Large unmanned aerial vehicle hangar

By designing a large drone hangar, using reel boxes and servo motors to drive the roller shutter doors and sliding covers, the automated batch take-off and landing of the drone is achieved, which solves the problem of labor relying on the take-off and landing of the drone and improves the convenience of use.

CN223279366UActive Publication Date: 2025-08-29FUYANG WANXING TRAFFIC ENG
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Patent Information

Application Number
CN202422728212.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-11-09
Publication Date
2025-08-29
Estimated Expiration
2034-11-09

AI Technical Summary

Technical Problem

Drone take-off and landing requires manual assistance, occupying the site and inconvenient storage, and existing equipment cannot achieve automatic batch take-off and landing and storage.

Method used

A large drone hangar is designed, including a reel box, servo motor, electric slide rail and gear tooth structure. The opening and closing of the roller shutter door and sliding cover plate is driven by the servo motor to realize the automatic take-off and landing and storage management of the drone.

Benefits of technology

It realizes automated batch take-off and landing and storage of drones, saves manpower, and improves the convenience and efficiency of drones.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a large unmanned aerial vehicle hangar, which relates to the technical field of unmanned aerial vehicle equipment and comprises a hangar, a reel box is fixedly mounted on the top surface of the hangar, and a sliding cover plate is placed above the hangar. According to the large unmanned aerial vehicle hangar, an electric sliding rail drives a set of sliding sleeves to move towards the left side, a supporting plate loaded with the unmanned aerial vehicles is driven to move towards the left side, so that the unmanned aerial vehicles in a row can take off at the same time, and when the unmanned aerial vehicles land, a second servo motor rotates anticlockwise to drive gears to rotate reversely; through teeth, meshed with a gear, at the bottom of the sliding cover plate, the sliding cover plate moves towards the left side, a landing opening in the right side of the hangar is opened, an electric sliding rail drives a no-load supporting plate to move towards the right side, the landing unmanned aerial vehicle is borne, and after landing, the supporting plate is driven to return to the middle position through the electric sliding rail; therefore, when the unmanned aerial vehicle hangar is used, the unmanned aerial vehicles can be better subjected to batch take-off, landing and storage management.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to a large-scale unmanned aerial vehicle hangar. Background Art

[0002] Drones are now ubiquitous in our daily lives, but their takeoff and landing still require manual labor to transport the drones to the takeoff site or land and recover them. Furthermore, drones occupy space when not in use. Therefore, a takeoff and landing device is needed that can automatically take off and land drones in batches and store them. This would save manpower and make drones more convenient to use. Utility Model Content

[0003] (1) Technical problems solved

[0004] In view of the shortcomings of the existing technology, the utility model provides a large-scale UAV hangar with the advantages of automatic batch take-off and landing and storage.

[0005] (2) Technical solution

[0006] In order to solve the above technical problems, the utility model provides the following technical solutions: a large-scale UAV hangar, comprising a hangar, a reel box is fixedly installed on the top surface of the hangar, and a sliding cover is placed above the hangar.

[0007] Two guide slot frames are fixedly installed on the left side of the hangar, and a rolling shutter door is placed between the two guide slot frames, and the top of the rolling shutter door is wrapped and fixed on the reel inside the reel box. A servo motor is fixedly installed on the front of the reel box, and the output end of the servo motor is fixedly connected to the input end of the reel in the reel box. Three groups of electric slide rails arranged at equal distances are fixedly installed inside the hangar, and a sliding sleeve is clamped on the outside of each slide rail, and a support plate is fixedly installed between the side surfaces of each group of sliding sleeves that are close to each other.

[0008] A servo motor 2 is fixedly installed on the front of the hangar, and a bearing is inlaid on the front of the hangar. The output end of the servo motor 2 passes through the bearing and extends to the interior of the hangar, and the outer surface of the output end of the servo motor 2 is fixedly connected to the inner ring of the bearing. Two guide bars are fixedly installed inside the hangar, and the front and rear sides of the sliding cover are provided with sliding grooves, and the two guide bars are respectively located inside the two sliding grooves. A gear is fixedly installed on the output end of the servo motor 2, and teeth arranged at equal distances are fixedly installed on the bottom surface of the sliding cover, and the teeth are engaged with the gear.

[0009] Furthermore, the upper surface of each support plate is provided with three take-off and landing areas.

[0010] By adopting the above technical solution, the landing area on the support plate is divided into zones, which is more conducive to confirming the landing position with the assistance of the UAV's visual system.

[0011] Furthermore, the teeth are adapted to the gear.

[0012] By adopting the above technical solution, the position of the sliding cover can be adjusted better through the operation of the servo motor 2, avoiding the problem of adjustment jamming or blocking caused by mismatch between teeth and gears.

[0013] Furthermore, the width of the sliding cover is equal to the width between the inner side walls of the hangar.

[0014] By adopting the above technical solution, the landing port on the upper right side of the hangar can be better closed.

[0015] Furthermore, the width of the rolling door is smaller than the width inside the guide groove frame.

[0016] By adopting the above technical solution, it is more convenient to open and close the rolling door and avoid the problem of jamming.

[0017] (3) Beneficial effects

[0018] Compared with existing technologies, this large UAV hangar has the following beneficial effects:

[0019] The utility model is provided with a reel box. During use, the operation of the servo motor 1 drives the reel in the reel box to rotate, which can reel up the rolling shutter door, so that the left side and the upper space of the hangar are opened, and the electric slide rail drives a group of sliding sleeves to move to the left, thereby driving the support plate carrying the drone to move to the left, so that a row of drones can take off at the same time. By providing a servo motor 2, when the drone is landing, the counterclockwise rotation of the servo motor 2 drives the gear to rotate in the opposite direction, so that the sliding cover plate is moved to the left through the teeth of the gear meshing with the bottom of the sliding cover plate, thereby opening the landing port on the right side of the hangar, and driving the empty support plate to move to the right side by the electric slide rail to receive the landed drone. After landing, the support plate is driven by the electric slide rail to return to the middle position, and the drone is stored in preparation for the next take-off. Therefore, when the drone hangar is used, batch take-off and landing and storage management of drones can be better performed. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a schematic diagram of the structure of the utility model;

[0021] Figure 2 This is a schematic diagram of the internal structure of the hangar of the utility model;

[0022] Figure 3This is a schematic diagram of the structure of the rolling shutter door of the utility model;

[0023] Figure 4 This is a schematic diagram of the external structure of the sliding cover of the utility model;

[0024] Figure 5 This is a schematic diagram of the guide bar structure of the utility model;

[0025] Figure 6 This is a schematic diagram of the external structure of the support plate of the utility model.

[0026] In the figure: 1-hangar, 2-guide frame, 3-rolling door, 4-reel box, 5-servo motor 1, 6-sliding cover, 7-servo motor 2, 8-guide bar, 9-bearing, 10-electric slide rail, 11-slide, 12-teeth, 13-gear, 14-sleeve, 15-support plate, 16-take-off and landing area. DETAILED DESCRIPTION

[0027] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0028] See also Figure 1-6 The utility model provides a technical solution: a large UAV hangar, including a hangar 1, a reel box 4 is fixedly installed on the top surface of the hangar 1, a sliding cover 6 is placed above the hangar 1, and the width of the sliding cover 6 is equal to the width between the inner walls of the hangar 1, so as to better seal the landing port on the upper right side of the hangar 1.

[0029] Two guide slot frames 2 are fixedly installed on the left side of the hangar 1, and a rolling shutter door 3 is placed between the two guide slot frames 2, and the top of the rolling shutter door 3 is wrapped and fixed on the reel inside the reel box 4. The width of the rolling shutter door 3 is smaller than the width of the inside of the guide slot frame 2, which is more conducive to the opening and closing of the rolling shutter door 3 and avoids the problem of jamming. A servo motor 5 is fixedly installed on the front of the reel box 4, and the output end of the servo motor 5 is fixedly connected to the input end of the reel in the reel box 4. Three groups of equally spaced electric slide rails 10 are fixedly installed inside the hangar 1, and a sliding sleeve 14 is clamped on the outside of each slide rail 10. A support plate 15 is fixedly installed between the side surfaces of each group of sliding sleeves 14 that are close to each other. Three take-off and landing areas 16 are provided on the upper surface of each support plate 15. The landing area on the support plate 15 is divided into zones, which is more conducive to confirming the landing position with the assistance of the drone's visual system.

[0030] A servo motor 27 is fixedly installed on the front of the hangar 1, and a bearing 9 is inlaid on the front of the hangar 1. The output end of the servo motor 27 passes through the bearing 9 and extends to the interior of the hangar 1, and the outer surface of the output end of the servo motor 27 is fixedly connected to the inner ring of the bearing 9. Two guide bars 8 are fixedly installed inside the hangar 1, and the front and rear sides of the sliding cover 6 are provided with slide grooves 11, and the two guide bars 8 are respectively located inside the two slide grooves 11. A gear 13 is fixedly installed on the output end of the servo motor 27, and the bottom surface of the sliding cover 6 is fixedly installed with teeth 12 arranged at equal distances, and the teeth 12 are meshed with the gear 13. The teeth 12 are adapted to the gear 13, and the position of the sliding cover 6 can be better adjusted by the operation of the servo motor 27 to avoid the problem of adjustment jamming or jamming caused by the mismatch between the teeth 12 and the gear 13.

[0031] The electrical components in the present invention are all connected to an external main controller and 220V mains electricity, and the main controller can be a conventional known device that plays a control role such as a computer.

[0032] Working principle: During takeoff, the operation of servo motor 15 drives the reel in the reel box 4 to rotate, and the rolling door 3 is reeled to open the left side and the upper space of the hangar 1. The electric slide rail 10 drives a group of sliding sleeves 14 to move to the left, and moves the support plate 15 carrying the drone to the left, so that a row of drones take off at the same time. When the drone is landing, the counterclockwise rotation of servo motor 27 drives the gear 13 to rotate in the opposite direction, and the teeth 12 at the bottom of the sliding cover plate 6 meshing with the gear 13 move the sliding cover plate 6 to the left, and the landing port on the right side of the hangar 1 is opened, and the electric slide rail 10 drives the empty support plate 15 to move to the right to receive the landed drone. After landing, the electric slide rail 10 drives the support plate 15 to return to the middle position of the hangar 1 to store the drone in preparation for the next takeoff.

[0033] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A large UAV hangar, comprising a hangar (1), characterized in that: A reel box (4) is fixedly mounted on the top surface of the hangar (1), and a sliding cover (6) is placed above the hangar (1); Two guide slot frames (2) are fixedly installed on the left side of the hangar (1), a rolling door (3) is placed between the two guide slot frames (2), and the top of the rolling door (3) is wound and fixed on the reel inside the reel box (4), a servo motor (5) is fixedly installed on the front of the reel box (4), and the output end of the servo motor (5) is fixedly connected to the input end of the reel in the reel box (4), and three groups of electric slide rails (10) arranged at equal distances are fixedly installed inside the hangar (1), and a sliding sleeve (14) is clamped on the outside of each slide rail (10), and a support plate (15) is fixedly installed between the sides of each group of sliding sleeves (14) that are close to each other; A servo motor 2 (7) is fixedly installed on the front of the hangar (1), and a bearing (9) is embedded on the front of the hangar (1). The output end of the servo motor 2 (7) passes through the bearing (9) and extends to the inside of the hangar (1), and the outer surface of the output end of the servo motor 2 (7) is fixedly connected to the inner ring of the bearing (9). Two guide bars (8) are fixedly installed inside the hangar (1), and the front and rear sides of the sliding cover (6) are provided with sliding grooves (11), and the two guide bars (8) are respectively located inside the two sliding grooves (11). A gear (13) is fixedly installed on the output end of the servo motor 2 (7), and teeth (12) arranged at equal distances are fixedly installed on the bottom surface of the sliding cover (6), and the teeth (12) are meshed with the gear (13).

2. A large UAV hangar according to claim 1, characterized in that: The upper surface of each support plate (15) is provided with three take-off and landing areas (16).

3. The large UAV hangar according to claim 1, characterized in that: The teeth (12) are matched with the gear (13).

4. The large UAV hangar according to claim 1, characterized in that: The width of the sliding cover (6) is equal to the width between the inner side walls of the hangar (1).

5. The large UAV hangar according to claim 1, characterized in that: The width of the rolling shutter door (3) is smaller than the width inside the guide groove frame (2).