Sky end structure of unmanned aerial vehicle mooring device
By designing an air-end structure for a UAV tethering device that includes components such as a battery holder, a beveled baffle, a heat sink, etc., the problem of unstable power supply during UAV flight due to complex structures in the existing technology has been solved, and a wireless power supply has been achieved. Continuous and stable power supply for humans and machines during flight.
Patent Information
- Application Number
- CN202420518288.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-03-18
- Publication Date
- 2025-01-24
- Estimated Expiration
- 2034-03-18
AI Technical Summary
Due to the complex structure of the existing drone tethering device, the sky end structure is not conducive to the continuous and stable power supply of the drone during flight.
An air end structure of a UAV tethering device is designed, including the air end shell, battery holder, inclined baffle, heat sink, battery adapter plug, power inlet and outlet connector and battery buckle. The stability of the battery is achieved through these components. Support, cooling and power supply.
The continuous and stable power supply of drones is achieved, the structure is simple and lightweight, easy to maintain, and widely adapted, ensuring the flying power supply of drones.
Smart Images

Figure CN222388378U_ABST
Abstract
Description
Technical Field
[0001] The utility model mainly relates to the technical field of unmanned aerial vehicle devices, in particular to a sky end structure of a tethered device for an unmanned aerial vehicle. Background Art
[0002] Unmanned aerial vehicles, also known as "drones", or "UAVs" in English, are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices, or are operated completely or intermittently autonomously by onboard computers. Compared with manned aircraft, drones are often more suitable for tasks that are too "dull, dirty or dangerous". Drones can be divided into military and civilian applications according to their application areas. The movement and flight of drones cannot be separated from the supply of electricity. The sky end of the drone tethering device is a convenient way to power the drone. The sky end can connect to the ground to supply power to the drone when the drone is working. However, when the sky end of the drone tethering device used for drones in the prior art is used, since the sky end of the drone tethering device needs to be loaded with batteries, in order to provide protection for the batteries, its structure is complex, which is not conducive to the continuous and stable power supply of the drone when it is working. Therefore, we provide a sky end structure of a drone tethering device to solve the defects of the prior art. Utility Model Content
[0003] The utility model mainly provides a sky end structure of a drone tethering device, which is used to solve the technical problems raised in the above-mentioned background technology.
[0004] The technical solution adopted by the utility model to solve the above technical problems is:
[0005] A sky end structure of a drone tethering device comprises a sky end shell, a battery holder 1 is provided at the front end of the bottom inner side of the sky end shell, a battery holder 2 is provided at the rear end of the bottom inner side of the sky end shell, an inclined baffle is provided on the right side of the top of the battery holder 1 and the battery holder 2, a plurality of heat sinks equidistantly distributed in a straight line are fixedly connected to the right side of the inclined baffle, a battery adapter plug is fixedly connected to the center of the inner side plate of the sky end shell, a power input and output connector is fixedly connected to the bottom of the sky end shell, a battery buckle is provided at the center of the front end of the sky end shell, and an antenna assembly is fixedly connected to the bottom of the front end of the sky end shell.
[0006] Furthermore, the front end of the bottom of the inclined baffle is fixedly connected to a second mounting plate, the rear end of the bottom of the inclined baffle is fixedly connected to a first mounting plate, and the inclined baffle is fixedly connected to the sky end housing via a mounting piece.
[0007] Furthermore, the inclined baffle is fixedly connected to the top of the battery holder 1 through a mounting plate 2 arranged at the bottom by bolts, and the inclined baffle is fixedly connected to the top of the battery holder 2 through a mounting plate 1 arranged at the bottom by bolts.
[0008] Furthermore, a fixing block is fixedly connected to the top of the front end of the sky end housing, a latch is provided on the top of the fixing block, and the latch passes through an outer sleeve of the fixing block and is provided with a spring.
[0009] Furthermore, the battery buckle is engaged with the center of the front end of the sky end housing, the top of the fixing block is slidably connected with the latch, and the latch is slidably connected with the penetration point of the fixing block.
[0010] Furthermore, the battery holder 1 is fixedly connected to the inner side of the sky end housing by bolts, and the battery holder 2 is fixedly connected to the inner side of the sky end housing by bolts.
[0011] Compared with the prior art, the beneficial effects of the utility model are:
[0012] The purpose of the utility model is to provide a sky end structure of a UAV tethering device, which can realize power supply within the range of the UAV during flight, ensure that the UAV has a continuous and stable power supply during flight, assist the UAV in power supply during flight when in use, ensure the coordination between the UAV sky end and the ground end, and assist the UAV at the automatic airport to have a continuous and stable power supply during flight. The structure is simple and lightweight, reasonably stable, widely adaptable, easy to maintain, and conducive to the continuous and stable power supply of the UAV during operation.
[0013] The present invention will be explained in detail below with reference to the accompanying drawings and specific embodiments. BRIEF DESCRIPTION OF THE DRAWINGS
[0014] Figure 1 It is a schematic diagram of the overall front view structure of the utility model;
[0015] Figure 2 It is a schematic diagram of the overall structure of the utility model when viewed from above.
[0016] In the figure: 1. Sky end housing; 2. Battery holder 1; 3. Antenna assembly; 4. Battery buckle; 5. Battery adapter plug; 6. Power input and output connector; 7. Slanted baffle; 8. Heat sink; 9. Mounting piece; 10. Mounting plate 1; 11. Mounting plate 2; 12. Battery holder 2; 13. Fixing block; 14. Spring; 15. Latch. DETAILED DESCRIPTION
[0017] In order to facilitate the understanding of the present invention, the present invention will be described in more detail below with reference to the relevant drawings. Several embodiments of the present invention are given in the drawings, but the present invention can be implemented in different forms and is not limited to the embodiments described in the text. On the contrary, these embodiments are provided to make the content disclosed in the present invention more thorough and comprehensive.
[0018] For examples, please refer to the attached Figure 1-2As shown, a sky end structure of a drone tethering device includes a sky end shell 1, a battery holder 1 2 is provided at the front end of the inner bottom of the sky end shell 1, a battery holder 2 12 is provided at the rear end of the inner bottom of the sky end shell 1, an inclined baffle 7 is provided on the right side of the top of the battery holder 1 2 and the battery holder 2 12, a plurality of heat sinks 8 equidistantly distributed in a straight line are fixedly connected to the right side of the inclined baffle 7, a battery adapter plug 5 is fixedly connected to the center of the inner side panel of the sky end shell 1, a power input and output connector 6 is fixedly connected to the bottom of the sky end shell 1, a battery buckle 4 is provided at the center of the front end of the sky end shell 1, and an antenna assembly 3 is fixedly connected to the bottom of the front end of the sky end shell 1.
[0019] Among them, the front end of the bottom of the inclined baffle 7 is fixedly connected with a mounting plate 2 11, the rear end of the bottom of the inclined baffle 7 is fixedly connected with a mounting plate 10, the inclined baffle 7 is fixedly connected to the sky end housing 1 through a mounting piece 9, the inclined baffle 7 is fixedly connected to the top of the battery holder 2 through the mounting plate 2 11 arranged at the bottom through bolts, and the inclined baffle 7 is fixedly connected to the top of the battery holder 2 12 through the mounting plate 10 arranged at the bottom through bolts, the antenna combination 3 is arranged to cooperate with the drone to receive signals, the battery adapter plug 5 is arranged to transfer the transition battery and the battery compartment, and the power input and output connector 6 is installed under the sky end housing 1. When the drone is flying, the power input and output connector 6 ensures that the overall structure of the drone is connected to the ground end when working to ensure power supply during the flight. At the same time, the inclined baffle 7 is fitted with the battery, and a number of heat sinks 8 arranged on the inclined baffle 7 can be used to cooperate with the battery and facilitate battery heat dissipation. By adopting the utility model, the structure is simple and lightweight, and the drone is stably and continuously powered when the drone is flying.
[0020] Among them, a fixing block 13 is fixedly connected to the top of the front end of the sky end housing 1, a latch 15 is provided on the top of the fixing block 13, the latch 15 passes through the outer side of the fixing block 13 and is sleeved with a spring 14, a battery buckle 4 is clamped with the center of the front end of the sky end housing 1, the top of the fixing block 13 is slidably connected with the latch 15, and the latch 15 is slidably connected with the penetration point of the fixing block 13, the battery buckle 4 can be clamped to the battery, and at the same time, the latch 15 cooperates with the spring 14 to limit the battery buckle 4, thereby preventing the battery from falling off during flight.
[0021] Among them, battery holder 1 2 is fixedly connected to the inner side of the sky end shell 1 by bolts, and battery holder 2 12 is fixedly connected to the inner side of the sky end shell 1 by bolts. The battery is inserted into the sky end shell 1. The set battery holder 1 2 and battery holder 2 12 can provide stable support for the battery, and then the sky end shell 1 and the drone are assembled by bolts.
[0022] The specific operation mode of the utility model is as follows:
[0023] First, insert the battery into the sky end housing 1, the battery holder 1 2 and the battery holder 2 12 can provide stable support for the battery, then assemble the sky end housing 1 and the drone by bolts, and the battery clip 4 can clip the battery, and at the same time, the latch 15 cooperates with the spring 14 to limit the battery clip 4, thereby preventing the battery from falling off during flight, the antenna combination 3 cooperates with the drone to receive signals, the battery adapter plug 5 is used to transfer the transition battery and the battery compartment, and the power input and output connector 6 is installed under the sky end housing 1. When the drone is flying, the power input and output connector 6 ensures that the overall structure of the drone is connected to the ground end when it is working to ensure power supply during flight. At the same time, the inclined baffle 7 is fitted with the battery, and the several heat sinks 8 arranged on the inclined baffle 7 can be used to cooperate with the battery and facilitate battery heat dissipation. The utility model has a simple and lightweight structure, and can provide stable and continuous power supply to the drone when the drone is flying.
[0024] The above description of the utility model in combination with the accompanying drawings is an exemplary description. Obviously, the specific implementation of the utility model is not limited to the above-mentioned method. As long as the non-substantial improvements are made by adopting the method concept and technical solution of the utility model, or the concept and technical solution of the utility model are directly applied to other occasions without improvement, they are all within the protection scope of the utility model.
Claims
1. A sky end structure of a drone tethering device, comprising a sky end housing (1), characterized in that: A battery holder 1 (2) is provided at the front end of the bottom inner side of the sky end housing (1), a battery holder 2 (12) is provided at the rear end of the bottom inner side of the sky end housing (1), an inclined baffle (7) is provided on the right side of the top of the battery holder 1 (2) and the battery holder 2 (12), a plurality of heat sinks (8) equidistantly distributed in a straight line are fixedly connected to the right side of the inclined baffle (7), a battery adapter plug (5) is fixedly connected at the center of the inner side plate of the sky end housing (1), a power input and output connector (6) is fixedly connected at the bottom of the sky end housing (1), a battery buckle (4) is provided at the center of the front end of the sky end housing (1), and an antenna assembly (3) is fixedly connected to the bottom of the front end of the sky end housing (1).
2. The sky end structure of the drone tethering device according to claim 1, characterized in that: The front end of the bottom of the inclined baffle (7) is fixedly connected to a second mounting plate (11), the rear end of the bottom of the inclined baffle (7) is fixedly connected to a first mounting plate (10), and the inclined baffle (7) is fixedly connected to the sky end housing (1) via a mounting member (9).
3. The sky end structure of the drone tethering device according to claim 2, characterized in that: The inclined baffle (7) is fixedly connected to the top of the battery tray (2) through the second mounting plate (11) arranged at the bottom by bolts, and the inclined baffle (7) is fixedly connected to the top of the battery tray (12) through the first mounting plate (10) arranged at the bottom by bolts.
4. The sky end structure of the drone tethering device according to claim 1, characterized in that: A fixing block (13) is fixedly connected to the top of the front end of the sky end housing (1), a latch (15) is provided on the top of the fixing block (13), and a spring (14) is sleeved on the outer side of the latch (15) which passes through the fixing block (13).
5. The sky end structure of the drone tethering device according to claim 4, characterized in that: The battery buckle (4) is snap-fitted to the front center of the sky end housing (1), the top of the fixing block (13) is slidably connected to the latch (15), and the latch (15) is slidably connected to the through-hole of the fixing block (13).
6. The sky end structure of the drone tethering device according to claim 1, characterized in that: The battery holder 1 (2) is fixedly connected to the inner side of the sky end housing (1) by means of bolts, and the battery holder 2 (12) is fixedly connected to the inner side of the sky end housing (1) by means of bolts.