Multi-shaft agricultural unmanned aerial vehicle

By designing a multi-axis agricultural drone, the connection between the support crossbar and the drive motor, combined with the weighing mounting mechanism and buffer landing components, the problems of non-versatility and tension detection of the drone when mounted different boxes are solved, and the convenient mounting, tension detection and landing protection of the box is achieved, ensuring the safety and reliability of the drone.

CN222921778UActive Publication Date: 2025-05-30HAINAN SAIFA TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202422046109.0
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-08-22
Publication Date
2025-05-30
Estimated Expiration
2034-08-22

AI Technical Summary

Technical Problem

Existing agricultural drones are not universal when mounting boxes for spraying, fertilization, seeding, etc., and it is difficult to detect tension during the mounting process, which can easily lead to damage to the drone.

Method used

A multi-axis agricultural drone is designed, which uses a uniformly installed support crossbar to connect to the drive motor. It uses a weighing mounting mechanism and buffer landing assembly to realize universal mounting and tension detection of the box, and provides buffer protection when landing.

Benefits of technology

It realizes convenient mounting of the box and detection of the drone tension, avoids falling problems caused by overweight, and provides good buffering protection when landing, ensuring the safety and reliability of the drone.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

The utility model discloses a multi-shaft agricultural unmanned aerial vehicle which comprises an unmanned aerial vehicle body, a plurality of supporting cross rods are evenly installed on the unmanned aerial vehicle body, driving motors are fixedly installed at the other ends of the supporting cross rods, spiral blades are installed at the output ends of the driving motors, front supports are symmetrically installed at the front end of the unmanned aerial vehicle body, and rear supports are symmetrically installed at the rear end of the unmanned aerial vehicle body. The unmanned aerial vehicle comprises an unmanned aerial vehicle body, a front support is installed on the unmanned aerial vehicle body, a high-altitude camera is installed on the front support and electrically connected with the unmanned aerial vehicle body, a weighing type mounting mechanism is installed at the bottom of the unmanned aerial vehicle body, and buffering landing assemblies are symmetrically installed at the bottom of the unmanned aerial vehicle body. The box body is conveniently hung below an unmanned aerial vehicle body, meanwhile, the pulling force on the unmanned aerial vehicle is detected, the safety of the unmanned aerial vehicle is ensured, and meanwhile, a good buffering effect is achieved during landing.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and more specifically, to a multi-axis agricultural unmanned aerial vehicle. Background Technique

[0002] An unmanned aerial vehicle, also known as an unmanned aircraft, and an agricultural unmanned aerial vehicle is an unmanned aircraft used for agricultural and forestry plant protection operations. This type of unmanned aerial vehicle consists of a flight platform (fixed-wing, helicopter, multi-axis aircraft), a navigation flight control, and a spraying mechanism. Through ground remote control or navigation flight control, spraying operations can be achieved, and agents, seeds, powders, etc. can be sprayed.

[0003] When an agricultural unmanned aerial vehicle is in use, a box for spraying, fertilizing, sowing and other operations needs to be hung at its bottom. Since the boxes used for spraying, fertilizing, sowing and other operations are different, the existing agricultural unmanned aerial vehicles cannot be universal when being hung, resulting in more trouble. At the same time, when the existing unmanned aerial vehicles are hung, the bearing tension cannot be detected, which easily causes damage to the unmanned aerial vehicle.

[0004] In view of the problems in the related art, no effective solution has been proposed yet. Content of the Utility Model

[0005] Aiming at the deficiencies existing in the prior art, the purpose of the utility model is to propose a multi-axis agricultural unmanned aerial vehicle.

[0006] To achieve the above purpose, the utility model is realized through the following technical solutions. A multi-axis agricultural unmanned aerial vehicle includes an unmanned aerial vehicle body. A plurality of support crossbars are evenly installed on the unmanned aerial vehicle body. The other ends of the support crossbars are fixedly installed with drive motors, and the output ends of the drive motors are all installed with spiral blades. The front end of the unmanned aerial vehicle body is symmetrically installed with front brackets. An aerial camera is installed on the front brackets, and the aerial camera is electrically connected to the unmanned aerial vehicle body. A weighing type hanging mechanism is installed at the bottom of the unmanned aerial vehicle body. Buffer landing components are symmetrically installed at the bottom of the unmanned aerial vehicle body.

[0007] Preferably, the weighing type hanging mechanism includes a mounting plate fixed to the bottom of the unmanned aerial vehicle body. Sliding plates I are symmetrically arranged at the bottom of the mounting plate. A C-shaped connecting plate is arranged below the mounting plate. Sliding plates II are symmetrically arranged on the C-shaped connecting plate. T-shaped guide blocks are arranged on the outer sides of the sliding plates II. T-shaped chutes matching the T-shaped guide blocks are arranged on the inner sides of the sliding plates I. Connecting columns are symmetrically arranged between the mounting plate and the C-shaped connecting plate. A tension sensor is connected between the connecting columns.

[0008] Preferably, a chemical spraying assembly is provided below the C-shaped connecting plate. Symmetrically arranged above the chemical spraying assembly are connecting side plates. Mounting holes are provided on both the C-shaped connecting plate and the connecting side plates. Mounting screws are passed through the mounting holes, and limit nuts are provided at both ends of the mounting screws.

[0009] Preferably, the chemical spraying assembly includes a chemical storage tank. A sealing cover is detachably mounted on the chemical storage tank. An anti-clogging filter screen I and an anti-clogging filter screen II are respectively installed in the chemical storage tank, and the pore diameter of the anti-clogging filter screen I is larger than that of the anti-clogging filter screen II.

[0010] Preferably, a submersible pump is installed at one end of the chemical storage tank located inside the anti-clogging filter screen II. The output end of the submersible pump is connected through a connecting pipe to a spraying cross pipe located outside the chemical storage tank. A plurality of groups of nozzles are provided on the spraying cross pipe.

[0011] Preferably, the buffer landing assembly includes a buffer support plate. A support frame is mounted on the buffer support plate. A sliding cross plate is arranged inside the support frame. Sliding blocks are provided at both ends of the sliding cross plate. Sliding grooves matching the sliding blocks are provided on both sides of the inner wall of the support frame. Elastic rubber columns are provided between the sliding cross plate and the buffer support plate.

[0012] Preferably, three support columns movably passing through the top of the support frame are mounted on the sliding cross plate. An assembly plate fixedly connected to the bottom of the UAV body is connected between the tops of the support columns. Springs are sleeved outside the support columns between the assembly plate and the support frame. A rubber gasket is provided at the bottom of the buffer support plate.

[0013] The present utility model provides a multi-axis agricultural UAV, and the beneficial effects are as follows:

[0014] The UAV body is connected to the driving motor through a support cross bar. The driving motor drives the spiral blades to rotate. The provided front bracket is used to mount a high-altitude camera, which is convenient for high-altitude shooting and information collection. The provided weighing type hanging mechanism, when the UAV is used for operations such as spraying chemicals and fertilizing crops, not only is it convenient to hang the box body below the UAV body, but also can detect the pulling force on the UAV, avoiding the problem of the UAV falling due to overweight. The provided buffer landing assembly can play a buffering role when the UAV lands, protecting the UAV. The structure of the present utility model is simple. During spraying and fertilizing operations, it is convenient to hang the box body below the UAV body, while detecting the pulling force on the UAV to ensure the safety of the UAV. At the same time, it has a good buffering effect during landing. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0016] Figure 1 is the front view of a multi-axis agricultural drone according to an embodiment of the present invention;

[0017] Figure 2 is the structural schematic diagram of a weighing type mounting mechanism in a multi-axis agricultural drone according to an embodiment of the present invention;

[0018] Figure 3 is the internal structural schematic diagram of a chemical spraying component in a multi-axis agricultural drone according to an embodiment of the present invention;

[0019] Figure 4 is the structural schematic diagram of a buffer landing component in a multi-axis agricultural drone according to an embodiment of the present invention.

[0020] In the figure:

[0021] 1, drone body; 2, support cross bar; 3, drive motor; 4, spiral blade; 5, high-altitude camera; 6, front support; 7, weighing type mounting mechanism; 8, buffer landing component; 9, mounting plate; 10, sliding plate one; 11, C-shaped connecting plate; 12, rubber gasket; 13, T-shaped guiding block; 14, connecting column; 15, tension sensor; 16, chemical spraying component; 17, connecting side plate; 18, mounting screw; 19, limit nut; 20, chemical storage tank; 21, sealing cover; 22, anti-blocking filter one; 23, anti-blocking filter two; 24, submersible pump; 25, spraying cross pipe; 26, nozzle; 27, buffer support plate; 28, support frame; 29, sliding cross plate; 30, sliding block; 31, chute; 32, elastic rubber column; 33, support column; 34, assembly plate; 35, spring. Detailed implementation manners

[0022] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention. Obviously, the described embodiments are only some embodiments of the present invention, rather than all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts belong to the scope of protection of the present invention.

[0023] Please refer to Figures 1-4, the present utility model provides a multi-axis agricultural drone, including a drone body 1. A plurality of support crossbars 2 are evenly installed on the drone body 1. The other ends of the support crossbars 2 are fixedly installed with drive motors 3, and spiral blades 4 are installed at the output ends of the drive motors 3. The drone body 1 is connected to the drive motors 3 through the support crossbars 2, and the spiral blades 4 are driven to rotate by the drive motors 3. Front brackets 6 are symmetrically installed at the front end of the drone body 1. An aerial camera 5 is installed on the front brackets 6, and the aerial camera 5 is electrically connected to the drone body 1. The provided front brackets 6 are used to install the aerial camera 5, facilitating aerial shooting and information collection. A weighing type mounting mechanism 7 is installed at the bottom of the drone body 1, and buffer landing components 8 are symmetrically installed at the bottom of the drone body 1. The provided weighing type mounting mechanism 7, when the drone is used for tasks such as spraying pesticides and fertilizing crops, not only facilitates hanging the box body below the drone body 1, but also can detect the pulling force on the drone, avoiding the problem of the drone falling due to excessive weight. The provided buffer landing components 8 can play a buffering role when the drone lands, protecting the drone.

[0024] In one embodiment, please refer to the attached drawings of the specification Figure 2 As shown, the weighing type mounting mechanism 7 includes a mounting plate 9 fixed to the bottom of the drone body 1. Sliding plates one 10 are symmetrically arranged at the bottom of the mounting plate 9. A C-shaped connecting plate 11 is arranged below the mounting plate 9. Sliding plates two are symmetrically arranged on the C-shaped connecting plate 11. T-shaped guide blocks 13 are arranged on the outer sides of the sliding plates two. T-shaped sliding grooves matching the T-shaped guide blocks 13 are arranged on the inner sides of the sliding plates one 10. Connecting columns 14 are symmetrically arranged between the mounting plate 9 and the C-shaped connecting plate 11. A tension sensor 15 is connected between the connecting columns 14. A chemical spraying assembly 16 is arranged below the C-shaped connecting plate 11. Connecting side plates 17 are symmetrically arranged above the chemical spraying assembly 16. Mounting holes are arranged on both the C-shaped connecting plate 11 and the connecting side plates 17. Mounting screws 18 penetrate through the mounting holes, and limit nuts 19 are arranged at both ends of the mounting screws 18. Through the cooperation of the provided mounting screws 18 and the limit nuts 19, the installation of the C-shaped connecting plate 11 and the chemical spraying assembly 16 is realized. Similarly, when fertilizing, the corresponding fertilizing box can also be installed in the above manner. After installation, a tension sensor 15 is connected between the mounting plate 9 and the C-shaped connecting plate 11 through two connecting columns 14, thereby detecting the pulling force generated by the chemical agent box body below to prevent excessive pulling force from affecting the drone. The provided T-shaped sliding grooves and T-shaped guide blocks 13 ensure the positions of the sliding plates one 10 and the sliding plates two.

[0025] In one embodiment, please refer to the attached drawings of the specification Figure 3As shown, the medicament spraying assembly 16 includes a medicament storage tank 20, on which a sealing cover 21 is detachably installed. An anti-clogging filter screen one 22 and an anti-clogging filter screen two 23 are respectively installed in the medicament storage tank 20, and the pore diameter of the anti-clogging filter screen one 22 is larger than that of the anti-clogging filter screen two 23. A submersible pump 24 is installed at one end of the anti-clogging filter screen two 23 in the medicament storage tank 20. The output end of the submersible pump 24 is connected through a connecting pipe to a spraying cross pipe 25 located outside the medicament storage tank 20, and a plurality of groups of nozzles 26 are arranged on the spraying cross pipe 25. The impurities in the medicament are filtered by the provided anti-clogging filter screen one 22 and anti-clogging filter screen two 23 to avoid clogging. The provided submersible pump 24 conveys the medicament to be sprayed out through the nozzles 26 on the spraying cross pipe 25 for spraying on crops.

[0026] In one embodiment, please refer to the accompanying Figure 4 As shown, the buffer landing assembly 8 includes a buffer support plate 27, on which a support frame 28 is installed. A sliding cross plate 29 is arranged in the support frame 28. Sliding blocks 30 are arranged at both ends of the sliding cross plate 29. Sliding grooves 31 matching the sliding blocks 30 are arranged on both sides of the inner wall of the support frame 28. Elastic rubber columns 32 are arranged between the sliding cross plate 29 and the buffer support plate 27. Three support columns 33 that penetrate through the top of the support frame 28 are installed on the sliding cross plate 29. An assembly plate 34 fixedly connected to the bottom of the UAV body 1 is connected between the tops of the support columns 33. Springs 35 are sleeved outside the support columns 33 between the assembly plate 34 and the support frame 28. A rubber gasket 12 is arranged at the bottom of the buffer support plate 27. When the UAV lands, the pressure generated during its descent is transmitted to the support columns 33 through the assembly plate 34, causing the sliding cross plate 29 to descend. The provided springs 35 and elastic rubber columns 32 play a buffering role.

[0027] During actual application, the UAV body 1 is connected to the driving motor 3 through the support cross bar 2, and the driving motor 3 is used to drive the spiral blades 4 to rotate. The provided front bracket 6 is used to install the high-altitude camera 5 for convenient high-altitude shooting and information collection. The provided weighing type mounting mechanism 7, when the UAV is used for operations such as spraying medicament and fertilizing on crops, not only facilitates mounting the box body under the UAV body 1, but also can detect the pulling force on the UAV to avoid the problem of the UAV falling due to exceeding the weight. The provided buffer landing assembly 8 can play a buffering role when the UAV lands and protect the UAV. The structure of the present utility model is simple. During spraying medicament and fertilizing operations, it is convenient to mount the box body under the UAV body 1, and at the same time detect the pulling force on the UAV to ensure the safety of the UAV. At the same time, it has a good buffering effect during landing.

[0028] Although this specification is described in terms of embodiments, not every embodiment contains only one independent technical solution. This narrative style of the specification is only for clarity. Those skilled in the art should regard the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A multi-axis agricultural drone, characterized in that: The invention comprises an unmanned aerial vehicle body (1), wherein a plurality of supporting cross bars (2) are evenly mounted on the unmanned aerial vehicle body (1), a driving motor (3) is fixedly mounted on the other end of the supporting cross bars (2), and a spiral blade (4) is mounted on the output end of each driving motor (3), a front bracket (6) is symmetrically mounted on the front end of the unmanned aerial vehicle body (1), a high-altitude camera (5) is mounted on the front bracket (6), and the high-altitude camera (5) is electrically connected to the unmanned aerial vehicle body (1), a weighing mounting mechanism (7) is mounted on the bottom of the unmanned aerial vehicle body (1), and a buffer landing assembly (8) is symmetrically mounted on the bottom of the unmanned aerial vehicle body (1).

2. A multi-axis agricultural drone according to claim 1, characterized in that: The weighing mounting mechanism (7) comprises a mounting plate (9) fixed to the bottom of the UAV body (1), a sliding plate 1 (10) is symmetrically arranged at the bottom of the mounting plate (9), a C-shaped connecting plate (11) is arranged below the mounting plate (9), a sliding plate 2 is symmetrically arranged on the C-shaped connecting plate (11), a T-shaped guide block (13) is arranged on the outer side of the sliding plate 2, a T-shaped slide groove matching the T-shaped guide block (13) is arranged on the inner side of the sliding plate 1 (10), connecting columns (14) are symmetrically arranged between the mounting plate (9) and the C-shaped connecting plate (11), and a tension sensor (15) is connected between the connecting columns (14).

3. A multi-axis agricultural drone according to claim 2, characterized in that: A medicine spraying assembly (16) is arranged below the C-shaped connecting plate (11), and a connecting side plate (17) is symmetrically arranged above the medicine spraying assembly (16). The C-shaped connecting plate (11) and the connecting side plate (17) are both provided with mounting holes, and a mounting screw (18) is arranged through the mounting hole, and limit nuts (19) are arranged at both ends of the mounting screw (18).

4. A multi-axis agricultural drone according to claim 3, characterized in that: The medicine spraying assembly (16) comprises a medicine storage box (20), on which a sealing cover (21) is detachably mounted, and an anti-clogging filter screen 1 (22) and an anti-clogging filter screen 2 (23) are respectively mounted in the medicine storage box (20), and the mesh diameter of the anti-clogging filter screen 1 (22) is larger than the mesh diameter of the anti-clogging filter screen 2 (23).

5. A multi-axis agricultural drone according to claim 4, characterized in that: A submersible pump (24) is installed at one end of the anti-clogging filter screen 2 (23) in the medicine storage box (20), and the output end of the submersible pump (24) is connected to a spraying transverse pipe (25) located outside the medicine storage box (20) through a connecting pipe, and an array of nozzles (26) are arranged on the spraying transverse pipe (25).

6. A multi-axis agricultural drone according to claim 5, characterized in that: The buffer drop assembly (8) comprises a buffer support plate (27), a support frame (28) is mounted on the buffer support plate (27), a sliding transverse plate (29) is arranged in the support frame (28), sliding blocks (30) are arranged at both ends of the sliding transverse plate (29), sliding grooves (31) matching the sliding blocks (30) are arranged on both sides of the inner wall of the support frame (28), and an elastic rubber column (32) is arranged between the sliding transverse plate (29) and the buffer support plate (27).

7. A multi-axis agricultural drone according to claim 6, characterized in that: The sliding horizontal plate (29) is provided with three support columns (33) which are movable and pass through the top of the support frame (28); the top ends of the support columns (33) are connected with an assembly plate (34) which is fixedly connected to the bottom of the drone body (1); a spring (35) is sleeved outside the support columns (33) and is located between the assembly plate (34) and the support frame (28); and a rubber gasket (12) is provided at the bottom of the buffer support plate (27).