Foldable multi-rotor unmanned aerial vehicle nest

Abstract

The utility model relates to unmanned plane technical field provides a kind of foldable multi-rotor unmanned plane nest, the nest includes cabin, groove, lifting plate, landing pad, telescopic rod and hatch cover. Energy compartment is equipped in cabin interior;Groove is arranged between cabin shell and energy compartment;Lifting plate is placed in groove, can be electrically lifted along groove;Landing pad includes main landing pad and accessory landing pad;Telescopic rod is equipped in the four corners of cabin, can be electrically lifted;Hatch cover is connected with telescopic rod by adjusting rod, can be closed and combined in the top of cabin. Accessory landing pad is equipped with fixed buckle, telescopic belt and positioning target, for the fixation and visual identification positioning of unmanned plane;Main landing pad is also equipped with connecting line, and energy compartment is electrically connected, for the charging of unmanned plane. The utility model is through the landing pad structure of liftable, reversible, realizes the parking and unfolding of multiple unmanned planes, with the advantages of high space utilization, convenient transportation and deployment.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a foldable multi-rotor UAV nest. Background Technology

[0002] Multirotor drones are widely used in inspection, surveying, and logistics, but parking and charging them often require dedicated hangars. Existing drone hangars mostly use fixed structures, which occupy a large area, lack flexibility, and cannot accommodate multiple drones simultaneously. Furthermore, traditional hangars lack effective folding and storage mechanisms, leading to inconvenience in transportation and deployment. To address these issues, this invention provides a foldable multirotor drone hangar. Through a liftable and flip-up landing pad structure, it enables compact parking and rapid deployment of drones, improving space utilization and operational efficiency. Utility Model Content

[0003] To address these issues, this invention provides a foldable multi-rotor drone nest, which solves the problems of large footprint, inability to accommodate multiple drones, and inconvenience of folding in existing technologies.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a foldable multi-rotor drone nest, comprising:

[0005] The cabin is a cube, and an energy compartment is located inside the cabin.

[0006] The tank is designed to be hollow and is disposed between the outer shell of the cabin and the energy compartment;

[0007] A lifting plate, which is disposed inside the trough and can be electrically raised and lowered along the trough;

[0008] The helipad includes a main helipad and an auxiliary helipad. The main helipad is located on top of the energy compartment. The auxiliary helipad is connected to the lifting platform by a rotating shaft. The lifting platform can be electrically driven to rotate the shaft to adjust the angle between the auxiliary helipad and the lifting platform.

[0009] Telescopic masts are located at the four corners of the cabin and can be electrically raised and lowered.

[0010] The hatch and the telescopic rod are connected by an adjusting rod.

[0011] Preferably, the tank is provided in four groups, which are respectively located on the four sides of the cabin.

[0012] Preferably, the number of lifting plates and the number of troughs are the same, with each lifting plate disposed in one of the troughs.

[0013] Preferably, the trough and the lifting plate are arranged vertically.

[0014] Preferably, the auxiliary helipads include a first helipad, a second helipad, a third helipad, and a fourth helipad.

[0015] Preferably, the auxiliary helipad can only rotate and fold towards the outside of the cabin, and the angle between the auxiliary helipad and the lifting platform is [value missing]. 90°≤ ≤180°.

[0016] Preferably, each of the auxiliary landing pads is equipped with a fixing buckle and a telescopic belt. The telescopic belt can be stretched and fastened to the outside of the UAV and connected and fixed with the fixing buckle, for fixing the UAV on the main landing pad and the auxiliary landing pad.

[0017] Preferably, both the main landing pad and the auxiliary landing pad are equipped with positioning targets, which are used for the UAV to perform visual recognition, positioning, and landing.

[0018] Preferably, the adjusting rod and the telescopic rod are connected by an electric rotating shaft, and the other end of the telescopic rod is provided with a hatch cover. The four hatch covers can be assembled and sealed on the top of the cabin.

[0019] Preferably, the main apron is provided with a plurality of connecting lines, one end of which is electrically connected to the energy compartment, and the connecting lines are stretchable.

[0020] The application employs the above technical solution and has at least the following beneficial effects:

[0021] The liftable and flip-up landing pad design enables compact parking and rapid deployment of multiple drones, saving space; the canopy and telescopic boom structure provide excellent airtight protection, adapting to outdoor environments; the fixing buckles and positioning targets ensure the stability and accuracy of drone parking; the overall structure is foldable, facilitating transportation and deployment, and improving practicality.

[0022] It should be understood that the above general description and the following detailed description are exemplary and explanatory only, and do not limit this application. Attached Figure Description

[0023] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, 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 utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0024] Figure 1 This is a structural schematic diagram provided by an embodiment of the present utility model;

[0025] Figure 2 This is a structural schematic diagram provided by an embodiment of the present utility model;

[0026] In the diagram: 1. Cabin; 2. Tank; 3. Lifting platform; 4. Main landing pad; 5. Telescopic boom; 6. Cabin cover; 7. Adjusting boom; 8. First landing pad; 9. Second landing pad; 10. Third landing pad; 11. Fourth landing pad; 12. Fixing buckle; 13. Telescopic belt; 14. Connecting line; 15. Positioning target. Detailed Implementation

[0027] To make the objectives, technical solutions, and advantages of this utility model clearer, the technical solutions of this utility model will be described in detail below. Obviously, the described embodiments are only a part of the embodiments of this utility model, and not all of them. Based on the embodiments of this utility model, all other implementation methods obtained by those skilled in the art without creative effort are within the scope of protection of this utility model.

[0028] A specific embodiment of this utility model provides a foldable multi-rotor drone nest, combined with an attached... Figure 1 and attached Figure 2 As shown, it mainly includes the cabin 1, the tank 2, the lifting platform 3, the landing pad, the telescopic boom 5, and the hatch cover 6.

[0029] Specifically, in this embodiment, the cabin 1 is configured as a cubic structure, with an energy compartment inside for storing electrical energy to provide power support for the drone; the trough 2 is configured as a hollow shape and is located between the outer shell of the cabin 1 and the energy compartment, for accommodating the lifting plate 3 and guiding its movement; in this embodiment, there are four sets of trough 2, which are fixed to the four sides of the cabin 1 respectively, and the trough 2 is vertically arranged.

[0030] Specifically, the lifting plate 3 is installed inside the tank 2 and can be electrically raised and lowered along the tank 2. The number of lifting plates 3 is the same as the number of tanks 2, with each lifting plate 3 corresponding to a set of tanks 2. The lifting plate 3 is driven by a motor to achieve lifting and lowering movement, thereby adjusting its height position.

[0031] Specifically, the helipad includes a main helipad 4 and auxiliary helipads. The main helipad 4 is fixedly located on top of the energy bay and is used to park one main UAV. The auxiliary helipads include a first helipad 8, a second helipad 9, a third helipad 10, and a fourth helipad 11, which are connected to four lifting platforms 3 via rotating shafts. Each lifting platform 3 integrates an electric rotating shaft drive mechanism, which can drive the rotating shaft to rotate, thereby adjusting the angle between the auxiliary helipads and the lifting platforms 3. , where 90°≤ The angle is ≤180°, which allows the auxiliary helipad to fold and unfold only towards the outside of cabin 1, avoiding interference with the internal structure of the cabin.

[0032] Specifically, the telescopic rods 5 are located at the four corners of the cabin 1 and can be electrically raised and lowered. The top of the telescopic rods 5 is connected to the hatch cover 6 via the adjusting rod 7. The adjusting rod 7 and the telescopic rods 5 are connected by an electric rotating shaft, which can realize the rotation and opening of the hatch cover 6. When closed, the four hatch covers 6 can be sealed and spliced ​​together on the top of the cabin 1. The shape of the spliced ​​hatch cover 6 is consistent with the bottom of the cabin 1, forming a complete protective shell.

[0033] Specifically, each auxiliary landing pad is equipped with a fixing buckle 12 and a telescopic belt 13. The telescopic belt 13 can be manually stretched and wrapped tightly around the outside of the UAV fuselage, and the end is connected to the fixing buckle 12 to achieve reliable fixation of the UAV. In addition, both the main landing pad 4 and the auxiliary landing pad are equipped with positioning targets 15 for visual recognition and precise positioning of the UAV when it lands.

[0034] Specifically, the main helipad 4 is also equipped with several connecting lines 14. One end of the connecting line 14 is electrically connected to the energy cabin, and the other end is equipped with an interface that can be extended to the surface of the helipad for charging or powering the parked drones.

[0035] The working principle of this embodiment:

[0036] When a drone needs to be deployed, the control system first drives the telescopic boom 5 to rise, causing the hatch 6 to rotate and open via the adjusting rod 7, exposing the landing pad. Subsequently, the lifting platform 3 rises along the trough 2 to a predetermined height, while simultaneously the electric rotating shaft drives the auxiliary landing pad to fold outwards, changing it from a vertically folded state to a horizontal or tilted unfolded state, forming multiple landing positions. The drone can accurately land by identifying and locating the target 15 through a vision system. After landing, the operator or automated mechanism uses the telescopic belt 13 and fixing buckles 12 to secure the drone. The connecting cable 14 can be used to charge the drone.

[0037] When the drone needs to be stored, the fixing mechanism releases the drone, the lifting platform 3 descends, and at the same time the electric rotating shaft drives the auxiliary landing pad to fold inward back to the vertical position, the telescopic rod 5 descends, and the canopy 6 closes, forming a sealed protective space to prevent the drone from being affected by the environment.

[0038] Through the above structure, this utility model realizes the foldable and multi-position parking function of the drone nest, improving space utilization and deployment efficiency.

[0039] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some or all of the technical features therein. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of this utility model.

Claims

1. A foldable multi-rotor drone nest, characterized in that, include: The cabin (1) is configured as a cube, and an energy compartment is provided inside the cabin (1); The tank (2) is hollow and is located between the outer shell of the cabin (1) and the energy cabin. Lifting plate (3), the lifting plate (3) is disposed inside the trough (2) and can be electrically lifted and lowered along the trough (2); The helipad is provided with a main helipad (4) and an auxiliary helipad. The main helipad (4) is located on the top of the energy compartment. The auxiliary helipad and the lifting plate (3) are connected by a rotating shaft. The lifting plate (3) can be electrically driven to rotate and adjust the angle between the auxiliary helipad and the lifting plate (3). Telescopic rods (5) are installed at the four corners of the cabin (1) and can be electrically raised and lowered; The hatch (6) and the telescopic rod (5) are connected by an adjusting rod (7).

2. The foldable multi-rotor UAV nest according to claim 1, characterized in that: The tank (2) is provided in four groups, which are respectively located on the four sides of the cabin (1).

3. A foldable multi-rotor UAV nest according to claim 2, characterized in that: The number of lifting plates (3) and the number of troughs (2) are the same, and one lifting plate (3) is set in a group of troughs (2).

4. A foldable multi-rotor UAV nest according to claim 3, characterized in that: The trough (2) and the lifting plate (3) are vertically arranged.

5. A foldable multi-rotor UAV nest according to claim 4, characterized in that: The attached helipads include the first helipad (8), the second helipad (9), the third helipad (10), and the fourth helipad (11).

6. A foldable multi-rotor UAV nest according to claim 5, characterized in that: The auxiliary helipad can only be rotated and folded towards the outside of the cabin (1), and the included angle between the auxiliary helipad and the lifting platform (3) is . 90°≤ ≤180°.

7. A foldable multi-rotor UAV nest according to claim 6, characterized in that: Each of the auxiliary landing pads is equipped with a fixing buckle (12) and a telescopic belt (13). The telescopic belt (13) can be stretched and fastened to the outside of the UAV and connected and fixed with the fixing buckle (12) to fix the UAV parked on the main landing pad (4) and the auxiliary landing pad.

8. A foldable multi-rotor UAV nest according to claim 7, characterized in that: Both the main helipad (4) and the auxiliary helipad are equipped with positioning targets (15), which are used for the UAV to perform visual recognition and positioning.

9. A foldable multi-rotor UAV nest according to claim 1, characterized in that: The adjusting rod (7) and the telescopic rod (5) are connected by an electric rotating shaft. The other end of the telescopic rod (5) is provided with the hatch cover (6). The four hatch covers (6) can be sealed and spliced ​​together on the top of the cabin (1). The hatch cover (6) after splicing is consistent with the bottom shape of the cabin (1).

10. A foldable multi-rotor UAV nest according to claim 1, characterized in that: The main apron (4) is provided with several connecting lines (14), one end of which is electrically connected to the energy cabin, and the connecting line (14) is stretchable.

Images