Unmanned aerial vehicle battery fixing structure

By designing the drone battery fixed structure of the case, battery compartment, hinge and cover, the problem of lack of protection in the battery compartment in the prior art is solved, effectively sealing dust and moisture, and improving the stability of the battery and the power supply performance of the drone.

CN222546521UActive Publication Date: 2025-02-28TIANJIN RED DOT NEW ENERGY TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202421024262.7
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-13
Publication Date
2025-02-28
Estimated Expiration
2034-05-13

AI Technical Summary

Technical Problem

The existing UAV battery fixed structure lacks effective protective measures, which leads to easy penetration of dust and debris and moisture into the battery compartment, affecting battery stability and power supply performance of the UAV.

Method used

A drone battery fixing structure including a housing, a battery compartment, a hinge and a cover plate is designed. The hinged cover plate on the outside of the housing is sealed with the open end of the battery compartment, and the fastening design of the rotor and ear block ensures that the cover plate is stable and blocked and reduces dust and moisture infiltration.

Benefits of technology

Effectively prevent dust and debris and moisture from entering the battery compartment, improve the battery stability and the power supply reliability of the drone, and facilitate the disassembly and assembly and replacement of the battery.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of unmanned aerial vehicle battery fixing structures, in particular to an unmanned aerial vehicle battery fixing structure which comprises a shell, two sets of battery bins for fixing an unmanned aerial vehicle battery are arranged on the inner side of the shell, a plurality of sets of hinges are assembled on the surface of the outer side wall of the shell through screws, and the outer side wall of the shell is provided with a plurality of fixing holes. A cover plate for blocking the battery compartment is assembled at one end, far away from the shell, of the hinge through a screw; when a battery used by the unmanned aerial vehicle is installed on the inner side of the battery bin, the cover plate hinged to the outer side of the shell through the hinge is used for conveniently blocking the open end of the battery bin and conveniently protecting the battery bin, so that the condition that dust, chippings or water permeates into the battery bin is reduced, and the battery in the battery bin on the inner side of the shell can operate more stably; and power can be conveniently supplied to the unmanned aerial vehicle.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle battery fixing structures, and in particular to a unmanned aerial vehicle battery fixing structure. Background Art

[0002] With the continuous development of science and technology, in recent years, drone technology has been greatly improved, and many intelligent and multifunctional unmanned aerial vehicles have emerged. Drones can realize real-time image transmission and high-risk area detection functions by carrying various types of sensors. At present, they are widely used in industries, specifically in aerial photography, surveying and mapping, plant protection, detection, disaster relief, etc.; Patent No. CN202021283026.9 discloses a drone battery fixing structure and a drone, which is used to fix the power supply on the drone body. The drone battery fixing structure includes a power supply compartment and a power supply fixing mechanism; the power supply fixing mechanism is installed on the power supply; a push-out piece is provided in the power supply compartment. When the power supply is fixed in the power supply compartment through the power supply fixing mechanism, the push-out piece abuts against the power supply, and the push-out piece is in a compressed energy storage state. When the power supply fixing mechanism unlocks the fixed connection between the power supply and the power supply compartment, the push-out piece will push the power supply out; however, since the battery used by the drone is directly installed on the inside of the battery compartment, and there is no good protective structure on the outside of the battery compartment, some dust and debris are easy to penetrate into the battery compartment, and the infiltrated dust and debris are easy to cause a certain impact on the battery. To this end, we propose a drone battery fixing structure. Utility Model Content

[0003] In view of the problems in the prior art, the utility model provides a battery fixing structure for an unmanned aerial vehicle.

[0004] The technical solution adopted by the utility model to solve the technical problem is a drone battery fixing structure, comprising a shell, a battery compartment for fixing drone batteries is arranged inside the shell, and the battery compartment has two groups, a hinge is assembled on the outer wall surface of the shell by screws, and the hinge has multiple groups, and a cover plate for sealing the battery compartment is assembled on the end of the hinge away from the shell by screws;

[0005] An ear block for support is integrally constructed at one end of the outer periphery of the cover plate away from the hinge, and pin holes for connection are provided on the outer periphery of the ear block and the outer wall surface of the shell, and a rotating rod for fixing is screwed into the inner side of the pin hole.

[0006] By adopting the above technical solution, when the battery used by the drone is installed inside the battery compartment, the cover plate hinged by the hinge on the outside of the shell is convenient for blocking the open end of the battery compartment, so as to protect the battery compartment, thereby reducing the infiltration of dust, debris or moisture, so that the battery in the battery compartment inside the shell can operate more stably and conveniently power the drone;

[0007] When the cover plate seals the battery compartment outside the shell, it is convenient to screw the rotary rod and the pin hole on the surface of the ear block outside the cover plate together, and at the same time, the rotary rod passes through the pin hole on the surface of the ear block and screws with the pin hole on the outer surface of the shell, which is convenient for tightening the position of the cover plate, so that the cover plate can seal and protect the battery compartment more stably, so that the battery inside the battery compartment can operate more safely and stably, and it is convenient to control the opening and closing, and to disassemble and replace the battery inside the battery compartment.

[0008] Specifically, the outer peripheral surface of the shell is provided with frame grooves located around the battery compartment, and there are two groups of frame grooves. The cover plate is integrally constructed with a frame body that fits and connects with the frame grooves on one side close to the battery compartment.

[0009] By adopting the above technical solution, the frame body and the frame groove are fitted and connected with each other, which is convenient for improving the tightness of the cover plate when sealing the battery compartment.

[0010] Specifically, a rubber pad that can be used to prevent leakage is bonded to the inner bottom surface of the frame groove.

[0011] By adopting the above technical solution, the rubber pad is convenient for improving the tightness of the frame body and the frame groove after being connected, and is convenient for further improving the airtightness of the cover plate when sealing the battery compartment.

[0012] Specifically, a handle is mounted on the outer side wall surface of the cover plate.

[0013] By adopting the above technical solution, the handle makes it more convenient to open and close the cover.

[0014] Specifically, a wiring socket is mounted on the top surface of the shell.

[0015] By adopting the above technical solution, the terminal block facilitates the connection between the battery inside the battery compartment and the circuit inside the drone, thereby facilitating power supply for the drone.

[0016] Specifically, a side of the cover plate close to the battery compartment is provided with grooves that can be used for connection, and there are multiple groups of grooves. A memory foam pad that can be used for protection is bonded to a side of the cover plate located on the inner side of the battery compartment.

[0017] By adopting the above technical solution, the multiple groups of grooves on the surface of the cover plate are conveniently fitted and connected with the protrusions on the inner side of the battery compartment, which is convenient for improving the stability of the cover plate when sealing. At the same time, the memory foam pad is convenient for protecting the cover plate and the battery, thereby reducing the friction between the cover plate and the battery and causing scratches.

[0018] Compared with the prior art, the utility model has the following beneficial effects:

[0019] 1. The technical solution of the present application adopts the design of the shell, battery compartment, hinge and cover. When the battery used by the drone is installed on the inner side of the battery compartment, the cover hinged on the outer side of the shell is used to seal the open end of the battery compartment, thereby protecting the battery compartment and reducing the infiltration of dust, debris or moisture, so that the battery in the battery compartment inside the shell can operate more stably and conveniently power the drone.

[0020] 2. The technical solution of the present application adopts the design of ear blocks, pin holes and rotating rods. When the cover plate blocks the battery compartment outside the shell, it is convenient to screw the rotating rod and the pin hole on the surface of the ear block on the outside of the cover plate together. At the same time, the rotating rod passes through the pin hole on the surface of the ear block and screws with the pin hole on the outer surface of the shell, which is convenient for tightening the position of the cover plate, so that the cover plate can seal and protect the battery compartment more stably, so that the battery inside the battery compartment can operate more safely and stably, and it is convenient to control the opening and closing, and to disassemble and replace the battery inside the battery compartment. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The utility model is further described below in conjunction with the accompanying drawings and embodiments.

[0022] Figure 1 It is an axonometric drawing of the utility model;

[0023] Figure 2 This is a schematic diagram of the inner structure of the battery compartment of the utility model;

[0024] Figure 3 This is a schematic diagram of the cover structure of the utility model;

[0025] In the figure: 1. Shell; 2. Battery compartment; 3. Hinge; 4. Cover; 5. Ear block; 6. Pin hole; 7. Rotary rod; 8. Frame slot; 9. Frame; 10. Rubber pad; 11. Groove; 12. Memory foam pad; 13. Handle; 14. Terminal block. DETAILED DESCRIPTION

[0026] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.

[0027] See also Figure 1-3The embodiment of the utility model provides a technical solution: a battery fixing structure for a drone, comprising a shell 1, a battery compartment 2 for fixing the drone battery is arranged on the inner side of the shell 1, and the battery compartment 2 has two groups, a hinge 3 is assembled on the outer wall surface of the shell 1 by screws, and the hinge 3 has multiple groups, and a cover plate 4 for sealing the battery compartment 2 is assembled on the end of the hinge 3 away from the shell 1 by screws; an ear block 5 for support is integrally constructed on the end of the outer periphery of the cover plate 4 away from the hinge 3, and the outer periphery of the ear block 5 and the outer wall surface of the shell 1 are both provided with pin holes 6 for connection, and a rotating rod 7 for fixing is screwed and installed inside the pin hole 6.

[0028] When the battery used by the drone is installed inside the battery compartment 2, the cover plate 4 hinged by the hinge 3 on the outside of the shell 1 is convenient for blocking the open end of the battery compartment 2, so as to protect the battery compartment 2 and reduce the infiltration of dust, debris or moisture, so that the battery in the battery compartment 2 inside the shell 1 can operate more stably and conveniently power the drone;

[0029] When the cover plate 4 blocks the battery compartment 2 outside the shell 1, it is convenient to screw the rotary rod 7 and the pin hole 6 on the surface of the ear block 5 outside the cover plate 4 together, and at the same time, the rotary rod 7 passes through the pin hole 6 on the surface of the ear block 5 and screws with the pin hole 6 on the outer surface of the shell 1, so as to tighten the position of the cover plate 4, so that the cover plate 4 can seal and protect the battery compartment 2 more stably, so that the battery inside the battery compartment 2 can operate more safely and stably, and it is convenient to control the opening and closing, and to disassemble and replace the battery inside the battery compartment 2.

[0030] like Figure 2 and Figure 3 As shown, the outer surface of the shell 1 is provided with frame grooves 8 around the battery compartment 2, and there are two groups of frame grooves 8. The cover plate 4 is integrally constructed with a frame body 9 that fits and connects with the frame grooves 8 on one side close to the battery compartment 2.

[0031] When in use, the frame body 9 and the frame groove 8 are fitted and connected with each other, so as to improve the tightness of the cover plate 4 when sealing the battery compartment 2 .

[0032] like Figure 2 As shown, a rubber pad 10 for preventing leakage is bonded to the inner bottom surface of the frame groove 8 .

[0033] When in use, the rubber pad 10 is convenient for improving the tightness of the frame body 9 and the frame groove 8 after being connected, and is convenient for further improving the airtightness of the cover plate 4 when sealing the battery compartment 2.

[0034] like Figure 1 As shown, a handle 13 is mounted on the outer side wall surface of the cover plate 4.

[0035] When in use, the handle 13 makes it more convenient to open and close the cover plate 4.

[0036] like Figure 1 As shown, a wiring seat 14 is mounted on the top surface of the housing 1 .

[0037] When in use, the connection socket 14 facilitates the connection between the battery inside the battery compartment 2 and the circuit inside the drone, so as to provide power for the drone.

[0038] like Figure 3 As shown, a side of the cover plate 4 close to the battery compartment 2 is provided with a groove 11 for connection, and there are multiple groups of grooves 11. A side of the cover plate 4 located on the inner side of the battery compartment 2 is bonded with a memory foam pad 12 for protection.

[0039] When in use, the multiple groups of grooves 11 on the surface of the cover plate 4 are conveniently fitted and connected with the protrusions on the inner side of the battery compartment 2, so as to improve the stability of the cover plate 4 when sealing. At the same time, the memory foam pad 12 is convenient for protecting the cover plate 4 and the battery, thereby reducing the friction between the cover plate 4 and the battery and causing scratches.

[0040] The working principle and use process of the utility model are as follows: when in use, firstly, the corresponding structural components are installed in the appropriate position. When the battery used by the drone is installed on the inner side of the battery compartment 2, the cover plate 4 hinged by the hinge 3 on the outer side of the shell 1 is convenient for sealing the open end of the battery compartment 2, so as to protect the battery compartment 2, thereby reducing the infiltration of dust, debris or moisture, so that the battery in the battery compartment 2 on the inner side of the shell 1 can operate more stably and conveniently power the drone. At the same time, when the cover plate 4 seals the battery compartment 2 on the outer side of the shell 1, it is convenient to screw the rotating rod 7 and the pin hole 6 on the surface of the ear block 5 on the outer side of the cover plate 4 together. At the same time, the rotating rod 7 passes through the pin hole 6 on the surface of the ear block 5 and screws with the pin hole 6 on the outer surface of the shell 1, so as to tighten the position of the cover plate 4, so that the cover plate 4 can more stably seal and protect the battery compartment 2, so that the battery inside the battery compartment 2 can operate more safely and stably, and it is convenient to control the opening and closing, and it is convenient to disassemble and replace the battery inside the battery compartment 2.

[0041] The above shows and describes the basic principles, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions in the specification are only to illustrate the principles of the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the protection required by the utility model. The scope of protection required by the utility model is defined by the attached claims and their equivalents.

Claims

1. A drone battery fixing structure, characterized in that: The invention comprises a shell (1), wherein a battery compartment (2) for fixing a battery of an unmanned aerial vehicle is arranged inside the shell (1), and the battery compartment (2) has two groups, a hinge (3) is assembled on the outer wall surface of the shell (1) by means of screws, and the hinge (3) has multiple groups, and a cover plate (4) for sealing the battery compartment (2) is assembled on the end of the hinge (3) away from the shell (1) by means of screws; An ear block (5) for supporting is integrally formed at one end of the outer periphery of the cover plate (4) away from the hinge (3), and a pin hole (6) for connecting is provided on the outer periphery of the ear block (5) and the outer wall surface of the shell (1), and a rotating rod (7) for fixing is screwedly installed inside the pin hole (6).

2. The battery fixing structure of a drone according to claim 1, characterized in that: The outer peripheral surface of the shell (1) is provided with frame grooves (8) located around the battery compartment (2), and there are two groups of frame grooves (8). The cover plate (4) is integrally constructed with a frame body (9) that is fitted and connected to the frame grooves (8) on one side close to the battery compartment (2).

3. The battery fixing structure of a drone according to claim 2, characterized in that: A rubber pad (10) that can be used to prevent leakage is bonded to the inner bottom surface of the frame groove (8).

4. The drone battery fixing structure according to claim 1, characterized in that: A handle (13) is mounted on the outer wall surface of the cover plate (4).

5. The drone battery fixing structure according to claim 1, characterized in that: A wiring seat (14) is mounted on the top surface of the housing (1).

6. The drone battery fixing structure according to claim 1, characterized in that: A groove (11) that can be used for connection is provided on one side of the cover plate (4) close to the battery compartment (2), and there are multiple groups of grooves (11). A memory foam pad (12) that can be used for protection is bonded to one side of the cover plate (4) located inside the battery compartment (2).

Citation Information

Patent Citations

  • Unmanned aerial vehicle battery fixing structure and unmanned aerial vehicle

    CN212136557U