Unmanned aerial vehicle fertilization device
By adopting air blades and rotary frame structures in the drone fertilization device, combining long pipe spraying pipes and multiple spray ports, the problems of small coverage and low efficiency in the prior art are solved, and wider fertilization coverage and higher fertilization efficiency are achieved.
Patent Information
- Application Number
- CN202421952504.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-13
- Publication Date
- 2025-06-20
- Estimated Expiration
- 2034-08-13
AI Technical Summary
When the existing drone fertilization device is fertilized in a large area, the spray coverage area is small and the spray range for a single flight is limited, resulting in multiple flights, high flight frequency, large drone consumption, and low overall spraying and fertilization efficiency.
A drone fertilization device is designed, using air blades and rotary frame structures, using airflow to drive the air blades to rotate, and the swelling frame and spraying pipes to achieve full integration of fertilizers and water and extensive spraying. The device is equipped with a spray tube in the form of a long tube and a plurality of spray ports. The booster pump is used to increase the pressure of the fertilizer solution and ensure uniformity and coverage of the spray.
Through this device, the spray range of a single flight is wider, which reduces the flight frequency of the drone, reduces consumption, improves fertilization efficiency, and is convenient to disassemble, simple to operate and flexible to use.
Smart Images

Figure CN223001681U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle fertilizing device. Background Art
[0002] In modern agricultural planting, in order to prevent and solve pests and supplement nutrients for crops, fertilization is an essential task. Some traditional fertilization methods are mostly completed by manual fertilization and mechanized fertilization. With the development of technology, the application of unmanned aerial vehicles in agricultural planting is also increasing, and the method of using unmanned aerial vehicles for auxiliary fertilization is becoming more and more common. In the prior art, some fertilizers are produced by the fusion of solid fertilizers and water, and most of the fertilization tanks of unmanned aerial vehicles are equipped with micro drive motors to stir the fertilizer liquid in the fertilization tank to prevent the insufficient dissolution of solid fertilizers from affecting the fertilization effect. This kind of drive motor is relatively energy-consuming;
[0003] An existing unmanned aerial vehicle fertilizing device with the publication number of CN213974473U can drive the fan to rotate by using the wind force generated when the body flies through the setting of the second rotating rod and the fan in cooperation with the second bevel gear. When the fan rotates, it will drive the first rotating rod to rotate through the second rotating rod. At this time, the first rotating rod can stir the fertilizer liquid in the storage tank through the cross plate. This can not only prevent the precipitation of the fertilizer solution in the storage tank but also play an energy-saving role. However, considering its overall structure, the spraying position coverage area of its structure is small, and the spraying range of a single flight is limited. Therefore, when carrying out spraying fertilization work for a large area, in order to achieve the requirement of uniform coverage spraying, the unmanned aerial vehicle needs to fly multiple times, with a high flight frequency, large consumption of the unmanned aerial vehicle, and often needs to be charged multiple times, and the overall spraying fertilization efficiency is not high. Summary of the Utility Model
[0004] The purpose of the utility model is to solve the deficiencies existing in the prior art and to propose an unmanned aerial vehicle fertilizing device.
[0005] To achieve the above object, the utility model adopts the following technical solutions: An unmanned aerial vehicle fertilizing device, comprising an unmanned aerial vehicle body, a liquid storage tank is fixedly connected to the bottom of the unmanned aerial vehicle body, a mixing chamber is arranged inside the liquid storage tank, a stirring frame is rotatably connected inside the mixing chamber, a rotating frame is fixedly connected to the top of the stirring frame and located above the liquid storage tank, a wind blade is fixedly connected to the rotating frame, a liquid outlet pipe is fixedly connected to the bottom of the liquid storage tank, a booster pump is fixedly connected to the liquid outlet pipe, and the bottom end of the liquid outlet pipe is fixedly connected to a connecting frame, a locking groove is arranged on the connecting frame, a spray pipe in the form of a long pipe is arranged below the liquid storage tank, a connecting frame is arranged at the middle position of the spray pipe, a connecting groove is arranged at the top of the connecting frame, and an activity groove communicated with the connecting groove is arranged on the connecting frame, a locking block is nested and slidably connected inside the activity groove, a pulling frame is fixedly connected to one end of the locking block, and a plurality of spray openings are evenly distributed at the bottom of the spray pipe.
[0006] As a further description of the above technical solution:
[0007] The position where the central axis of the stirring frame is connected to the liquid storage tank is positioned and installed through a bearing.
[0008] As a further description of the above technical solution:
[0009] A plurality of the wind blades are arranged and evenly distributed on the side surface of the rotating frame.
[0010] As a further description of the above technical solution:
[0011] A feed inlet is arranged at the top of the liquid storage tank.
[0012] As a further description of the above technical solution:
[0013] The connecting frame and the connecting groove are arranged in a nested fit, the locking block and the locking groove are arranged in a nested fit, and two groups of the locking block and the locking groove are correspondingly arranged.
[0014] As a further description of the above technical solution:
[0015] A sealing gasket is arranged at the bottom of the inner wall of the connecting groove.
[0016] As a further description of the above technical solution:
[0017] A fixing groove is arranged at the bottom of the inner wall of the activity groove, a moving block is slidably connected inside the fixing groove, a spring is connected between the inner wall of the fixing groove and the outer surface of the moving block, and the moving block is fixedly connected to the locking block.
[0018] As a further description of the above technical solution:
[0019] A liquid level scale is provided on the liquid storage tank.
[0020] The utility model has the following beneficial effects:
[0021] For the unmanned aerial vehicle fertilizing device, through the arrangement of the wind blades and the rotating frame structure, when the unmanned aerial vehicle is flying, affected by the air flow, the wind blades drive the rotating frame to rotate, and then the stirring frame can be driven to rotate, so as to stir the water body in the liquid storage tank, which can promote the full dissolution of the fertilizer and the water body, ensure the sufficiency of the nutrients in the fertilizer solution, and avoid the deposition of the fertilizer; through the arrangement of the booster pump, it is convenient to send the fertilizer solution in the liquid storage tank into the spraying pipe through the liquid outlet pipe, and finally spray out from multiple spraying ports. The arrangement of the long-tube spraying pipe and multiple spraying ports can make the range of single fertilization wider, and the range of single-flight spraying fertilization is wider. When fertilizing a large area, the flight frequency of the unmanned aerial vehicle can be reduced, the consumption can be reduced, and the spraying efficiency can be improved; through the arrangement of structures such as the connecting frame, the connecting groove, the locking block, and the locking groove, only the spraying pipe can be stably docked and installed with the liquid outlet pipe, so that stable spraying fertilization work can be carried out. At the same time, the structure can be conveniently disassembled, convenient for storage, simple in structure operation, and flexible and convenient to use. Description of the Drawings
[0022] Figure 1 is a schematic diagram of the overall structure of a unmanned aerial vehicle fertilizing device proposed by the utility model;
[0023] Figure 2 is a front view of a unmanned aerial vehicle fertilizing device proposed by the utility model;
[0024] Figure 3 is a unmanned aerial vehicle fertilizing device proposed by the utility model Figure 2 is an enlarged view of A in
[0025] Legend:
[0026] 1, unmanned aerial vehicle body; 2, liquid storage tank; 3, mixing chamber; 4, stirring frame; 5, rotating frame; 6, wind blades; 7, feed inlet; 8, liquid outlet pipe; 9, booster pump; 10, connecting frame; 11, locking groove; 12, spraying pipe; 13, connecting frame; 14, connecting groove; 15, sealing gasket; 16, movable groove; 17, locking block; 18, pulling frame; 19, fixing groove; 20, moving block; 21, spring; 22, spraying port; 23, liquid level scale. Detailed Embodiments
[0027] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.
[0028] In the description of the present invention, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings. It is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to the present invention. The terms "first", "second", "third" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance. In addition, unless otherwise clearly defined and limited, the terms "installation", "connection", "connection" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific situations.
[0029] Referring to Figures 1-3 , an embodiment provided by the present invention: a drone fertilization device, including a drone body 1, a liquid storage tank 2 is fixedly connected to the bottom of the drone body 1, a mixing chamber 3 is arranged inside the liquid storage tank 2, a stirring frame 4 is rotatably connected inside the mixing chamber 3, the connection position between the central axis of the stirring frame 4 and the liquid storage tank 2 is positioned and installed through a bearing, and a plurality of stirring rods are arranged at the position of the stirring frame 4 inside the mixing chamber 3. When rotating, the water body inside the mixing chamber 3 can be stirred, so that the fertilizer can be fully dissolved with the water body, avoiding sedimentation. Thus, the sufficiency of the nutrients in the fertilizer solution is ensured, and the situation of fertilizer sedimentation is also avoided. A rotating frame 5 is fixedly connected to the top of the stirring frame 4 and above the liquid storage tank 2, a wind blade 6 is fixedly connected to the rotating frame 5, a plurality of wind blades 6 are provided and evenly distributed on the side surface of the rotating frame 5. The wind blade 6 is in the form of a blade. When the drone is flying, the airflow can drive the wind blade 6 to rotate, so as to drive the rotating frame 5 to rotate, and the rotating frame 5 can drive the stirring frame 4 to rotate for stirring work. A liquid outlet pipe 8 is fixedly connected to the bottom of the liquid storage tank 2, a booster pump 9 is fixedly connected to the liquid outlet pipe 8, and the bottom end of the liquid outlet pipe 8 is fixedly connected to a connecting frame 10. A locking groove 11 is arranged on the connecting frame 10. A spray pipe 12 in the form of a long pipe is arranged below the liquid storage tank 2, asFigures 1-2 As shown, the spraying pipe 12 is in the form of a long pipe, which can ensure a wider spraying coverage area. A large area can be covered in a single flight. When spraying a large area, the flight frequency of the drone can be reduced, and the fertilization efficiency can be improved. An adapter 13 is provided at the middle position of the spraying pipe 12. A connecting groove 14 is provided at the top of the adapter 13, and a movable groove 16 communicating with the connecting groove 14 is provided on the adapter 13. A locking block 17 is nested and slidably connected in the movable groove 16. The connecting frame 10 and the connecting groove 14 are nested and matched. The locking block 17 and the locking groove 11 are nested and matched, and two groups of the locking block 17 and the locking groove 11 are correspondingly arranged. The settings of structures such as the connecting frame 10, the connecting groove 14, the locking block 17, and the locking groove 11 can not only make the spraying pipe 12 stably dock with the liquid outlet pipe 8 for stable spraying work, but also be conveniently disassembled for easy storage. One end of the locking block 17 is fixedly connected with a pulling frame 18. A plurality of spraying ports 22 are evenly distributed at the bottom of the spraying pipe 12. The booster pump 9 can transport the fertilizer solution into the spraying pipe 12 through the liquid outlet pipe 8 and finally spray it out from the spraying ports 22.
[0030] A feed inlet 7 is provided at the top of the liquid storage tank 2. The setting of the feed inlet 7 can facilitate the addition of fertilizers and water into the liquid storage tank 2. A lid can be provided on the feed inlet 7 to seal it, ensuring that the fertilizer solution will not splash out from the feed inlet 7 during the flight fertilization of the drone.
[0031] A sealing gasket 15 is provided at the bottom inner wall of the connecting groove 14. The setting of the sealing gasket 15 can ensure the tightness of the docking between the connecting frame 10 and the connecting groove 14.
[0032] A fixing groove 19 is provided at the bottom inner wall of the movable groove 16. A moving block 20 is slidably connected in the fixing groove 19, and a spring 21 is connected between the inner wall of the fixing groove 19 and the outer surface of the moving block 20. The moving block 20 is fixedly connected with the locking block 17. The elastic action of the spring 21 can push the moving block 20 to drive the locking block 17 to stably insert into the locking groove 11, thereby ensuring the stability of the structural connection. At the same time, when the locking block 17 is pulled, the moving block 20 can also be driven to compress the spring 21, so that the locking block 17 can normally slide out of the locking groove 11, facilitating the disassembly of the structure.
[0033] A liquid level scale 23 is provided on the liquid storage tank 2. The setting of this structure can facilitate the observation of the liquid level in the liquid storage tank 2.
[0034] Working principle: When using the drone fertilization device, insert the connecting frame 10 into the connecting groove 14 and insert the locking block 17 into the locking groove 11, then the spraying pipe 12 can be docked with the liquid outlet pipe 8. When the drone is flying, the airflow will drive the wind blade 6 to rotate, the wind blade 6 drives the rotating frame 5 to rotate, and the rotating frame 5 drives the stirring frame 4 to rotate, so as to stir the water body, making the fertilizer fully dissolve with the water body. The booster pump 9 sends the fertilizer solution into the spraying pipe 12 through the liquid outlet pipe 8 and finally sprays out from the spraying port 22 position, then the spraying and fertilization work can be carried out.
[0035] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.
Claims
1. A drone fertilizing device, comprising a drone body (1), characterized in that: The bottom of the unmanned aerial vehicle (1) is fixedly connected to a liquid storage tank (2), a mixing chamber (3) is provided in the liquid storage tank (2), a stirring frame (4) is rotatably connected in the mixing chamber (3), a rotating frame (5) is fixedly connected to the top of the stirring frame (4) and located above the liquid storage tank (2), a fan blade (6) is fixedly connected to the rotating frame (5), a liquid outlet pipe (8) is fixedly connected to the bottom of the liquid storage tank (2), a booster pump (9) is fixedly connected to the liquid outlet pipe (8), and a connecting frame (10) is fixedly connected to the bottom end of the liquid outlet pipe (8), and the connecting frame (10) A locking groove (11) is arranged on the top, a long tube-shaped spray pipe (12) is arranged below the liquid storage tank (2), a connecting frame (13) is arranged in the middle of the spray pipe (12), a connecting groove (14) is arranged on the top of the connecting frame (13), and a movable groove (16) connected to the connecting groove (14) is arranged on the connecting frame (13), a locking block (17) is nested and slidably connected in the movable groove (16), one end of the locking block (17) is fixedly connected to a pulling frame (18), and a plurality of spraying ports (22) are evenly distributed on the bottom of the spray pipe (12).
2. The drone fertilization device according to claim 1, characterized in that: The position where the central axis of the stirring frame (4) connects with the liquid storage tank (2) is positioned and installed via a bearing.
3. The drone fertilization device according to claim 1, characterized in that: The fan blades (6) are provided in plurality and are evenly distributed on the side surface of the rotating frame (5).
4. The drone fertilizing device according to claim 1, characterized in that: The top of the liquid storage tank (2) is provided with a feed inlet (7).
5. The drone fertilizing device according to claim 1, characterized in that: The connecting frame (10) and the connecting groove (14) are arranged in a nested manner, the locking block (17) and the locking groove (11) are arranged in a nested manner, and two groups of locking blocks (17) and locking grooves (11) are arranged correspondingly.
6. The drone fertilizing device according to claim 1, characterized in that: A sealing gasket (15) is provided at the bottom of the inner wall of the connecting groove (14).
7. The drone fertilizing device according to claim 1, characterized in that: A fixed groove (19) is provided at the bottom of the inner wall of the movable groove (16), a moving block (20) is slidably connected in the fixed groove (19), and a spring (21) is connected between the inner wall of the fixed groove (19) and the outer surface of the moving block (20), and the moving block (20) is fixedly connected to the locking block (17).
8. The drone fertilizing device according to claim 1, characterized in that: The liquid storage tank (2) is provided with a liquid level scale (23).
Citation Information
Patent Citations
Unmanned aerial vehicle fertilization device
CN213974473U