Anti-swing stable structure for hoisting of multi-rotor unmanned aerial vehicle

Abstract

The anti-swing stabilizing structure comprises an unmanned aerial vehicle body and a hoisting mechanism, a stabilizing mechanism is arranged on the lower side of the hoisting mechanism, the stabilizing mechanism comprises a fixing frame, a telescopic mechanism and a stabilizing plate, the fixing frame is arranged on the lower side of the hoisting mechanism, and the telescopic mechanism is arranged on the lower side of the fixing frame. And multi-stage electric telescopic rods are arranged on the two sides of the telescopic mechanism, clamping plates are fixedly installed at the output ends of the multi-stage electric telescopic rods, the stabilizing plate is arranged at the output end of the hoisting mechanism, a clamping column is fixedly installed on the upper side of the stabilizing plate, and clamping grooves are formed in the peripheral side of the clamping column and one sides of the two clamping plates. According to the utility model, through the stabilizing mechanism, the lifting rope and the lifting hook can be limited when an article is lifted, so that the article cannot swing after being lifted by the lifting hook, and the article can be stably lifted, thereby avoiding the risk that the article swings in the air and falls off when being lifted.

Description

Technical Field

[0001] This utility model relates to the field of drone hoisting technology, and in particular to an anti-sway stabilizing structure for hoisting multi-rotor drones. Background Technology

[0002] A multi-rotor drone is a special type of unmanned helicopter with three or more rotor shafts. It generates lift and thrust by rotating rotors via electric motors on each shaft. Unlike conventional helicopters, the collective pitch of the rotors is fixed. By changing the relative speeds between the different rotors, the magnitude of the thrust per shaft can be altered, thereby controlling the aircraft's trajectory.

[0003] Multi-rotor drone hoisting refers to the technology of using a multi-rotor drone equipped with a hoisting system to safely and efficiently move heavy objects from one location to another through precise flight control and sling operation. This technology integrates high-precision positioning, cutting-edge sensors, a powerful power system, and intelligent control algorithms to ensure the stability and accuracy of hoisting operations.

[0004] Existing hoisting mechanisms have the following drawbacks in actual use:

[0005] Most existing hoisting mechanisms use ropes and hooks to lift objects. However, since the ropes are soft, the objects tend to swing in the air after being lifted, which can easily cause them to fall and create danger. Utility Model Content

[0006] In view of the technical problem that most existing hoisting mechanisms use ropes and hooks to lift objects, the ropes are soft and the objects are prone to swinging in the air after being lifted, which can easily lead to the objects falling and causing danger, this utility model provides an anti-sway stabilizing structure for hoisting multi-rotor drones.

[0007] The technical solution adopted in this utility model is: a sway-resistant stabilizing structure for hoisting multi-rotor UAVs, including a UAV body and a hoisting mechanism. A stabilizing mechanism is provided on the lower side of the hoisting mechanism. The stabilizing mechanism includes a fixed frame, a telescopic mechanism, and a stabilizing plate. The fixed frame is located on the lower side of the hoisting mechanism, and the telescopic mechanism is located on the lower side of the fixed frame. Multi-stage electric telescopic rods are provided on both sides of the telescopic mechanism. A snap-fit ​​plate is fixedly installed at the output end of the multi-stage electric telescopic rod. The stabilizing plate is located at the output end of the hoisting mechanism. A snap-fit ​​post is fixedly installed on the upper side of the stabilizing plate. Snap-fit ​​grooves are provided on the periphery of the snap-fit ​​post and on one side of each of the two snap-fit ​​plates. The snap-fit ​​plates and the snap-fit ​​posts are snapped together through the snap-fit ​​grooves.

[0008] Furthermore, the telescopic mechanism includes a fixed shell, a rotating shaft, a gear, and a toothed plate, wherein the number of toothed plates is two.

[0009] Furthermore, the fixed shell is fixedly installed on the lower side of the fixed frame, a sliding cavity is provided inside the fixed shell, the rotating shaft is rotatably installed in the sliding cavity, the gear is fixedly installed on the circumference of the rotating shaft, the toothed plate is slidably installed in the sliding cavity, and the toothed plate meshes with the gear.

[0010] Furthermore, a fixing sleeve is fixedly installed at one end of each of the two toothed plates, and the two fixing sleeves are respectively located at both ends of the fixing shell, with the multi-stage electric telescopic rod fixedly installed inside the fixing sleeve.

[0011] Furthermore, a turbine is fixedly installed on the circumference of the rotating shaft, a groove is provided on one side of the inner wall of the sliding cavity, a rotating motor is fixedly installed in the groove, and a worm is fixedly installed at the output end of the rotating motor, the worm meshing with the turbine.

[0012] Furthermore, the hoisting mechanism includes a mounting frame, a take-up roller, a hoisting rope, and a hook. The mounting frame is fixedly installed on the lower side of the UAV body, the take-up roller is rotatably installed between the mounting frames, the hoisting rope is wound around the circumference of the take-up roller, the stabilizing plate is fixedly installed on one end of the hoisting rope, the hook is fixedly installed on the lower side of the stabilizing plate, and a drive motor is fixedly installed on one side of the inner wall of the mounting frame. The output end of the drive motor is fixedly connected to one end of the take-up roller.

[0013] Furthermore, two support legs are fixedly installed on the lower side of the drone body, and the mounting frame is located between the two support legs.

[0014] The beneficial effects of this utility model are:

[0015] 1. This utility model, through a stabilizing mechanism, can limit the lifting rope and hook when hoisting items, so that the items will not swing after the hook lifts them, and the items can be hoisted stably, thereby avoiding the danger of the items swinging in the air and falling during hoisting.

[0016] 2. Secondly, this utility model, through a telescopic mechanism, can drive two multi-stage electric telescopic rods and two locking plates to move synchronously to limit the hook, and can ensure the stability of the hook after the locking plates limit the hook, thus providing stability and convenience when using the stabilizing mechanism. Attached Figure Description

[0017] Figure 1 This is a three-dimensional view of the main body of the drone of this utility model;

[0018] Figure 2 This is a perspective view of the hoisting mechanism and stabilizing mechanism of this utility model;

[0019] Figure 3 This is a perspective view of the stabilizing plate of this utility model;

[0020] Figure 4 This is a cross-sectional view of the telescopic mechanism of this utility model.

[0021] The components in the diagram are labeled as follows: 1. UAV body; 2. Support legs; 3. Lifting mechanism; 4. Mounting frame; 5. Rewind roller; 6. Lifting rope; 9. Drive motor; 10. Stabilizing mechanism; 11. Fixing frame; 12. Telescopic mechanism; 13. Multi-stage electric telescopic rod; 14. Clip plate; 15. Hook; 16. Stabilizing plate; 17. Clip post; 18. Clip groove; 19. Fixing shell; 20. Sliding cavity; 21. Rotating shaft; 22. Gear; 23. Gear plate; 24. Fixing sleeve; 25. Turbine; 26. Worm gear; 27. Rotating motor. Detailed Implementation

[0022] In the description of this utility model, it should be noted that the terms "front", "up", "down", "left", "right", "vertical", "horizontal", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0023] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0024] The following is in conjunction with the appendix Figures 1-4 The present invention will be further described below.

[0025] To address the problems existing in the background technology, this application proposes the following technical solution: an anti-sway stabilizing structure for hoisting multi-rotor UAVs.

[0026] The specific technical solution includes a drone body 1 and a hoisting mechanism 3. A stabilizing mechanism 10 is provided on the lower side of the hoisting mechanism 3. The stabilizing mechanism 10 includes a fixed frame 11, a telescopic mechanism 12, and a stabilizing plate 16. The fixed frame 11 is located on the lower side of the hoisting mechanism 3, and the telescopic mechanism 12 is located on the lower side of the fixed frame 11. Multi-stage electric telescopic rods 13 are provided on both sides of the telescopic mechanism 12. A snap-fit ​​plate 14 is fixedly installed at the output end of the multi-stage electric telescopic rod 13. The stabilizing plate 16 is located at the output end of the hoisting mechanism 3. A snap-fit ​​post 17 is fixedly installed on the upper side of the stabilizing plate 16. Snap-fit ​​grooves 18 are provided on the periphery of the snap-fit ​​post 17 and on one side of the two snap-fit ​​plates 14. The snap-fit ​​plates 14 and the snap-fit ​​posts 17 are snapped together through the snap-fit ​​grooves 18. The telescopic mechanism 12 includes a fixed shell 19, a rotating shaft 21, a gear 22, and a toothed plate 23. There are two toothed plates 23. The fixed shell 19 is fixedly installed on the lower side of the fixed frame 11. A stabilizing plate 19 is provided inside the fixed shell 19. The device has a sliding cavity 20, a rotating shaft 21 rotatably mounted inside the sliding cavity 20, a gear 22 fixedly mounted around the rotating shaft 21, a toothed plate 23 slidably mounted inside the sliding cavity 20 and meshing with the gear 22, and a fixed sleeve 24 fixedly mounted at one end of each of the two toothed plates 23. The two fixed sleeves 24 are located at both ends of the fixed housing 19. A multi-stage electric telescopic rod 13 is fixedly mounted inside the fixed sleeve 24. A turbine 25 is fixedly mounted around the rotating shaft 21. A groove is opened on one side of the inner wall of the sliding cavity 20, and a rotating motor 27 is fixedly mounted in the groove. A worm gear 26 is fixedly mounted at the output end of the rotating motor 27 and meshes with the turbine 25. Through the self-locking of the worm gear 26 and the turbine 25, the rotating shaft 21 can be locked, thereby preventing the gear from rotating and ensuring the stability of the snap-fit ​​plate 14 during use. There are through grooves in the middle of both the fixed housing 19 and the rotating shaft 21 to facilitate the passage of the lifting rope 6.

[0027] Reference Figure 2 and Figure 3 As shown, the hoisting mechanism 3 includes a mounting frame 4, a take-up roller 5, a hoisting rope 6, and a hook 15. The mounting frame 4 is fixedly installed on the lower side of the UAV body 1. The take-up roller 5 is rotatably installed between the mounting frames 4. The hoisting rope 6 is wound around the take-up roller 5. The stabilizing plate 16 is fixedly installed at one end of the hoisting rope 6. The hook 15 is located on the lower side of the stabilizing plate 16. A drive motor 9 is fixedly installed on one side of the inner wall of the mounting frame 4. The output end of the drive motor 9 is fixedly connected to one end of the take-up roller 5. Two support legs 2 are fixedly installed on the lower side of the UAV body 1. The mounting frame 4 is located between the two support legs 2. By starting the drive motor 9, the take-up roller 5 is driven to rotate. The rotation of the take-up roller 5 can wind and unwind the hoisting rope 6, thereby facilitating the adjustment of the length of the hoisting rope 6. The height of the multi-stage electric telescopic rod 13 after being retrieved is less than the height of the support legs 2, thereby avoiding any impact on the landing of the UAV body 1.

[0028] To ensure that those skilled in the art can fully understand the technical solution, this application provides the following overall overview:

[0029] In use, after the hook 15 lifts an item, the multi-stage electric telescopic rod 13 is activated, causing the locking plate 14 to move to correspond with the locking post 17. Then, the rotary motor 27 is activated, causing the worm gear 26 to rotate. The rotation of the worm gear 26 drives the worm wheel 25 to rotate, which in turn drives the rotating shaft 21 to rotate. The rotation of the rotating shaft 21 drives the gear 22 to rotate, which in turn drives the two toothed plates 23 to move synchronously. The synchronous movement of the two toothed plates 23 drives the two gears to move synchronously. The synchronous movement of two fixed sleeves 24 can drive the synchronous movement of two multi-stage electric telescopic rods 13. The synchronous movement of the two multi-stage electric telescopic rods 13 can drive the two locking plates 14 to move toward the locking post 17. The locking plates 14 and the locking post 17 can lock each other to limit the stabilizing plate 16, so that after the hook 15 lifts the item, the item will not swing during transportation, so that the item can be lifted stably, thereby avoiding the danger of the item swinging in the air and falling during lifting.

[0030] All standard parts used in this utility model can be purchased from the market, and irregular parts can be customized according to the description and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the prior art. The machinery, parts and equipment adopt conventional models in the prior art. In addition, the circuit connection adopts conventional connection methods in the prior art, which will not be described in detail here. The contents not described in detail in this specification belong to the prior art known to those skilled in the art.

[0031] Although embodiments of the present invention have been shown and described, the scope of the present invention will be defined by the appended claims and their equivalents for those skilled in the art.

Claims

1. A swing-preventing stabilizing structure for hoisting a multi-rotor drone, characterized by, The utility model provides a kind of unmanned aerial vehicle hoisting device, including unmanned aerial vehicle body (1) and hoisting mechanism (3), the lower side of the hoisting mechanism (3) is provided with stabilizing mechanism (10), the stabilizing mechanism (10) includes fixed frame (11), telescopic mechanism (12) and stabilizing plate (16), the fixed frame (11) is arranged in the lower side of the hoisting mechanism (3), the telescopic mechanism (12) is arranged in the lower side of the fixed frame (11), the telescopic mechanism (12) both sides are provided with multiple-stage electric telescopic rod (13), the multiple-stage electric telescopic rod (13) output end is fixedly installed with clamping plate (14), the stabilizing plate (16) is arranged in the output end of the hoisting mechanism (3), the stabilizing plate (16) upper side is fixedly installed with clamping column (17), the clamping column (17) and the one side of two clamping plate (14) are all provided with clamping groove (18), the clamping plate (14) and the clamping column (17) are mutually clamped by the clamping groove (18).

2. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 1, characterized in that, The telescopic mechanism (12) includes fixed shell (19), rotating shaft (21), gear (22) and toothed plate (23), the number of the toothed plate (23) is two.

3. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 2, characterized in that, The fixed shell (19) is fixedly installed in the lower side of the fixed frame (11), the fixed shell (19) is internally provided with sliding cavity (20), the rotating shaft (21) is rotatably installed in the sliding cavity (20), the gear (22) is fixedly installed on the rotating shaft (21) periphery, the toothed plate (23) is slidably installed in the sliding cavity (20), and the toothed plate (23) is engaged with the gear (22).

4. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 3, characterized in that, One end of two toothed plates (23) is fixedly installed with fixed sleeve (24), and two fixed sleeves (24) are respectively located at both ends of the fixed shell (19). The multi-stage electric telescopic rod (13) is fixedly installed in the fixed sleeve (24).

5. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 3, wherein The rotating shaft (21) periphery is fixedly installed with turbine (25), the sliding cavity (20) inner wall one side is provided with recess, the recess is fixedly installed with rotating motor (27), the rotating motor (27) output end is fixedly installed with worm (26), and the worm (26) is engaged with the turbine (25).

6. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 1, wherein The hoisting mechanism (3) includes mounting frame (4), winding roller (5), lifting rope (6) and lifting hook (15), the mounting frame (4) is fixedly installed in the lower side of the unmanned aerial vehicle body (1), the winding roller (5) is rotatably installed between the mounting frame (4), the lifting rope (6) is wound and arranged on the periphery of the winding roller (5), the stabilizing plate (16) is fixedly installed at one end of the lifting rope (6), the lifting hook (15) is fixedly installed in the lower side of the stabilizing plate (16), and the driving motor (9) is fixedly installed on the inner wall of the mounting frame (4) one side. The output end of the driving motor (9) is fixedly connected with one end of the winding roller (5).

7. The sway-prevention stabilizing structure for hoisting a multi-copter drone according to claim 6, characterized in that, The lower side of the unmanned aerial vehicle body (1) is fixedly installed with two supporting legs (2), and the mounting frame (4) is located between the two supporting legs (2).

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