Field unmanned aerial vehicle nest power supply device
By designing a flip unit combining solar panels and electromagnets in the drone nest device, the drone nest is independent power supply in the field, solving the problems of field drone inspection endurance and coverage area, and improving patrol efficiency and power supply stability.
Patent Information
- Application Number
- CN202322970963.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2023-11-03
- Publication Date
- 2025-03-11
- Estimated Expiration
- 2033-11-03
AI Technical Summary
The existing drone nest devices cannot provide independent power in the field, which limits the battery life and coverage area of the drone patrol in the field.
A field drone nest power supply device is designed, using a flip unit combining solar panels and electromagnets. The flip of the solar panel is controlled by the motor to realize the automatic positioning of the solar panels and clear debris, ensuring stable power supply.
It realizes independent power supply for the drone nest in the wild, extends the battery life of the drone, improves the coverage area of patrol, and ensures the stability of power supply through automatic debris removal.
Smart Images

Figure CN222591810U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of outdoor electric power engineering machinery, in particular to a drone nest device. Background Art
[0002] Nowadays, drones are gradually being used in wildlife inspections due to their many advantages, and have become an important measure to protect wildlife. However, since the battery capacity of drones is very small, they can only maintain the flight time of the drone for a few hours, making the area that drone inspections can cover relatively small. In order to solve the problem of drone endurance, many drone companies have developed drone charging nests. For example, DJI has launched a DJI Airport (Nest) product, but this type of product requires a 220V AC fixed power supply and is not suitable for use in the wild. In order to enable this type of product to be used normally in the wild, a field automatic charging device is designed to power this type of product. Summary of the invention
[0003] The utility model provides a power supply device for a drone nest in the wild, and its purpose is to solve the problem that the existing DJI drone nest cannot supply power independently. In order to enable the drone nest used in the wild to complete the power supply smoothly and allow the drone to have sufficient power to complete the inspection, the utility model designs a power supply device for a drone nest in the wild. According to the characteristics of the DJI drone nest, a field power supply device suitable for the DJI drone nest is designed. At the same time, the control system and the flip unit are also used to achieve regular removal of debris above the solar panel.
[0004] In order to achieve the above-mentioned purpose, the utility model adopts the following technical scheme: a field UAV nest power supply device, including flip unit 1, flip unit 2, flip unit 3, flip unit 4, a UAV nest, an electric control box, and a field bracket;
[0005] The flip unit 1 includes a solar panel, a flip axis 1, a U-shaped bracket, a coupling, a large triangular bracket, a motor dust cover, a motor, a transverse bracket 1, a small triangular bracket, a coarse support profile 1, an electromagnet 1, a proximity switch 1, a proximity switch 2, a coarse nail foot, a transverse bracket 2, a fine nail foot, a fine support profile 1, a fine support profile 2, an electromagnet 2, a coarse support profile 2, an electromagnet 3, an electromagnet 4, and a flip axis 2, characterized in that: the coarse support profile 1 is fixed to the field bracket by the coarse nail foot, the coarse support profile 2 is fixed in the same manner as the coarse support profile 1 and is symmetrically distributed on the field bracket, the transverse bracket 2 is installed between the coarse support profile 2 and the coarse support profile 1 by eight small triangular brackets, the electromagnet 1 is fixed to the coarse support profile 1 by bolts, the electromagnet 2 is fixed to the coarse support profile 2 by bolts, and the electromagnet 1 and electromagnet 2 are symmetrically distributed and are respectively located at both ends of proximity switch 1. Proximity switch 1 is installed at the midpoint of horizontal bracket 2. Thin support profile 1 is installed on the field bracket through thin nail feet. Thin support profile 2 is fixed in the same way as thin support profile 1 and is symmetrically distributed on the field bracket. Electromagnet 3 is fixed to the top of thin support profile 1 through bolts. Electromagnet 4 is fixed to the top of thin support profile 2 through bolts. The motor is fixed to horizontal bracket 1 through a large triangular bracket. The large triangular bracket is connected to horizontal bracket 1 through bolts. Horizontal bracket 1 is fixed to thick support profile 1 through 4 small triangular brackets. The motor is connected to flip shaft 1 through a coupling. Flip shaft 1 is fixedly connected to the solar panel and coaxially matched with the U-shaped bracket. The motor dust cover is fixed to the outside of the motor through bolts. Flip shaft 2 is coaxially matched with the hole on the solar panel.
[0006] The flip unit 2, flip unit 3, and flip unit 4 have the same structure as the flip unit 1 and are symmetrically distributed on the field bracket front to back and left to right. The drone nest is connected to the field bracket by bolts and is located in the middle of the entire bracket. The electric control box is connected to the field bracket by bolts and is located between the flip unit 2 and the flip unit 3.
[0007] As a further description of the above technical solution, when the solar panel is rotated to a horizontal position, two electromagnets on the supporting profile will adsorb and fix it in this working position.
[0008] As a further description of the above technical solution, the solar panel rotates to a nearly vertical position close to a proximity switch, and the proximity switch receives a signal so that two electromagnets adsorb and stabilize it in a vertical position.
[0009] The utility model has the following advantages:
[0010] 1. In the utility model, the motor controls the flip axis 1 to realize the flipping of the solar panel, and the electromagnet and the proximity switch are used to control the position of the solar panel to make the flipping more stable.
[0011] 2. In the present utility model, when debris is detected on the solar panel during field work, the motor drives the solar panel to flip over and dump out the debris. BRIEF DESCRIPTION OF THE DRAWINGS
[0012] Figure 1 A schematic diagram of the position of a flip unit in the overall structure of a field drone nest power supply device proposed by the utility model;
[0013] Figure 2 A solar panel flip unit structure of a field drone nest power supply device proposed by the utility model;
[0014] Figure 3 The utility model discloses a specific structure for connecting a motor and a solar panel in a flip unit of a power supply device for a nest of a field unmanned aerial vehicle.
[0015] Figure 4 This is a schematic diagram of the overall structure of a field UAV nest power supply device proposed by the utility model;
[0016] In the figure: 1- flip unit 1; 2- flip unit 2; 3- flip unit 3; 4- flip unit 4; 5- drone nest; 6- electric control box; 7- field bracket; 8- solar panel; 9- flip axis 1; 10- U-shaped bracket; 11- coupling; 12- large triangular bracket; 13- motor dust cover; 14- motor; 15- horizontal bracket 1; 16- small triangular bracket; 17- thick support profile 1; 18- electromagnet 1; 19- proximity switch 1; 20- proximity switch 2; 21- thick nail foot; 22- horizontal bracket 2; 23- thin nail foot; 24- thin support profile 1; 25- thin support profile 2; 26- electromagnet 2; 27- thick support profile 2; 28- electromagnet 3; 29- electromagnet 4; 30- flip axis 2. DETAILED DESCRIPTION
[0017] Reference Figure 1 , a power supply device for a field drone nest, 1- flip unit 1; 2- flip unit 2; 3- flip unit 3; 4- flip unit 4; 5- drone nest; 6- electric control box; 7- field bracket; characterized in that: the flip unit 2, flip unit 3, flip unit 4 have the same structure as flip unit 1 and are symmetrically distributed on the field bracket front and back and left and right, the drone nest is connected to the field bracket by bolts and is located in the middle of the entire bracket, the electric control box is connected to the field bracket by bolts and is located between the flip unit 2 and the flip unit 3,
[0018] Furthermore, the flip unit 1 includes a solar panel, a flip axis 1, a U-shaped bracket, a coupling, a large triangular bracket, a motor dust cover, a motor, a transverse bracket 1, a small triangular bracket, a coarse support profile 1, an electromagnet 1, a proximity switch 1, a proximity switch 2, a coarse nail foot, a transverse bracket 2, a fine nail foot, a fine support profile 1, a fine support profile 2, an electromagnet 2, a coarse support profile 2, an electromagnet 3, an electromagnet 4, and a flip axis 2, characterized in that: the coarse support profile 1 is fixed to the field bracket by the coarse nail foot, the coarse support profile 2 is fixed in the same manner as the coarse support profile 1 and is symmetrically distributed on the field bracket, the transverse bracket 2 is installed between the coarse support profile 2 and the coarse support profile 1 by eight small triangular brackets, the electromagnet 1 is fixed to the coarse support profile 1 by bolts, the electromagnet 2 is fixed to the coarse support profile 2 by bolts, and the electromagnet 1 and the electromagnet 2 are symmetrically distributed, respectively. At both ends of the proximity switch 1, it can stabilize the solar panel to a vertical position when it is turned over. The proximity switch 1 is fixed by bolts at the midpoint of the horizontal bracket 2. The thin support profile 1 is installed on the field bracket by thin nail feet. The thin support profile 2 is fixed in the same way as the thin support profile 1 and is symmetrically distributed on the field bracket. The electromagnet 3 is fixed by bolts to the thin support profile 1. The electromagnet 4 is fixed by bolts to the top of the thin support profile 2. The motor is fixed to the horizontal bracket 1 through a large triangular bracket. The large triangular bracket is connected to the horizontal bracket 1 by bolts. The horizontal bracket 1 is fixed to the thick support profile 1 through 4 small triangular brackets. The motor is connected to the flip shaft 1 through a coupling. The flip shaft 1 is fixedly connected to the solar panel and coaxially matched with the U-shaped bracket. The motor dust cover is installed on the outside of the motor to prevent debris from entering and interfering with the motor. The flip shaft 2 is coaxially matched with the hollow space on the solar panel.
[0019] When working in the field, when fallen leaves and other debris appear on the solar panel, the motor drives the flip shaft 1 to rotate and then drives the solar panel to rotate to a nearly vertical position. During this process, the flip shaft 2 cooperates with the solar panel coaxially. When the solar panel approaches the proximity switch 1, the proximity switch 1 receives a signal so that the electromagnet 1 and the electromagnet 2 start working to adsorb the solar panel and stabilize it in a vertical position to dump out the debris. After dumping, the motor drives the flip shaft 1 to rotate and then drives the solar panel to rotate to a nearly horizontal position. During this process, the flip shaft 2 cooperates with the solar panel coaxially. When approaching the proximity switch 2, the proximity switch receives a signal so that the electromagnet 3 and the electromagnet 4 start working to adsorb the solar panel and stabilize it in a horizontal position to continue working to power the machine nest. Under sufficient sunlight, the solar panel machine nest in flip unit 1, flip unit 2, flip unit 3, and flip unit 4 is powered.
Claims
1. A power supply device for a field drone nest, comprising a flip unit 1 (1), a flip unit 2 (2), a flip unit 3 (3), a flip unit 4 (4), a drone nest (5), an electric control box (6), and a field bracket (7); The flip unit 1 (1) comprises a solar panel (8), a flip shaft 1 (9), a U-shaped bracket (10), a coupling (11), a large triangular bracket (12), a motor dust cover (13), a motor (14), a transverse bracket 1 (15), a small triangular bracket (16), a thick supporting profile 1 (17), an electromagnet 1 (18), a proximity switch 1 (19), a proximity switch 2 (20), a thick nail foot (21), a transverse bracket 2 (22), a thin nail foot (23), a thin supporting profile 1 (24), a thin supporting profile 2 (25), an electromagnet 2 (26), a thick supporting profile 2 (27), an electromagnet 3 (28), an electromagnet 4 (29), and a flip shaft 2 (30), characterized in that: The coarse support profile 1 (17) is fixed to the field support (7) by means of coarse nail feet (21); the coarse support profile 2 (27) is fixed in the same manner as the coarse support profile 1 (17) and is symmetrically distributed on the field support (7); the cross support 2 (22) is installed between the coarse support profile 2 (27) and the coarse support profile 1 (17) by means of eight small triangular brackets (16); the electromagnet 1 (18) is fixed to the coarse support profile 1 (17) by means of bolts; the electromagnet 2 (26) is fixed to the coarse support profile 2 (27) by means of bolts; the electromagnet 1 (18) and the electromagnet 2 (26) are symmetrically distributed and are respectively located at two ends of the proximity switch 1 (19); the proximity switch 1 (19) is fixed to the midpoint of the cross support 2 (22) by means of bolts; the thin support profile 1 (24) is installed on the field support (7) by means of thin nail feet (23); the thin support profile 2 (25) is fixed to the field support (7) by means of thin nail feet (23); The thin support profile 1 (24) is fixed in the same manner and symmetrically distributed on the field bracket (7), the electromagnet 3 (28) is fixed to the top of the thin support profile 1 (24) by bolts, the electromagnet 4 (29) is fixed to the top of the thin support profile 2 (25) by bolts, the motor (14) is fixed to the transverse bracket 1 (15) by a large triangular bracket (12), the large triangular bracket (12) is connected to the transverse bracket 1 (15) by bolts, the transverse bracket 1 (15) is fixed to the thick support profile 1 (17) by four small triangular brackets (16), the motor (14) is connected to the flip shaft 1 (9) by a coupling (11), the flip shaft 1 (9) is fixedly connected to the solar panel (8) and is coaxially matched with the U-shaped bracket (10), the motor dust cover (13) is fixed to the outside of the motor (14) by bolts, and the flip shaft 2 (30) is coaxially matched with the hole on the solar panel (8); The flip unit 2 (2), flip unit 3 (3), and flip unit 4 (4) have the same structure as the flip unit 1 (1) and are symmetrically distributed on the field bracket (7); the drone nest (5) is connected to the field bracket (7) by bolts and is located in the middle of the entire bracket; the electric control box (6) is connected to the field bracket (7) by bolts and is located between the flip unit 2 (2) and the flip unit 3 (3).