Fixing cover for battery compartment of unmanned aerial vehicle
By designing a rotatable drone battery compartment fixing cover, the rotating disc and gear system are used to fix the battery compartment of different sizes, and the impact force is released through the combination of dampers and springs, the fixing cover in the prior art is solved. Adjustment and easy damage issues improve fixation effect and service life.
Patent Information
- Application Number
- CN202421033402.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-13
- Publication Date
- 2025-02-11
- Estimated Expiration
- 2034-05-13
AI Technical Summary
The existing drone battery compartment fixed cover cannot be adjusted according to the size of the battery compartment and battery, and there are restrictions on use, and it is susceptible to external impact damage when flying and landing, reducing service life.
A rotatable fixed cover is designed, which drives the rotating rod, gear and threaded rod to rotate through the rotating disc, and drives the thread sleeve, support rod and fixed cover plate to move to one side, making it closely fit with the bottom of the battery compartment to achieve fixed. At the same time, the combination of dampers and springs can effectively release impact force and protect the fixing cover from damage.
This design can be fixed according to different sizes of battery compartments and batteries, eliminating usage restrictions, improving fixing effect and practicality, and extending the service life of the fixed cover by effectively releasing impact force.
Smart Images

Figure CN222463275U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle battery compartments, and in particular to a fixed cover for an unmanned aerial vehicle battery compartment. Background Art
[0002] The domestic drone market has been developing for nearly 30 years, gradually expanding from the initial military field to the consumer field. The domestic consumer drone market is booming, and the recognition and demand of ordinary people for drones are gradually increasing. Drones often need to cope with high-speed flight, rotation, flipping and other flight conditions, as well as various severe weather conditions. As a drone powered by electricity and batteries as a power carrier, the battery compartment protective cover is the best barrier for the power carrier, and the battery compartment needs to be fixed with a fixed cover;
[0003] The current fixed cover is usually a cover plate. During use, the fixed cover is usually snapped onto the bottom of the battery compartment. However, in actual use, due to the different sizes of the battery compartment and the battery, the current fixed cover is usually of a fixed size and cannot be adjusted according to the size of the battery compartment and the battery. It can only be used in combination with a matching battery compartment, and has certain usage restrictions. At the same time, the current fixed cover does not have a protective function. Since the fixed cover is usually installed at the bottom of the drone, the drone is susceptible to collisions caused by external factors when it lands during flight. If it is hit, the impact force cannot be effectively released, resulting in damage to the fixed cover and reducing the service life of the fixed cover. Therefore, we provide a fixed cover for a drone battery compartment. Utility Model Content
[0004] 1. Technical issues to be solved
[0005] In view of the deficiencies in the prior art, the purpose of the utility model is to provide a fixed cover for a battery compartment of an unmanned aerial vehicle, by rotating a rotating disk, driving a rotating rod, a first gear, a second gear and a threaded rod to rotate through the rotating disk, and driving a threaded sleeve, a support rod and a fixed cover plate to move to one side through the threaded rod, so that one side of the fixed cover plate is tightly fitted with the bottom of the battery compartment, and fixation is completed. Battery compartments and batteries of different sizes can be fixed without usage restrictions, and the fixing effect is better and the practicability is strong, so as to solve the problems raised in the above-mentioned background technology.
[0006] (II) Technical solution
[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a technical solution adopted by a fixed cover for a battery compartment of an unmanned aerial vehicle is: it includes a base plate, a rear end of the base plate is fixedly connected to a support plate, the top of the support plate is fixedly connected to a connecting box, a rotating rod is movably connected to the center of the top of the connecting box, the top of the rotating rod is fixedly connected to a rotating disk, the surface of the rotating disk and the inner cavity of the connecting box are fixedly connected to a first gear, both sides of the first gear are meshed with second gears, one side of the second gear is fixedly connected to a threaded rod, the surface of the threaded rod is threadedly connected to a threaded sleeve, the surface of the threaded sleeve is fixedly connected to the support rod, and one side of the support rod is fixedly connected to a fixed cover plate.
[0008] As a preferred solution, dampers are fixedly connected around the bottom of the base plate, springs are wound around the surface of the dampers, and a connecting plate is fixedly connected to the bottom of the dampers.
[0009] Optionally, when the drone lands during flight and the bottom is hit by external factors, the impact object contacts the bottom of the connecting plate, and the impact force generated by the collision drives the connecting plate to move upward, and the spring and damper are squeezed through the connecting plate. The impact force is effectively released through the characteristics of the spring, and the fixed cover will not be damaged when hit, thereby increasing its service life.
[0010] As a preferred solution, mounting blocks are fixedly connected to both sides of the bottom of the connection box, and the mounting blocks and the support plates are fixedly connected by mounting bolts.
[0011] Optionally, the provision of mounting blocks and mounting bolts facilitates the user to install the connection box.
[0012] As a preferred solution, bearings are fixedly connected to both sides of the inner cavity of the connection box, and one side of the threaded rod is fixedly connected to the inner ring of the bearing.
[0013] Optionally, the wear of the threaded rod during rotation is reduced by providing a bearing.
[0014] As a preferred solution, both sides of the bottom of the inner cavity of the connection box are provided with sliding grooves, the bottom of the threaded sleeve is fixedly connected with a sliding block, and the bottom of the sliding block is slidably connected to the inner cavity of the sliding groove.
[0015] Optionally, the jitter of the threaded sleeve during movement is reduced by setting the slide groove and the slider.
[0016] As a preferred solution, a box door is movably connected to the back of the connection box, and a handle is fixedly connected to the lower end of the surface of the box door.
[0017] Optionally, the provision of a box door and a handle facilitates the user to clean and wipe the inner cavity of the connection box.
[0018] (III) Beneficial effects
[0019] Compared with the prior art, the utility model provides a fixed cover for a battery compartment of a drone, which has the following beneficial effects.
[0020] 1. The utility model rotates the rotating disk, and drives the rotating rod, the first gear, the second gear and the threaded rod to rotate through the rotating disk, and drives the threaded sleeve, the support rod and the fixed cover plate to move to one side through the threaded rod, so that one side of the fixed cover plate is tightly fitted with the bottom of the battery compartment, and the fixation is completed. Battery compartments and batteries of different sizes can be fixed without usage restrictions, the fixing effect is better, and the practicability is strong.
[0021] 2. When the drone lands during flight, the bottom is hit by external factors. The impact object contacts the bottom of the connecting plate. The impact force generated by the collision drives the connecting plate to move upward, and the spring and damper are squeezed through the connecting plate. The impact force is effectively released through the characteristics of the spring. When hit, the fixed cover will not be damaged, thereby increasing its service life. BRIEF DESCRIPTION OF THE DRAWINGS
[0022] Figure 1 It is a three-dimensional schematic diagram of the structure of the utility model;
[0023] Figure 2 This is a back view of the connection box of the utility model;
[0024] Figure 3 This is a cross-sectional view of the connection box of the utility model.
[0025] In the figure: 1. rotating rod; 2. rotating disk; 3. connecting box; 4. supporting rod; 5. supporting plate; 6. bottom plate; 7. connecting plate; 8. fixed cover plate; 9. spring; 10. damper; 11. mounting bolt; 12. mounting block; 13. first gear; 14. second gear; 15. threaded rod; 16. threaded sleeve; 17. bearing; 18. slide groove; 19. slider. DETAILED DESCRIPTION
[0026] The following is a further detailed description of the implementation of the present invention in conjunction with the accompanying drawings and examples. The following examples are used to illustrate the present invention, but cannot be used to limit the scope of the present invention.
[0027] See also Figure 1-3 , the embodiments of the utility model will be further described below in conjunction with the accompanying drawings.
[0028] Example
[0029] A technical solution adopted by a fixed cover for a battery compartment of an unmanned aerial vehicle is as follows: it includes a base plate 6, a support plate 5 is fixedly connected to the rear end of the base plate 6, a connection box 3 is fixedly connected to the top of the support plate 5, a rotating rod 1 is movably connected to the center of the top of the connection box 3, a rotating disk 2 is fixedly connected to the top of the rotating rod 1, a first gear 13 is fixedly connected to the surface of the rotating disk 2 and located in the inner cavity of the connection box 3, second gears 14 are meshed on both sides of the first gear 13, a threaded rod 15 is fixedly connected to one side of the second gear 14, a threaded sleeve 16 is threadedly connected to the surface of the threaded rod 15, a support rod 4 is fixedly connected to the surface of the threaded sleeve 16, and a fixed cover plate 8 is fixedly connected to one side of the support rod 4.
[0030] Specifically: when the drone battery compartment needs to be fixed, the user holds the rotating disk 2 and rotates the rotating disk 2 clockwise, drives the rotating rod 1 to rotate through the rotating disk 2, drives the first gear 13 to rotate through the rotating rod 1, drives the second gear 14 to rotate through the first gear 13, and drives the threaded rod 15 to rotate through the second gear 14. Since the threads of the threaded rod 15 are opposite, the threaded sleeve 16 is driven to move to the opposite side through the threaded rod 15, drives the support rod 4 to move to one side through the threaded sleeve 16, and drives the fixed cover plate 8 to move to one side through the support rod 4, so that one side of the fixed cover plate 8 is tightly fitted with both sides of the bottom of the battery compartment, and the fixation is completed. Battery compartments and batteries of different sizes can be fixed without usage restrictions, the fixing effect is better, and the practicability is strong.
[0031] Damper 10 is fixedly connected to all around the bottom of the base plate 6, spring 9 is wound on the surface of the damper 10, and a connecting plate 7 is fixedly connected to the bottom of the damper 10. Mounting blocks 12 are fixedly connected to both sides of the bottom of the connection box 3, and the mounting blocks 12 and the support plate 5 are fixedly connected by mounting bolts 11. Bearings 17 are fixedly connected to both sides of the inner cavity of the connection box 3, and one side of the threaded rod 15 is fixedly connected to the inner ring of the bearing 17. Slide grooves 18 are provided on both sides of the bottom of the inner cavity of the connection box 3, and a slider 19 is fixedly connected to the bottom of the threaded sleeve 16, and the bottom of the slider 19 is slidably connected to the inner cavity of the slide groove 18. A box door is movably connected to the back of the connection box 3, and a handle is fixedly connected to the lower end of the box door surface.
[0032] Specifically: when the drone lands during flight, if the bottom is hit by an external factor, the impactor contacts the bottom of the connecting plate 7, and the impact force generated by the collision drives the connecting plate 7 to move upward, and the spring 9 and the damper 10 are squeezed through the connecting plate 7. The impact force is effectively released through the characteristics of the spring 9, and the fixed cover will not be damaged when hit, thereby increasing its service life.
[0033] The working principle of the utility model is as follows: when it is necessary to fix the battery compartment of the drone, the user holds the rotating disk 2 and rotates the rotating disk 2 in a clockwise direction, drives the rotating rod 1 to rotate through the rotating disk 2, drives the first gear 13 to rotate through the rotating rod 1, drives the second gear 14 to rotate through the first gear 13, and drives the threaded rod 15 to rotate through the second gear 14. Since the threads of the threaded rod 15 are opposite, the threaded sleeve 16 is driven to move to the opposite side through the threaded rod 15, drives the support rod 4 to move to one side through the threaded sleeve 16, and drives the fixed cover plate 8 to move to one side through the support rod 4, so that one side of the fixed cover plate 8 is tightly fitted with the two sides of the bottom of the battery compartment, and the fixation is completed. Battery compartments and batteries of different sizes can be fixed without usage restrictions, the fixing effect is better, and the practicality is strong. When the drone lands during flight, when the bottom is hit by external factors, the impactor contacts the bottom of the connecting plate 7, and the impact force generated by the collision drives the connecting plate 7 to move upward, and the connecting plate 7 is connected. The connecting plate 7 squeezes the spring 9 and the damper 10. Through the characteristics of the spring 9, the impact force is effectively released. When the collision occurs, the fixed cover will not be damaged, thereby improving the service life. The user rotates the mounting bolt 11 with the help of an external tool, and transfers the mounting bolt 11 into the inner cavity of the mounting block 12 and the support plate 5 to complete the installation of the connection box 3. The operation steps are simple and no complicated operation steps are required. The function of quick installation is achieved. Through the setting of the bearing 17, the wear of the threaded rod 15 during the rotation is reduced, and the loss during the rotation of the threaded rod 15 is reduced, thereby greatly improving the service life of the threaded rod 15. During the movement of the threaded sleeve 16, the slider 19 is driven by the threaded sleeve 16 to slide in the inner cavity of the slide groove 18, thereby reducing the shaking of the threaded sleeve 16 during the movement, thereby greatly improving the service life of the threaded sleeve 16. The user holds the handle and pulls the handle outward to open the box door. The user wipes the inner cavity of the connection box 3 with the help of an external tool to improve the cleanliness of the inner cavity of the connection box 3.
[0034] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit the protection scope of the utility model. Although the utility model has been described in detail with reference to the preferred embodiments, ordinary technicians in this field should understand that the technical solution of the utility model can be modified or replaced by equivalents without departing from the essence and scope of the technical solution of the utility model.
Claims
1. A fixed cover for a battery compartment of an unmanned aerial vehicle, comprising a bottom plate (6), characterized in that: The rear end of the bottom plate (6) is fixedly connected to a support plate (5), the top of the support plate (5) is fixedly connected to a connection box (3), the center of the top of the connection box (3) is movably connected to a rotating rod (1), the top of the rotating rod (1) is fixedly connected to a rotating disk (2), the surface of the rotating disk (2) and located in the inner cavity of the connection box (3) is fixedly connected to a first gear (13), both sides of the first gear (13) are meshed with second gears (14), one side of the second gear (14) is fixedly connected to a threaded rod (15), the surface of the threaded rod (15) is threadedly connected to a threaded sleeve (16), the surface of the threaded sleeve (16) is fixedly connected to a support rod (4), and one side of the support rod (4) is fixedly connected to a fixed cover plate (8).
2. A fixed cover for a battery compartment of an unmanned aerial vehicle according to claim 1, characterized in that: The bottom of the base plate (6) is fixedly connected to a damper (10) on all four sides, a spring (9) is wound around the surface of the damper (10), and the bottom of the damper (10) is fixedly connected to a connecting plate (7).
3. The fixed cover for the battery compartment of an unmanned aerial vehicle according to claim 1, characterized in that: Both sides of the bottom of the connection box (3) are fixedly connected with mounting blocks (12), and the mounting blocks (12) and the support plate (5) are fixedly connected via mounting bolts (11).
4. The fixed cover for the battery compartment of an unmanned aerial vehicle according to claim 1, characterized in that: Bearings (17) are fixedly connected to both sides of the inner cavity of the connection box (3), and one side of the threaded rod (15) is fixedly connected to the inner ring of the bearing (17).
5. The fixed cover for the battery compartment of an unmanned aerial vehicle according to claim 1, characterized in that: Slide grooves (18) are provided on both sides of the bottom of the inner cavity of the connection box (3); a slider (19) is fixedly connected to the bottom of the threaded sleeve (16), and the bottom of the slider (19) is slidably connected to the inner cavity of the slide groove (18).
6. The fixed cover for the battery compartment of an unmanned aerial vehicle according to claim 1, characterized in that: The back side of the connection box (3) is movably connected to a box door, and the lower end of the surface of the box door is fixedly connected to a handle.