systems, hydraulic systems and control systems may not be fully described. However, under the premise that those skilled in the art understand the concept of this application, they can implement the above-mentioned specific forms and arrangements in a well-known manner.

[0030] When a component is referred to as being "fixed to" or "set on" another component, it can be directly on or indirectly on that other component. When a component is referred to as being "connected to" another component, it can be directly connected to or indirectly connected to that other component.

[0031] The terms “length”, “width”, “up”, “down”, “front”, “back”, “left”, “right”, “vertical”, “horizontal”, “top”, “bottom”, “inner”, “outer”, etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this application.

[0032] The terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Therefore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this application, "multiple" means two or more, and "several" means one or more, unless otherwise explicitly specified.

[0033] The mobile drone airport provided in this application, which is easy to deploy quickly, will now be described.

[0034] Please refer to the following: Figures 1 to 5The mobile drone airport, which is easy to deploy quickly, includes a vehicle body 1, a housing 2, a landing platform 3, and a locking mechanism 4. The housing 2 is rotatable and mounted on top of the vehicle body 1. A towing arm 201 is provided on the side wall of the housing 2 for connecting to a towing vehicle. The landing platform 3 consists of a top plate 101 of the housing 2, four flip-up plates 301, and four splicing plates 302. The flip-up plates 301 are rotatable and mounted on the side wall of the housing 2. When the landing platform 3 is unfolded, the flip-up plates 301 are arranged horizontally, and the splicing plates 302 are detachably connected between adjacent flip-up plates 301. When the landing platform 3 is retracted, the splicing plates 302 are disassembled, and the flip-up plates 301 are arranged vertically. The locking mechanism 4 is located between the housing 2 and the vehicle body 1. When the locking mechanism 4 is locked, the housing 2 is fixed relative to the vehicle body 1.

[0035] The advantages of the mobile drone airport provided in this embodiment, which facilitates rapid deployment, are as follows: Compared with the prior art, the mobile drone airport provided in this embodiment, through the structure of the vehicle body 1 and the flip-up container 2, allows the container 2 to be towed by a tractor with the assistance of the vehicle body 1, realizing the mobile deployment of the drone airport. On the other hand, the container 2 can be flipped so that the top landing platform 3 is always in a horizontal state, which facilitates the take-off and landing of drones. At the same time, combined with the design of the deployable and retractable landing platform 3, the landing platform 3 can be retracted when moving and deployed when used, so that the airport can quickly adapt to the different terrain requirements along the railway line. The mobile feature breaks through the power and terrain limitations of fixed airports, and the position can be dynamically adjusted according to the inspection needs, reducing the ineffective round-trip time of drones and improving the effective inspection coverage.

[0036] Combination Figure 2 , Figure 3 and Figure 4 As shown, when the flip-up plate 301 is arranged horizontally, a support rod 303 is provided between the flip-up plate 301 and the housing 2. One end of the support rod 303 is detachably connected to the flip-up plate 301, and the other end of the support rod 303 is detachably connected to the side wall of the housing 2. The detachable connection of the support rod 303 ensures the stability of the platform 3 during deployment while enabling quick assembly and disassembly. The dual-end independent connection design gives the support structure modular characteristics, minimizing the storage volume while ensuring load-bearing capacity, meeting the core requirement of space efficiency for mobile deployment.

[0037] Specifically, the support rod 303 has a first connecting shaft 304 and a second connecting shaft 305 at both ends. The bottom of the flip plate 301 has two first support blocks 306, which are spaced apart. The first support blocks 306 have a first support groove 307, and the groove opening of the first support block 307 is located on the side wall of the first support block 306 away from the box 2. The first support shaft is inserted into the first support groove 307. The side wall of the box 2 has two second support blocks 308, which are spaced apart. The second support blocks 308 have a second support groove 309, and the groove opening of the second support groove 309 is located on the side wall of the second support block 308 away from the box 2. The second support shaft is inserted into the second support groove 309.

[0038] The design of the first and second support grooves 309 ensures that the first and second connecting shafts 305 form a self-locking effect when under force. Simultaneously, since the first and second support grooves 309 are oriented in the same direction, it facilitates the insertion of the first and second connecting shafts 305 of the support rod 303, improving the ease of installation and disassembly of the support rod 303. The spaced double support blocks form a stable triangular support structure, which can evenly distribute the load of the landing platform 3 when horizontally deployed, making it particularly suitable for heavy-duty UAV operation scenarios.

[0039] Furthermore, the first support block 306 has a first support hole, into which a bolt is screwed to secure the first support shaft within the first support groove 307; the second support block 308 has a second support hole, into which a bolt is screwed to secure the second support shaft within the second support groove 309. The bolt securing mechanism enables rapid locking and releasing of the connecting shaft. The threaded connection maintains a stable connection even under vibration, making it particularly suitable for vibration conditions caused by vehicle traffic along railway lines, preventing accidental loosening of the support structure during operation.

[0040] like Figure 5 Near the top of each side wall of the housing 2, two rotating blocks 102 are arranged at intervals. Each rotating block 102 has a rotating hole. A pair of opposite side walls of the rotating plate 301 are provided with rotating shafts 310. The rotating plate 301 corresponds one-to-one with each set of rotating blocks 102, and the rotating shafts 310 are inserted into the corresponding rotating holes. The rotating blocks 102 and rotating shafts 310 cooperate with each other to facilitate the rotation of the rotating plate relative to the housing 2. At the same time, in order to prevent the top of the rotating plate 301 from interfering with the housing 2, the top of the rotating plate 301 is chamfered.

[0041] The top surface of the flip plate 301 is provided with four splicing slots 311. One end of some splicing slots 311 is flush with the left side wall of the flip plate 301, and one end of the remaining splicing slots 311 is flush with the right side wall of the flip plate 301. The bottom surface of the splicing slots 311 is provided with a first threaded hole 312. The two adjacent side walls of the splicing plate 302 are provided with multiple splicing blocks 313. The splicing blocks 313 correspond one-to-one with the splicing slots 311. The splicing block 313 on one side wall of the splicing plate 302 is inserted into the corresponding splicing slot 311 of one of the two adjacent flip plates 301, and the splicing block 313 on the other side wall of the splicing plate 302 is inserted into the corresponding splicing slot 311 of the other of the two adjacent flip plates 301. The splicing block 313 is provided with a second threaded hole. When the stop platform 3 is unfolded, the bolt is screwed into the corresponding first threaded hole 312 and second threaded hole. The precise fit between the splicing block 313 and the splicing groove 311 achieves millimeter-level positioning accuracy for multiple panels, ensuring that the flatness error of the unfolded landing platform 3 is ≤2mm. The staggered splicing groove 311 is designed to form an interlocking structure, effectively preventing horizontal displacement of the splicing plate 302 and meeting the stringent requirements for platform flatness for precise UAV landing.

[0042] like Figure 1 , Figure 2 and Figure 6 As shown, the side wall of the housing 2 has four insertion holes 103, each corresponding to a splicing plate 302. The insertion holes 103 are strip-shaped. When the platform 3 is retracted, the disassembled splicing plate 302 is inserted into the corresponding insertion hole 103, with a portion of the splicing plate 302 extending outside the housing 2. Fixing rods 104 are provided on both sides of the housing 2, and the two ends of a fixing rope 106 are fixed to the fixing rods 104 respectively. The fixing rope 106 passes through the second threaded hole of the splicing plate 302 to secure it. This combination of insertion holes 103 and fixing rope 106 provides double fixation for the splicing plate 302 during storage: physical insertion restricts longitudinal displacement, and the threaded hole with rope constrains lateral movement. This design integrates disparate components into the structural components of the vehicle body 1 during transportation, preventing the loss of small parts and reducing loading space occupation.

[0043] Furthermore, when the tilting plates 301 are arranged parallel to the side walls of the container 2, each tilting plate 301 is secured with cable ties on its outer side. The cable ties 105, when in the vertically stowed state, form a flexible constraint, allowing for a small amount of deformation space between the side walls of the container 2 and the tilting plates 301, while also preventing mechanical collision damage caused by vehicle bumps. This solution strikes a balance between transportation safety and structural durability, and is particularly suitable for rugged road conditions in high-slope areas.

[0044] In this embodiment, the bottom of the housing 2 is provided with two first mounting plates 107, and a first adjusting shaft 108 is provided between the first mounting plates 107. The top of the vehicle body 1 is provided with two second mounting plates 109 spaced apart, and the first adjusting shaft 108 passes through the second mounting plates 109. The clearance fit design between the first adjusting shaft 108 and the second mounting plates 109 enables the housing 2 to have horizontal adjustment capability. This adaptive characteristic can compensate for the unevenness of the ground when the vehicle body 1 is parked, ensuring that the housing 2 always maintains a horizontal reference when unfolded, providing the necessary basic conditions for the take-off and landing of the UAV.

[0045] like Figure 5 As shown, the locking mechanism 4 includes two third mounting plates 401, a first locking shaft 402, a mounting rod 403, an adjusting rod 404, two fourth mounting plates 405, a mounting tube 406, and an adjusting tube 408. The two third mounting plates 401 are spaced apart at the bottom of the housing 2; the first locking shaft 402 is rotatably positioned between the two third mounting plates 401; the top of the mounting rod 403 is located on the first locking shaft 402; and the adjusting rod 404 is connected to the mounting rod 405. The mounting rod 404 is rotatably mounted on the mounting rod 403, and two fourth mounting plates 405 are spaced apart on the top of the vehicle body 1. The second locking shaft 407 is rotatably mounted between the two fourth mounting plates 405. The bottom end of the mounting tube 406 is mounted on the second locking shaft 407. The adjusting tube 408 is coaxially arranged with the mounting tube 406, and the adjusting tube 408 is rotatably mounted on the mounting tube 406. A portion of the adjusting rod 404 is screwed into the adjusting tube 408. The dual-axis four-bar locking mechanism 4 generates a mechanical force amplification effect through the threaded pair, requiring only a small torque to produce a large vertical locking force. This design achieves high-ratio locking within a limited space, effectively suppressing the impact of vehicle engine vibration on the stability of the housing 2, and ensuring absolute structural stability during operation. At the same time, the horizontality of the housing 2 can be adjusted by the extension and retraction between the adjusting rod 404 and the adjusting tube 408.

[0046] Finally, the vehicle body 1 is equipped with four support plates 110, which are located at the four corners of the vehicle body 1. Each support plate 110 has support holes, and a balance bar 111 is screwed into each support hole. The balance bar 111 can rotate to abut against or release from the bottom surface. Rotating the balance bar 111 forms a four-point leveling system. By adjusting the stroke of the balance bar 111, the ground tilt angle can be adapted. Millimeter-level height control is achieved through threaded fine-tuning, enabling the vehicle body 1 to maintain stable load-bearing capacity even on complex ground conditions such as soft soil and gravel.

[0047] The above are merely preferred embodiments of this application and are not intended to limit this application. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of this application should be included within the protection scope of this application.

Claims

1. A mobile unmanned aerial vehicle (UAV) airport that is easy to deploy quickly, characterized in that, include: Vehicle body (1); The box (2) is flipped and located on the top of the vehicle body (1). A traction arm (201) is provided on the side wall of the box (2). The traction arm (201) is used to connect with the tractor. The stop platform (3) consists of a top plate (101) of the housing (2), four flip plates (301) and four splicing plates (302). The flip plates (301) can be flipped and installed on the side wall of the housing (2). When the stop platform (3) is unfolded, the flip plates (301) are arranged horizontally, and the splicing plates (302) are detachably connected between adjacent flip plates (301). When the stop platform (3) is retracted, the splicing plates (302) are disassembled, and the flip plates (301) are arranged vertically. A locking mechanism (4) is provided between the box (2) and the vehicle body (1). When the locking mechanism (4) is locked, the box (2) is fixed relative to the vehicle body (1).

2. The mobile drone airport as described in claim 1, characterized in that: When the flip plate (301) is arranged horizontally, a support rod (303) is provided between the flip plate (301) and the box (2). One end of the support rod (303) is detachably connected to the flip plate (301), and the other end of the support rod (303) is detachably connected to the side wall of the box (2).

3. The mobile drone airport as described in claim 2, characterized in that: The support rod (303) has a first connecting shaft (304) and a second connecting shaft (305) at both ends. The bottom of the flip plate (301) has two first support blocks (306). The first support blocks (306) are arranged at intervals, and the first support blocks (306) have a first support groove (307). The groove of the first support groove (307) is located on the side wall of the first support block (306) away from the box (2). The first support shaft is inserted into the first support groove (307). The box (2) has two second support blocks (308) on its side wall. The second support blocks (308) are arranged at intervals and the second support blocks (308) are provided with second support grooves (309). The groove opening of the second support groove (309) is located on the side wall of the second support block (308) away from the box (2). The second support shaft is inserted into the second support groove (309).

4. The mobile drone airport as described in claim 3, characterized in that: The first support block (306) is provided with a first support hole, and a bolt is screwed into the first support hole to block the first support shaft in the first support groove (307); The second support block (308) is provided with a second support hole, and a bolt is screwed into the second support hole to block the second support shaft in the second support groove (309).

5. The mobile drone airport as described in claim 4, characterized in that: Two flip blocks (102) are arranged at intervals near the top of each side wall of the box (2). The flip blocks (102) are provided with flip holes. A pair of opposite side walls of the flip plate (301) are provided with flip shafts (310). The flip plate (301) corresponds one-to-one with each set of flip blocks (102). The flip shafts (310) are inserted into the corresponding flip holes. The top surface of the flip plate (301) is provided with four splicing grooves (311), one end of two of the splicing grooves (311) is flush with the left side wall of the flip plate (301), and one end of the other two splicing grooves (311) is flush with the right side wall of the flip plate (301). The bottom surface of the splicing grooves (311) is provided with a first threaded hole (312). The splicing plate (302) has multiple splicing blocks (313) on two adjacent side walls. The splicing blocks (313) correspond one-to-one with the splicing grooves (311). The splicing block (313) on one side wall of the splicing plate (302) is inserted into the corresponding splicing groove (311) of one of the two adjacent flip plates (301), and the splicing block (313) on the other side wall of the splicing plate (302) is inserted into the corresponding splicing groove (311) of the other of the two adjacent flip plates (301). The splicing block (313) is provided with a second threaded hole. When the stop platform (3) is unfolded, the bolt is screwed into the corresponding first threaded hole (312) and second threaded hole.

6. The mobile drone airport as described in claim 5, characterized in that: The side wall of the box (2) is provided with four insertion holes (103), each of which corresponds to a splicing plate (302). The insertion holes (103) are strip-shaped holes. When the stop platform (3) is retracted, the disassembled splicing plate (302) is inserted into the corresponding insertion hole (103), and a portion of the splicing plate (302) is located outside the box (2). The two sides of the box (2) are provided with fixing rods (104), and the two ends of the fixing rope (106) are respectively fixed on the fixing rods (104). The fixing rope (106) passes through the second threaded hole of the splicing plate (302) to fix the splicing plate (302).

7. The mobile drone airport as described in claim 6, characterized in that: When the flip-up plate (301) is arranged parallel to the side wall of the box (2), each flip-up plate (301) is bound with a cable tie on its outer side.

8. The mobile drone airport as described in claim 7, characterized in that: The bottom of the box (2) is provided with two first mounting plates (107), and a first adjusting shaft (108) is provided between the first mounting plates (107). The top of the vehicle body (1) is provided with two second mounting plates (109) spaced apart, and the first adjusting shaft (108) passes through the second mounting plates (109).

9. The mobile unmanned aerial vehicle airport for rapid deployment as described in claim 8, characterized in that, The locking mechanism (4) includes: Two third mounting plates (401) are spaced apart at the bottom of the housing (2); The first locking shaft (402) is rotatably disposed between the two third mounting plates (401); The mounting rod (403) has its top end located on the first locking shaft (402); An adjusting rod (404) is arranged coaxially with the mounting rod (403), and the adjusting rod (404) is rotatably mounted on the mounting rod (403); Two fourth mounting plates (405) are spaced apart on the top of the vehicle body (1); The second locking shaft (407) is rotatably disposed between the two fourth mounting plates (405); The mounting tube (406) is located at its bottom end on the second locking shaft (407); The adjusting tube (408) is arranged coaxially with the mounting tube (406), and the adjusting tube (408) is rotatably mounted on the mounting tube (406). The adjusting rod (404) is partially screwed into the adjusting tube (408).

10. The mobile unmanned aerial vehicle airport for rapid deployment as described in claim 9, characterized in that: The vehicle body (1) is provided with four support plates (110), which are located at the four corners of the vehicle body (1). The support plates (110) are provided with support holes, and a balance bar (111) is screwed into the support hole. The balance bar (111) can abut against the bottom surface or release from the bottom surface due to rotation.

Images