Automatic unhooking device for unmanned aerial vehicle

Through the decoupling components and installation components of the automatic decoupling device of the drone, the complex problem of drone hook operation is solved, and the single-person fast hooking and decoupling is achieved, which improves transportation efficiency and connection convenience.

CN223086281UActive Publication Date: 2025-07-11GUANGXI JIUCHONGTIAN ZHIHANG TECHNOLOGY SERVICE CO LTD
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Patent Information

Application Number
CN202422269346.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-18
Publication Date
2025-07-11
Estimated Expiration
2034-09-18

AI Technical Summary

Technical Problem

The existing drone hooks require two operators to cooperate when hooking and decoupling operations, and the connection between the rope and the hook is cumbersome, time-consuming and labor-intensive, which increases labor costs and operational complexity.

Method used

An automatic unhooking device for drone is designed to control the opening and closing of the buckle by decoupling components to realize single operation, and the connection process between the rope and the hook is simplified by installing the components, including the combination of components such as biting teeth, transmission teeth, rack plates, guide rods, extrusion blocks, friction blocks and top bolts.

Benefits of technology

It realizes quick hooking and decoupling for single persons, reduces labor costs, improves transportation efficiency, and simplifies the connection steps between the rope and the hook, reducing operation difficulty and time consumption.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides an automatic unhooking device of an unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicle equipment and comprises a shell, a lifting hook is fixedly connected in the shell, a connecting block is fixedly connected on the lifting hook, a hasp is rotatably connected in the connecting block, a movable groove for the hasp to move is formed in the lifting hook, and the lower end of the hasp extends into the movable groove. And a lifting rope is arranged above the shell. According to the device, opening and closing of the hasp can be controlled through the unhooking assembly, so that hooking and unhooking operation can be carried out by a single person, the labor use cost is reduced, the operation is more convenient and faster, the transportation efficiency is improved, secondly, the lifting rope and the lifting hook can be connected through the mounting assembly, the connecting process is simple and convenient, the connecting steps are reduced, and more time and labor are saved.
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Description

Technical Field

[0001] The utility model relates to the technical field of UAV equipment, in particular to an automatic hook - off device for UAVs. Background Technique

[0002] The unmanned aerial vehicle is abbreviated as "UAV", and its English abbreviation is "UAV". It is an unmanned aircraft controlled by radio remote control equipment and self - contained program control devices, or is completely or intermittently autonomously operated by an on - vehicle computer. In the prior art, in the wide application of UAVs, there has already been a technology of using UAVs as transportation devices to deliver goods to designated locations. With the wide application of UAVs in the field of material transportation, higher requirements are put forward for the material delivery function of UAVs. Currently, existing UAVs use hooks during material transportation and delivery. However, when the existing hooks are hooked, at least two operators are required to cooperate with each other, one for control operation and one for hooking operation to complete the hooking, which increases the labor cost. At the same time, when the UAV hoists materials, the suspension rope on the UAV needs to be connected to the hook for use first. However, the existing connection method between the suspension rope and the hook is to use a knot or a fastener, which is not only more troublesome but also time - consuming and laborious. Content of the Utility Model

[0003] The purpose of the utility model is to solve the shortcomings existing in the background technique, and provide an automatic hook - off device for UAVs. Through the hook - off component, the opening and closing of the buckle can be controlled, so that a single person can perform the hooking and unhooking operations, reducing the labor cost, being more convenient and fast, and improving the transportation efficiency. Secondly, through the installation component, the suspension rope can be connected to the hook, and the connection process is simple and convenient, reducing the connection steps, and being more time - saving and labor - saving.

[0004] To achieve the above - mentioned purpose, the utility model provides the following technical solution. An automatic hook - off device for UAVs includes: a housing, a hook fixedly connected inside the housing, a connecting block fixedly connected to the hook, a buckle rotatably connected inside the connecting block, an activity groove for the buckle to move is opened on the hook, the lower end of the buckle extends into the activity groove, a suspension rope is arranged above the housing, a hook - off component arranged on the hook for controlling the opening and closing of the buckle, the hook - off component includes: a biting tooth, a transmission tooth and a rack plate, and an installation component arranged on the housing for connecting the suspension rope, the installation component includes: a guide rod, a pressing block, a friction block, a threaded hole and a top - piece bolt.

[0005] Furthermore, the higher end of the buckle is arranged in an arc-shaped structure, and a plurality of equally spaced engaging teeth are fixedly connected to the outside of the buckle arc-shaped structure, a rotating cavity communicated with the outside is opened inside the hook, a transmission tooth is rotatably connected inside the rotating cavity, and the transmission tooth is engaged with the engaging teeth, a movable groove communicated with the rotating cavity is opened inside the hook, a rack plate is arranged inside the movable groove, and the rack plate is engaged with the transmission teeth.

[0006] Furthermore, a mounting groove is provided on the top of the shell, a guide rod is fixedly connected between the inner walls on both sides of the mounting groove, an extrusion block is slidably connected to the outside of the guide rod, and two symmetrically arranged friction blocks are fixedly connected to one side of the extrusion block. A threaded hole communicating with the interior of the mounting groove is provided on one side of the shell, and a top bolt is threadedly connected to the threaded hole, and one end of the suspension rope bypasses the guide rod and extends from the inside of the mounting groove to the outside.

[0007] Furthermore, a threaded rod is provided inside the movable groove, and both ends of the threaded rod are rotatably connected to the inner walls of the shell on both sides respectively. The outer thread of the threaded rod is threadedly connected to a threaded block, and the bottom of the threaded block is connected to the rack plate.

[0008] Furthermore, a motor is fixedly mounted on one side of the shell, a driving shaft of the motor is transmission-connected to one end of the threaded rod, and travel switches are fixedly mounted on opposite sides of the inner wall of the shell, and the two travel switches are on the same horizontal plane as the threaded block.

[0009] Furthermore, the extrusion block is fixedly connected to guide blocks on opposite sides, and guide grooves used in conjunction with the guide blocks are respectively opened on inner walls on opposite sides of the installation groove, and the two guide blocks are respectively located inside the two guide grooves.

[0010] Furthermore, a spring is sleeved on the outside of the top bolt, one end of the spring fits with the nut of the top bolt, and the other end of the spring fits with the shell.

[0011] The utility model provides an automatic unhooking device for a drone, which has the following beneficial effects:

[0012] The advantage of the utility model is that the opening and closing of the buckle can be controlled by the unhooking component, so that a single person can perform the hooking and unhooking operations, reducing the manpower cost, being more convenient and quick, and improving the transportation efficiency. Secondly, the sling rope and the hook can be connected by installing the component, the connection process is simple and convenient, the connection steps are reduced, and it is more time-saving and labor-saving. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the overall structure of the utility model.

[0014] Figure 2 It is a sectional view of the overall structure of the utility model.

[0015] Figure 3 It is a schematic diagram of the hook structure of the utility model.

[0016] Figure 4 It is a schematic diagram of the transmission gear structure of the utility model.

[0017] Figure 5 This is a schematic diagram of the top bolt structure of the utility model.

[0018] Figure 6 For the utility model Figure 2 Enlarged view of point A in the middle.

[0019] Figure 7 For the utility model Figure 2 Enlarged view of point B in the middle.

[0020] Figures 1-7 In: 1. Shell; 11. Hook; 12. Connecting block; 13. Buckle; 14. Movable groove; 15. Lifting rope; 2. Engaging teeth; 21. Transmission teeth; 22. Rack plate; 23. Threaded rod; 24. Threaded block; 25. Motor; 26. Travel switch; 3. Guide rod; 31. Extrusion block; 32. Friction block; 33. Threaded hole; 34. Top bolt; 35. Guide block; 36. Guide groove; 37. Spring. DETAILED DESCRIPTION

[0021] The technical solutions in the embodiments of the present application will be described clearly and completely below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative work are within the scope of protection of the present application.

[0022] An embodiment of the present application provides an automatic unhooking device for a drone, which can control the opening and closing of the buckle through a unhooking component, so that a single person can perform the hooking and unhooking operations, thereby reducing manpower costs, being more convenient and quick, and improving transportation efficiency.

[0023] The automatic unhooking device for the drone is described in detail below. It should be noted that the description order of the following embodiments is not intended to limit the preferred order of the embodiments.

[0024] The present application is described in detail below with reference to the accompanying drawings and specific implementation methods.

[0025] Example 1

[0026] See alsoFigures 1-7 Among them, an automatic unhooking device for an unmanned aerial vehicle provided in this embodiment includes: a housing 1, a hook 11 fixedly connected inside the housing 1, a connecting block 12 fixedly connected to the hook 11, a buckle 13 rotatably connected inside the connecting block 12, a moving groove 14 for the buckle 13 to move is formed on the hook 11, the lower end of the buckle 13 extends into the moving groove 14, a suspension rope 15 is provided above the housing 1, and an unhooking assembly is arranged on the hook 11 and used to control the opening and closing of the buckle 13. The unhooking assembly includes: a biting tooth 2, a transmission tooth 21 and a rack plate 22, and an installation assembly is arranged on the housing 1 and used to connect the suspension rope 15. The installation assembly includes: a guide rod 3, a pressing block 31, a friction block 32, a threaded hole 33 and a top bolt 34.

[0027] During use, the suspension rope 15 is connected to the housing 1 through the installation assembly, the buckle 13 is controlled to open through the unhooking assembly, the steel cable for lifting the goods is hung on the hook 11, and then the buckle 13 is controlled to close to prevent the steel cable from falling off. After the goods are transported to the destination, the goods first land and the buckle 13 is controlled to open. Subsequently, the hook 11 moves downward and moves to the side opposite to the buckle 13, so that the steel cable is disengaged from the hook 11, thereby completing the unhooking operation. When lifting the goods, the hook 11 is controlled to move to the steel cable of the goods, so that the steel cable is clamped on the hook 11, and then the buckle 13 is controlled to close, thereby completing the hooking of the goods.

[0028] Embodiment 2

[0029] On the basis of Embodiment 1, the higher end of the buckle 13 is arranged in an arc-shaped structure, and a number of equally spaced biting teeth 2 are fixedly connected to the outside of the arc-shaped structure of the buckle 13. A rotating cavity communicating with the outside is formed inside the hook 11, a transmission tooth 21 is rotatably connected inside the rotating cavity, the transmission tooth 21 is in biting connection with the biting tooth 2, a moving groove communicating with the rotating cavity is formed inside the hook 11, a rack plate 22 is arranged inside the moving groove, the rack plate 22 is in biting connection with the transmission tooth 21, a threaded rod 23 is arranged inside the moving groove, both ends of the threaded rod 23 are rotatably connected between the opposite inner walls of the housing 1, a threaded block 24 is threadedly connected to the outside of the threaded rod 23, the bottom of the threaded block 24 is connected to the rack plate 22, a motor 25 is fixedly installed on one side of the housing 1, the driving shaft of the motor 25 is in transmission connection with one end of the threaded rod 23, and two stroke switches 26 are respectively fixedly installed on the opposite inner walls of the housing 1, and the two stroke switches 26 are on the same horizontal plane as the threaded block 24.

[0030] When controlling the opening and closing of the buckle 13, the motor 25 is started through the remote control device of the drone. The motor 25 is a forward and reverse motor and its rotation mode can be switched through the remote control device. When the motor 25 rotates, it drives the threaded rod 23 to rotate. The threaded rod 23 rotates and is screwed with the threaded block 24. Since the threaded block 24 is restricted by the moving groove, the threaded block 24 can only move in the horizontal direction. Therefore, when the threads are screwed together, the threaded block 24 will be driven to move. The threaded block 24 drives the rack plate 22 to move. The rack plate 22 moves and meshes with the transmission gear 21, thereby driving the transmission gear 21 to rotate. The transmission gear 21 rotates and meshes with the engaging teeth 2 outside the buckle 13, thereby driving the buckle 13 to rotate. When the buckle 13 rotates, one end of it moves inside the movable groove 14. By controlling the rotation direction of the motor 25, the opening and closing of the buckle 13 can be controlled. When the threaded block 24 touches the travel switch 26 on the moving side during movement, the motor 25 stops working, thereby restricting the maximum moving distance of the threaded block 24.

[0031] Embodiment 3

[0032] On the basis of Embodiment 1, an installation groove is opened at the top of the housing 1. A guide rod 3 is fixedly connected between the inner walls on the opposite sides of the installation groove. A pressing block 31 is slidably connected to the outside of the guide rod 3. One side of the pressing block 31 is fixedly connected with two symmetrically arranged friction blocks 32. A threaded hole 33 communicating with the inside of the installation groove is opened on one side of the housing 1. A top bolt 34 is threadedly connected to the inside of the threaded hole 33. One end of the lifting rope 15 bypasses the guide rod 3 and extends from the inside of the installation groove to the outside. Guide blocks 35 are respectively fixedly connected to the opposite sides of the pressing block 31. Guide grooves 36 matching the guide blocks 35 are respectively opened on the inner walls on the opposite sides of the installation groove. The two guide blocks 35 are respectively located inside the two guide grooves 36. A spring 37 is sleeved outside the top bolt 34. One end of the spring 37 is in contact with the nut of the top bolt 34, and the other end of the spring 37 is in contact with the housing 1.

[0033] When connecting the lifting rope 15, the bottom end of the lifting rope 15 is bypassed around the guide rod 3 and extends out from the installation groove. Then, the top bolt 34 is rotated by a wrench to screw the top bolt 34 into the threaded hole 33. One end of the top bolt 34 extends into the installation groove and pushes the pressing block 31 to move. The pressing block 31 is restricted by the two guide blocks 35 and the guide grooves 36 on both sides, so as to support the pressing block 31 and make it move only on the horizontal line of the guide groove 36. The pressing block 31 clamps the lifting rope 15, and the pressing block 31 can improve the friction force. When the top bolt 34 is screwed in, it will compress the spring 37, causing the spring 37 to contract and store energy. Under the elastic force of the spring 37, the loosening of the top bolt 34 can be avoided, thereby fixing the lifting rope 15 and completing the connection.

[0034] In the above embodiments, the descriptions of each embodiment have their own emphases. For the parts not detailed in a certain embodiment, reference can be made to the relevant descriptions of other embodiments.

[0035] The above has introduced in detail an automatic unhooking device for an unmanned aerial vehicle provided by the embodiments of the present application. Specific examples are used herein to elaborate on the principle and implementation manner of the present application. The description of the above embodiments is only used to help understand the technical solution and its core idea of the present application; those of ordinary skill in the art should understand that they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements on some of the technical features; and these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of the present application.

Claims

1. An automatic unhooking device for an unmanned aerial vehicle, characterized in that, Including: A housing (1) with a hook (11) fixedly connected inside. A connecting block (12) is fixedly connected to the hook (11). A buckle (13) is rotatably connected inside the connecting block (12). An activity groove (14) for the buckle (13) to move is formed on the hook (11). The lower end of the buckle (13) extends into the activity groove (14). A lifting rope (15) is provided above the housing (1). A hook - releasing assembly which is arranged on the hook (11) and used to control the opening and closing of the buckle (13). The hook - releasing assembly includes: engaging teeth (2), a driving gear (21) and a rack plate (22). An installation assembly which is arranged on the housing (1) and used to connect the lifting rope (15). The installation assembly includes: a guide rod (3), a pressing block (31), a friction block (32), a threaded hole (33) and a top - piece bolt (34).

2. The automatic unhooking device for the unmanned aerial vehicle according to claim 1, wherein, The higher end of the buckle (13) is arranged in an arc - shaped structure, and a number of equally - spaced engaging teeth (2) are fixedly connected to the outside of the arc - shaped structure of the buckle (13). A rotation cavity communicating with the outside is formed inside the hook (11). A driving gear (21) is rotatably connected inside the rotation cavity. The driving gear (21) is engaged with the engaging teeth (2). A moving groove communicating with the rotation cavity is formed inside the hook (11). A rack plate (22) is arranged inside the moving groove. The rack plate (22) is engaged with the driving gear (21).

3. The automatic unhooking device for the drone according to claim 1, wherein, An installation groove is formed at the top of the housing (1). A guide rod (3) is fixedly connected between the opposite inner walls of the installation groove. A pressing block (31) is slidably connected to the outside of the guide rod (3). Two symmetrically - arranged friction blocks (32) are fixedly connected to one side of the pressing block (31). A threaded hole (33) communicating with the inside of the installation groove is formed on one side of the housing (1). A top - piece bolt (34) is threadedly connected inside the threaded hole (33). One end of the lifting rope (15) bypasses the guide rod (3) and extends from the inside of the installation groove to the outside.

4. The drone automatic decoupling device according to claim 2, wherein, A threaded rod (23) is arranged inside the moving groove. The two ends of the threaded rod (23) are respectively rotatably connected between the opposite inner walls of the housing (1). A threaded block (24) is threadedly connected to the outside of the threaded rod (23). The bottom of the threaded block (24) is connected to the rack plate (22).

5. The drone automatic decoupling device according to claim 4, wherein, A motor (25) is fixedly installed on one side of the housing (1). The driving shaft of the motor (25) is in transmission connection with one end of the threaded rod (23). Two travel switches (26) are respectively fixedly installed on the opposite inner walls of the housing (1) inner wall. The two travel switches (26) and the threaded block (24) are on the same horizontal plane.

6. The automatic unhooking device for unmanned aerial vehicle according to claim 3, wherein Guide blocks (35) are respectively fixedly connected to the opposite sides of the pressing block (31). Guide grooves (36) matching with the guide blocks (35) are respectively formed on the opposite inner walls of the installation groove. The two guide blocks (35) are respectively located inside the two guide grooves (36).

7. The drone automatic decoupling device according to claim 3, characterized in that, A spring (37) is sleeved outside the top bolt (34). One end of the spring (37) is in contact with the nut of the top bolt (34), and the other end of the spring (37) is in contact with the housing (1).