Unmanned aerial vehicle integrated operation platform

Abstract

The utility model discloses an unmanned aerial vehicle integrated operation platform, and particularly relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle integrated operation platform comprises a case, a mounting groove is formed in the front surface of the case, a placement table is arranged in the mounting groove, a linear motor is fixed at the top of the placement table, a movable track is arranged above the linear motor, and a movable guide rail is arranged on the movable track. The unmanned aerial vehicle device is placed above the track, iron blocks are fixed to the tops of wings of the unmanned aerial vehicle device, fixing blocks are fixed to the tops of the mounting grooves, and telescopic devices are arranged at the bottoms of the fixing blocks. The rail is driven by the linear motor to move towards the outside of the case, and the unmanned aerial vehicle device can enter a to-fly state, so that time can be saved, the unmanned aerial vehicle device can take off quickly and enter shooting work, and the unmanned aerial vehicle device can enter a working state quickly.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to an integrated UAV operating platform. Background Technology

[0002] Drones are unmanned aircraft controlled by radio remote control equipment and their own program control devices. Small drones are small and lightweight unmanned aerial vehicles, usually used in civilian fields such as personal entertainment, aerial photography, and environmental monitoring.

[0003] With the development of drone technology, small drones are now being used in public service sectors. In situations such as traffic jams, fires, and floods, drones can be remotely controlled by operators. The drones, carrying aerial cameras, depart from the operating platform, and the cameras capture images of the areas the drones pass through. These images are then transmitted to the operating platform, allowing personnel at the control center to understand the specific environmental conditions. Currently, drone operating platforms mainly use loading containers to carry the drones. When performing tasks, staff need to remove the operating platform from the vehicle transporting the platform, open the loading container to take out the drone, and perform other setup and testing operations such as installing batteries. This process consumes a significant amount of time in preparing the drone, resulting in slow deployment of the drones. Utility Model Content

[0004] The purpose of this invention is to provide an integrated operating platform for unmanned aerial vehicles (UAVs) to address the aforementioned shortcomings in the technology.

[0005] To achieve the above objectives, this utility model provides the following technical solution:

[0006] An integrated unmanned aerial vehicle (UAV) operating platform includes a chassis. A mounting slot is formed on the front surface of the chassis, and a placement platform is located within the mounting slot. A linear motor is fixed to the top of the placement platform, and a movable track is positioned above the linear motor. A UAV device is placed above the track, and an iron block is fixed to the top of the UAV device's wing. A fixing block is fixed to the top of the mounting slot, and a telescopic device is located at the bottom of the fixing block. A connecting plate is connected to the telescopic end of the telescopic device, and a stabilizing rod is fixed to the bottom of the connecting plate. A magnetic block is fixed to the bottom end of the stabilizing rod.

[0007] Preferably, a charging socket is provided on the rear surface of the drone device, and a power supply device is also provided inside the chassis. A power plug is provided on one side of the power supply device, and a fixing tube is provided on the outside of the power plug. The power plug is matched with the charging socket.

[0008] Preferably, the top of the track has an arc groove, and the bottom of the drone device is provided with a support foot, which is a cylindrical structure and can move in the arc groove.

[0009] Preferably, a baffle is provided at the bottom of the front surface of the mounting groove, multiple fans are fixed on the rear surface of the baffle, air holes are also provided on the surface of the baffle, and several arrayed through holes are provided on the top of the placement platform.

[0010] Preferably, a dust collection box is also provided above the track, with an inlet at the bottom of the dust collection box and an exhaust fan at the top of the dust collection box. The air inlet of the exhaust fan is connected to the dust collection box, and a duct is connected to the air outlet of the exhaust fan. An exhaust box is provided on the side wall of the chassis, and the extension end of the duct penetrates the side wall of the chassis and is connected to the exhaust box.

[0011] Preferably, the top of the track has a ventilation hole, which corresponds to the through hole on the top of the placement platform.

[0012] The technical effects and advantages provided by this utility model in the above technical solution are as follows:

[0013] The drone is housed in a chassis with a movable track. When the drone is in use, a linear motor moves the track out of the chassis, allowing the drone to enter a ready-to-fly state. This saves time, allows the drone to take off quickly and begin filming, and improves its efficiency by enabling it to quickly get into working condition. Attached Figure Description

[0014] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in this utility model. For those skilled in the art, other drawings can be obtained based on these drawings.

[0015] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 This is a front view of the present invention;

[0017] Figure 3 This is a schematic diagram of the internal structure of the present invention;

[0018] Figure 4 This is a schematic diagram of the structure of the support component, guide rail device, and unmanned aerial vehicle device of this utility model;

[0019] Figure 5 for Figure 4 Enlarged view of section A in the middle;

[0020] Figure 6for Figure 1 Diagram showing the state of the computer after the chassis has been removed;

[0021] Figure 7 for Figure 6 Enlarged view of section B in the middle.

[0022] Explanation of reference numerals in the attached figures:

[0023] 1. Chassis; 2. Exhaust box; 3. Baffle; 31. Fan; 4. Placement platform; 5. Dust collection box; 6. Mounting slot; 7. Fixing block; 8. Track; 9. Linear motor; 10. UAV device; 11. Telescopic device; 12. Exhaust fan; 13. Duct; 14. Stabilizer; 15. Connecting plate; 16. Arc groove; 17. Magnetic block; 18. Iron block; 19. Power supply device; 20. Charging socket; 21. Power plug; 22. Fixing pipe. Detailed Implementation

[0024] To enable those skilled in the art to better understand the technical solution of this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings.

[0025] This utility model provides, for example Figure 1 - Figure 7 The integrated unmanned aerial vehicle (UAV) operating platform shown includes a chassis 1. The front surface of the chassis 1 has a mounting groove 6. A placement platform 4 is provided in the mounting groove 6. A linear motor 9 is fixed on the top of the placement platform 4. A movable track 8 is provided above the linear motor 9. A UAV device 10 is placed on the track 8. An iron block 18 is fixed on the top of the wing of the UAV device 10. A fixing block 7 is fixed on the top of the mounting groove 6. A telescopic device 11 is provided at the bottom of the fixing block 7. A connecting plate 15 is connected to the telescopic end of the telescopic device 11. A stabilizing rod 14 is fixed at the bottom of the connecting plate 15. A magnetic block 17 is fixed at the bottom end of the stabilizing rod 14.

[0026] The chassis 1 can be used in conjunction with fire trucks or other vehicles. The vehicle needs to be equipped with a cargo box. The chassis 1 is placed in the cargo box. Specifically, the surface of the chassis 1 is exposed outside the cargo box so that the track 8 can extend outward, making it easier for the drone device 10 to move outward and enter the ready-to-fly state.

[0027] In this embodiment, during the specific operation of the operating platform, the user holds the remote control of the drone device 10 to control the drone device 10. After starting the linear motor 9, the sliding block of the linear motor 9 drives the track 8 to move outside the chassis 1. At this time, the magnetic block 17 and the iron block 18 are in a separated state and will not affect the movement of the drone device 10. After the track 8 reaches the outside of the chassis 1, the drone device 10 is also located outside the chassis 1. At this time, the user can directly control the drone device 10 to take off.

[0028] After completing its mission, the drone device 10 flies back to the track 8. The slider of the linear motor 9 drives the track 8 and the drone device 10 back to their original positions. The telescopic device 11 is activated, and the telescopic device 11 pushes the connecting plate 15 downward. The connecting plate 15 pushes the stabilizing rod 14 and the magnetic block 17 downward. After the magnetic block 17 comes into contact with the iron block 18, it attracts the iron block 18. At this time, the wings of the drone device 10 are supported by the stabilizing rod 14, and the drone device 10 can be placed more stably on the track 8, which is beneficial for vehicle transportation.

[0029] It should be noted that the telescopic device 11 can be an electric telescopic rod or a cylinder. The telescopic device 11, the connecting plate 15 and the stabilizing rod 14 form a support assembly. The support assembly supports the wings of the UAV device 10 to ensure that the UAV device 10 can be stably parked on the track 8 without swaying or moving back and forth or left and right.

[0030] like Figure 6 and Figure 7 As shown, a charging socket 20 is provided on the rear surface of the drone device 10, and a power supply device 19 is also provided inside the chassis 1. A power plug 21 is provided on one side of the power supply device 19, and a fixing tube 22 is provided on the outside of the power plug 21. The power plug 21 is matched with the charging socket 20.

[0031] The top of the track 8 is provided with an arc groove 16, and the bottom of the drone device 10 is provided with a support foot. The support foot is a cylindrical structure and can move in the arc groove 16. Specifically, after the drone device 10 performs a task, it flies back. The user controls the drone device 10 to land on the track 8 via a remote control. Then it can continue to fly backward and dock the drone device 10 at the end of the track 8 near the inside of the chassis 1, which is conducive to the charging of the drone device 10.

[0032] After the drone device 10 is supported by the support components, the drone device 10 is in a stable parking state. At the same time, the charging socket 20 on the rear surface of the drone device 10 is connected to the power plug 21. The power supply device 19 supplies current to the charging socket 20 through the power plug 21 to charge the drone device 10. The drone device 10 can be automatically charged after being parked inside the chassis 1, thus ensuring that the drone device 10 is always powered so that it can be used immediately when performing the next mission, which helps to save time for charging or replacing the drone device 10's battery.

[0033] like Figure 3 and Figure 6As shown, a baffle 3 is provided at the bottom of the front surface of the mounting slot 6. Multiple fans 31 are fixed on the rear surface of the baffle 3. Air holes are also provided on the surface of the baffle 3. Several arrayed through holes are provided on the top of the placement platform 4. Ventilation holes are provided on the top of the track 8, and the ventilation holes correspond to the through holes on the top of the placement platform 4. A dust collection box 5 is provided above the track 8. An inlet is provided at the bottom of the dust collection box 5. An exhaust fan 12 is provided on the top of the dust collection box 5. The air inlet of the exhaust fan 12 is connected to the dust collection box 5. A duct 13 is connected to the end of the air outlet of the exhaust fan 12. An exhaust box 2 is provided on the side wall of the casing 1. The extension end of the duct 13 penetrates the side wall of the casing 1 and is connected to the exhaust box 2.

[0034] After completing its mission, the drone device 10 flies back to the housing 1 and lands on the track 8. To remove dust or impurities from the surface of the drone device 10, the fans 31 are activated. Multiple fans 31 work simultaneously and continuously blow air upwards. The rapidly flowing air passes through the through holes of the placement platform 4, then through the vent holes at the top of the track 8, and then blows towards the drone device 10. The dust on the surface of the drone device 10 is blown upwards, and the dust-laden air flows upwards and passes through the inlet at the bottom of the dust collection box 5, then enters the interior of the dust collection box 5. The exhaust fan 12 is activated, and the exhaust fan 12 draws the dust-laden air from inside the dust collection box 5. The dust-laden air passes through the exhaust fan 12 and the duct 13 and then enters the interior of the exhaust box 2. The front surface of the exhaust box 2 has an exhaust outlet, through which the dust-laden air is discharged outwards. In this process, the drone device 10, which has completed its mission, can be continuously dusted, thus achieving the purpose of cleaning the drone device 10.

[0035] The foregoing description only illustrates certain exemplary embodiments of the present invention. Undoubtedly, those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. An integrated unmanned aerial vehicle (UAV) operation platform, characterized in that: The device includes a chassis (1), the front surface of which has an installation groove (6), a placement platform (4) is provided in the installation groove (6), a linear motor (9) is fixed on the top of the placement platform (4), a movable track (8) is provided above the linear motor (9), a drone device (10) is placed above the track (8), an iron block (18) is fixed on the top of the wing of the drone device (10), a fixing block (7) is fixed on the top of the installation groove (6), a telescopic device (11) is provided at the bottom of the fixing block (7), a connecting plate (15) is connected to the telescopic end of the telescopic device (11), a stabilizing rod (14) is fixed at the bottom of the connecting plate (15), and a magnetic block (17) is fixed at the bottom of the stabilizing rod (14).

2. The integrated UAV operation platform according to claim 1, characterized in that: The rear surface of the unmanned aerial vehicle (10) is provided with a charging socket (20), and the inside of the chassis (1) is also provided with a power supply device (19). A power plug (21) is provided on one side of the power supply device (19), and a fixing tube (22) is provided on the outside of the power plug (21). The power plug (21) is matched with the charging socket (20).

3. The integrated UAV operation platform according to claim 1, characterized in that: The top of the track (8) is provided with an arc groove (16), and the bottom of the drone device (10) is provided with a support foot. The support foot is a cylindrical structure and can move in the arc groove (16).

4. The integrated UAV operation platform according to claim 1, characterized in that: The bottom of the front surface of the mounting groove (6) is provided with a baffle (3), and a plurality of fans (31) are fixed on the rear surface of the baffle (3). The surface of the baffle (3) is also provided with air holes, and the top of the placement platform (4) is provided with a plurality of arrayed through holes.

5. The integrated UAV operation platform according to claim 4, characterized in that: A dust collection box (5) is also provided above the track (8). The bottom of the dust collection box (5) has an inlet. The top of the dust collection box (5) is provided with an exhaust fan (12). The air inlet of the exhaust fan (12) is connected to the dust collection box (5). The exhaust outlet end of the exhaust fan (12) is connected to a duct (13). An exhaust box (2) is provided on the side wall of the chassis (1). The extension end of the duct (13) passes through the side wall of the chassis (1) and is connected to the exhaust box (2).

6. The integrated UAV operation platform according to claim 1, characterized in that: The top of the track (8) is provided with a ventilation hole, which corresponds to the through hole on the top of the placement platform (4).

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