Unmanned aerial vehicle mounting device
By designing a drone mounting device including pulling plate, extension plate, support mechanism and clamping mechanism, the problem of cumbersome fixing process of the drone mounting device in the prior art is solved, and fast and stable connections are achieved. Disassembly improves efficiency and safety.
Patent Information
- Application Number
- CN202421309252.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-07
- Publication Date
- 2025-01-17
- Estimated Expiration
- 2034-06-07
AI Technical Summary
The existing drone mounting devices lack a fast fixing mechanism, which leads to cumbersome assembly and disassembly processes, affecting the rapid deployment of drones and the efficiency of equipment use, and is prone to wear and damage when frequently replacing mounted devices.
A drone mounting device including a connecting mechanism is designed, which consists of a pulling plate, an extension plate, a support mechanism, a fixing sleeve, a spring, an external sleeve, a thread sleeve, a thread section, a pressing plate and a clamping mechanism, through The spring elastic connection, the fastening of thread sleeves and thread segments, and the locking mechanism of telescopic rods and rubber rings achieves rapid and stable connection and disassembly, and provides a stable load-bearing platform through the support mechanism to evenly disperse weight.
Achieve fast and stable connection between the drone and the mounting device, ensures vibration absorption and stability in flight, simplifies the operation process, improves the efficiency of use and maintenance convenience, and enhances the reliability and safety of operation. sex.
Smart Images

Figure CN222361085U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicle mounting devices, and more specifically, to a unmanned aerial vehicle mounting device. Background Art
[0002] Under current technical conditions, the design of drone mounting devices has certain limitations. Specifically, these devices are often not easy to fix during use. This is mainly because the existing mounting devices lack an effective quick fixing mechanism, which requires users to spend more time and energy during assembly and disassembly. This not only reduces the efficiency of the drone mounting device, but also may affect the rapid deployment of the drone in an emergency.
[0003] To further illustrate this problem, it can be described as follows: In actual situations, when a drone needs to carry out a mission, the existing mounting devices often need to be completed through complex screws, clips or other cumbersome fixing methods. This design not only makes the operation process cumbersome, but also easily causes wear and damage to the device when the mounting equipment is frequently replaced. Utility Model Content
[0004] 1. Technical issues to be resolved
[0005] In view of the problems existing in the prior art, the utility model provides a drone mounting device to solve the technical problems mentioned in the background technology.
[0006] (II) Technical solution
[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV mounting device, including a UAV body, a connecting mechanism is arranged on the UAV body, the connecting mechanism includes a pulling plate, an extending plate, a supporting mechanism, a fixing sleeve, a spring, an external sleeve, a threaded sleeve, a threaded segment, a pressing plate and a clamping mechanism, the extending plate is installed on the UAV body, the supporting mechanism is installed on the UAV body, a plurality of springs are provided, and the two ends of the plurality of springs are respectively connected to the fixing sleeve and the external sleeve, the fixing sleeve and the external sleeve are respectively slidably connected to the extending plate and the pulling plate, the threaded sleeve is installed on the external sleeve, the threaded segment is threadedly connected to the threaded sleeve, the pressing plate is installed on the threaded segment, and the clamping mechanism is installed on the fixing sleeve.
[0008] The utility model is further configured that a plurality of compression springs are arranged on the pressure plate, and the plurality of compression springs respectively abut against the pull plate, and the design of the compression springs ensures the fixation of the pull plate.
[0009] The utility model is further configured such that the clamping mechanism includes a telescopic rod and a rubber ring, a plurality of lateral holes are opened on the fixing sleeve, the telescopic rod is slidably connected in each lateral hole, a rubber ring is installed on the telescopic rod, and the rubber ring is slidably connected in the lateral hole, and the design of the clamping mechanism ensures the convenience of clamping.
[0010] The utility model is further configured such that each of the two ends of the telescopic rod is provided with a pin respectively, an intermediate rod is coaxially provided on the threaded section, the pin inside the telescopic rod abuts against the side wall of the intermediate rod, and the design of the pin ensures the stability of the abutment.
[0011] The utility model is further configured that a fitting sleeve is slidably provided on the fixing sleeve, the fitting sleeve abuts against the fitting sleeve, and the design of the fitting sleeve ensures the fixation of the pull plate.
[0012] The utility model is further configured that a plurality of annular grooves are equidistantly provided on the inner wall of the fitting sleeve, and the outer head of the telescopic rod abuts against the annular grooves. The design of the annular grooves ensures the fixation of the fitting sleeve.
[0013] The utility model is further configured that the support mechanism includes a connecting rod and a support rod, and two ends of the connecting rod are respectively connected to the drone body and the support rod. The design of the support mechanism ensures the convenience of support.
[0014] The utility model is further configured that a box body is provided on the pull plate.
[0015] (III) Beneficial effects
[0016] Compared with the prior art, the utility model provides a UAV mounting device, which has the following beneficial effects:
[0017] 1. The design of the connection mechanism realizes a fast and stable connection between the UAV body and the mounting device. Through the configuration of the spring, an elastic connection is provided between the fixed sleeve and the external sleeve, which effectively absorbs the vibration of the UAV during flight and ensures the reliability of the connection. The sliding connection between the pull plate and the extension plate, combined with the tightening effect of the threaded sleeve and the threaded section, keeps the device stable during movement. In addition, the application of the compression spring ensures a close fit between the pull plate and the UAV body, further enhancing the stability of the connection.
[0018] 2. The clamping mechanism provides a safe and easy-to-operate locking mechanism through the cooperation of the rubber ring and the top head on the telescopic rod with the middle rod and the annular groove. This design enables the device to be firmly positioned during the connection process, preventing accidental falling off due to vibration or external force. At the same time, the lateral sliding of the telescopic rod and the locking of the top head and the annular groove make the disassembly process also simple and quick, improving the use efficiency and convenience of maintenance.
[0019] 3. The support mechanism provides a solid load-bearing platform for the drone mounting device through the setting of connecting rods and support rods. When mounting heavy objects, the support frame can stably resist the ground to ensure the balance and stability of the drone body. The box is installed on the pull plate, which not only increases the flexibility of mounting, but also can evenly disperse the weight, reducing the risk of damage to the drone due to weight concentration during the mounting process. The design of the support mechanism enables the drone to perform mounting tasks more stably and improves the reliability and safety of the overall operation. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 This is a schematic diagram of the overall structure of a UAV mounting device in the utility model;
[0021] Figure 2 It is a structural schematic diagram of the connecting mechanism in the utility model;
[0022] Figure 3 For the utility model Figure 2 Schematic diagram of the explosion structure;
[0023] Figure 4 It is a structural schematic diagram of the telescopic rod in the utility model;
[0024] Figure 5 It is a structural schematic diagram of the fixing sleeve in the utility model.
[0025] In the figure: 1. UAV body; 2. Pull plate; 3. Extension plate; 4. Fixed sleeve; 5. Spring; 6. External sleeve; 7. Threaded sleeve; 8. Threaded section; 9. Pressure plate; 10. Compression spring; 11. Telescopic rod; 12. Rubber ring; 13. Lateral hole; 14. Top head; 15. Middle rod; 16. Fitting sleeve; 17. Annular groove; 18. Connecting rod; 19. Support rod; 20. Box body. DETAILED DESCRIPTION
[0026] It should be noted that, in the absence of conflict, the embodiments and features in the embodiments of the present application can be combined with each other. The present utility model will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.
[0027] It should be noted that, unless otherwise specified, all technical and scientific terms used in this application have the same meanings as commonly understood by ordinary technicians in the technical field to which this application belongs.
[0028] In the present invention, unless otherwise specified, directions such as "up" and "down" are usually used in reference to the directions shown in the drawings, or in reference to the vertical, perpendicular or gravity direction; similarly, for ease of understanding and description, "left" and "right" are usually used in reference to the left and right shown in the drawings; "inside" and "outside" refer to the inside and outside relative to the outline of each component itself, but the above-mentioned directions are not used to limit the present invention.
[0029] See also Figure 1-5 A UAV mounting device comprises a UAV body 1, on which a connecting mechanism is arranged, the connecting mechanism comprises a pulling plate 2, an extending plate 3, a supporting mechanism, a fixing sleeve 4, a spring 5, an external sleeve 6, a threaded sleeve 7, a threaded segment 8, a pressing plate 9 and a clamping mechanism, the extending plate 3 is mounted on the UAV body 1, the supporting mechanism is mounted on the UAV body 1, a plurality of springs 5 are arranged, and the two ends of the plurality of springs 5 are respectively connected to the fixing sleeve 4 and the external sleeve 6, the fixing sleeve 4 and the external sleeve 6 are respectively slidably connected to the extending plate 3 and the pulling plate 2, the threaded sleeve 7 is mounted on the external sleeve 6, the threaded segment 8 is threadedly connected to the threaded sleeve 7, the pressing plate 9 is mounted on the threaded segment 8, the clamping mechanism is mounted on the fixing sleeve 4, a plurality of compression springs 10 are arranged on the pressing plate 9, the plurality of compression springs 10 respectively abut against the pulling plate 2, the clamping mechanism comprises an extending sleeve 4, a plurality of compression springs 10 are respectively abutted against the pulling plate 2, and the clamping mechanism comprises an extending sleeve 4, a plurality of compression springs 10 are arranged on the pressing plate 9, the plurality of compression springs 10 respectively abut against the pulling plate 2, and the clamping mechanism comprises an extending sleeve 4, a plurality of compression springs 10 are respectively abutted ... A retractable rod 11 and a rubber ring 12, a plurality of lateral holes 13 are provided on the fixed sleeve 4, each lateral hole 13 is slidably connected to the telescopic rod 11, a rubber ring 12 is installed on the telescopic rod 11, the rubber ring 12 is slidably connected in the lateral hole 13, a top head 14 is respectively provided at both ends of each telescopic rod 11, an intermediate rod 15 is coaxially provided on the threaded section 8, the top head 14 inside the telescopic rod 11 abuts against the side wall of the intermediate rod 15, a fitting sleeve 16 is slidably provided on the fixed sleeve 4, the fitting sleeve 16 abuts against the fitting sleeve 16, a plurality of annular grooves 17 are equidistantly provided on the inner wall of the fitting sleeve 16, the external top head 14 of the telescopic rod 11 abuts in the annular groove 17, the supporting mechanism includes a connecting rod 18 and a supporting rod 19, the two ends of the connecting rod 18 are respectively connected to the drone body 1 and the supporting rod 19, and a box 20 is provided on the pull plate 2.
[0030] In this embodiment, when connection is required, since the rubber ring 12 is installed on the telescopic rod 11, the telescopic rod 11 has corresponding resistance when sliding in the lateral hole 13, and then the fixing sleeve 4 and the external sleeve 6 are respectively inserted into the pull plate 2 and the extension plate 3, and the fitting sleeve 16 is installed in the fixing sleeve 4, and then the intermediate rod 15 is inserted into the external sleeve 6 and the fixing sleeve 4, so that the top head 14 inside the telescopic rod 11 is in contact with the side wall of the intermediate rod 15, and then the top head 14 outside the telescopic rod 11 can be in contact with the annular groove 17, and then the fixing sleeve 4 and the fitting sleeve 16 can be fixed, and through the threaded section 8 and the threaded sleeve 7, and then the intermediate rod 15 is fixed, and then the compression spring 10 is pressed against the side wall of the pull plate 2, thereby completing the connection between the two.
[0031] More specifically, when the drone body 1 needs to be mounted, the support frame is first pressed against the ground, the box 20 is installed on the pull plate 2, and then the pull plate 2 is connected to the extension plate 3, thereby completing the mounting process and then completing the fixing process.
[0032] In summary, when the overall equipment is in use or running: when connection is required, since the rubber ring 12 is installed on the telescopic rod 11, the telescopic rod 11 has corresponding resistance when sliding in the lateral hole 13, and then the fixing sleeve 4 and the external sleeve 6 are respectively inserted into the pull plate 2 and the extension plate 3, and the fitting sleeve 16 is installed in the fixing sleeve 4, and then the intermediate rod 15 is inserted into the external sleeve 6 and the fixing sleeve 4, so that the top head 14 inside the telescopic rod 11 is in contact with the side wall of the intermediate rod 15, and then the top head 14 outside the telescopic rod 11 can be in contact with the annular groove 17, and then the fixing sleeve 4 and the fitting sleeve 16 can be fixed, and through the threaded section 8 and the threaded sleeve 7, and then the intermediate rod 15 is fixed, and then the compression spring 10 is pressed against the side wall of the pull plate 2, thereby completing the connection between the two.
[0033] When the drone body 1 needs to be mounted, the support frame is first pressed against the ground, the box body 20 is installed on the pull plate 2, and then the pull plate 2 is connected to the extension plate 3, thereby completing the mounting process and then completing the fixing process.
[0034] In all the schemes mentioned above, the connection between two parts can be selected according to actual conditions by welding, bolt and nut matching connection, bolt or screw connection or other well-known connection methods, which are not described here one by one. In the above, all fixed connections are preferably welded. Although the embodiments of the utility model have been shown and described, it can be understood by ordinary technicians in this field that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the utility model. The scope of the utility model is defined by the attached claims and their equivalents.
Claims
1. A drone mounting device, comprising a drone body (1), characterized in that: The drone body (1) is provided with a connection mechanism, which comprises a pull plate (2), an extension plate (3), a support mechanism, a fixing sleeve (4), a spring (5), an external sleeve (6), a threaded sleeve (7), a threaded section (8), a pressure plate (9) and a clamping mechanism. The extension plate (3) is mounted on the drone body (1), the support mechanism is mounted on the drone body (1), a plurality of springs (5) are provided, and the two ends of the plurality of springs (5) are respectively connected to the fixing sleeve (4) and the external sleeve (6), the fixing sleeve (4) and the external sleeve (6) are respectively slidably connected to the extension plate (3) and the pull plate (2), the threaded sleeve (7) is mounted on the external sleeve (6), the threaded section (8) is threadedly connected to the threaded sleeve (7), the pressure plate (9) is mounted on the threaded section (8), and the clamping mechanism is mounted on the fixing sleeve (4).
2. The UAV mounting device according to claim 1, characterized in that: The pressure plate (9) is provided with a plurality of compression springs (10), and the plurality of compression springs (10) respectively abut against the pull plate (2).
3. The UAV mounting device according to claim 2, characterized in that: The clamping mechanism comprises a telescopic rod (11) and a rubber ring (12); a plurality of lateral holes (13) are provided on the fixing sleeve (4); each of the lateral holes (13) is slidably connected to the telescopic rod (11); a rubber ring (12) is installed on the telescopic rod (11); and the rubber ring (12) is slidably connected to the lateral hole (13).
4. The UAV mounting device according to claim 3 is characterized in that: Each telescopic rod (11) is provided with a top head (14) at both ends, and an intermediate rod (15) is coaxially provided on the threaded section (8). The top head (14) inside the telescopic rod (11) abuts against the side wall of the intermediate rod (15).
5. The UAV mounting device according to claim 4 is characterized in that: A fitting sleeve (16) is slidably provided on the fixing sleeve (4), and the fitting sleeve (16) abuts against the fitting sleeve (16).
6. The UAV mounting device according to claim 5, characterized in that: A plurality of annular grooves (17) are equidistantly formed on the inner wall of the fitting sleeve (16), and the outer head (14) of the telescopic rod (11) abuts against the annular grooves (17).
7. The UAV mounting device according to claim 1, characterized in that: The support mechanism comprises a connecting rod (18) and a supporting rod (19), and two ends of the connecting rod (18) are respectively connected to the drone body (1) and the supporting rod (19).
8. The UAV mounting device according to claim 7, characterized in that: A box body (20) is provided on the pull plate (2).