Lightweight plant protection unmanned aerial vehicle with simplified structure
The lightweight and streamlined structural design solves the problem of difficult maintenance of agricultural drones, improves maintenance efficiency and reduces costs, simplifies the maintenance process, and enhances the stability and adaptability of the equipment.
Patent Information
- Application Number
- CN202520314135.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-26
- Publication Date
- 2025-12-19
- Estimated Expiration
- 2035-02-26
AI Technical Summary
The complex installation structure of existing agricultural drones leads to difficult and costly maintenance, and they are also difficult to maintain when used in harsh environments, requiring specialized tools and skills.
It adopts a lightweight and streamlined structural design, including modular load fixing components and screw-in connections, integrating the load mechanism on the landing gear struts, and integrating the battery compartment and flight control expansion mechanism inside the medicine box, reducing the number of parts and intermediate connectors, and using high-strength materials and quick connection methods.
It improves the relocation and maintenance efficiency of drones, reduces maintenance costs, enhances equipment reliability and adaptability, simplifies the maintenance process, extends equipment reliability, improves equipment stability and adaptability, reduces the number of parts, lightens weight, reduces manufacturing costs, simplifies maintenance time, and reduces maintenance costs.
Smart Images

Figure CN223686829U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to unmanned plane technical field especially relates to a light weight simple structure's plant protection unmanned plane. BACKGROUND
[0002] At present, the continuous improvement of plant protection unmanned plane has played a huge role for the development of agricultural intelligence, a large number of manual operation is saved through the operation of plant protection unmanned plane, labor is reduced, the development of agriculture is continuously promoted, and the intelligentization of production and life is realized.
[0003] In the prior art, as the functions of plant protection unmanned plane are more and more, a large number of devices need more and more complex installation structure, which increases the cost and also increases the production and maintenance cost, plant protection unmanned plane is agricultural machinery, and the working environment is relatively poor, needs to work under various climates and environments, and needs to be regularly maintained and repaired at any time. The complex installation structure makes maintenance and maintenance more difficult, once the equipment fails, professional tools and skills are needed for maintenance, and the maintenance time is long, which affects the normal use of unmanned plane, and professional technical personnel are needed for operation, which increases the cost of manpower and material resources.
[0004] Based on the above-mentioned defects, a light weight simple structure's plant protection unmanned plane is provided. CONTENT OF THE UTILITY MODEL
[0005] The utility model aims at: in order to solve the above-mentioned problem, and put forward a light weight simple structure's plant protection unmanned plane.
[0006] In order to realize the above-mentioned purpose, the utility model adopts the following technical scheme: a light weight simple structure's plant protection unmanned plane, including main body and the machine arm power assembly installed on the main body, the bottom of the main body is installed with two pairs of foot support inclined braces through fasteners, the bottom of each pair of foot support inclined braces is provided with a support structure, and a load mechanism is installed between the two pairs of foot support inclined braces through a load fixing part.
[0007] Preferably, the foot support screw is rotatably connected through the main body and the foot support inclined brace.
[0008] Preferably, the foot support inclined brace and the foot support are fixed through a tee joint fixing part.
[0009] Preferably, a battery compartment is formed in the medicine box, a storage battery is placed in the battery compartment, a binding structure fixed with the storage battery is arranged on the medicine box, the output end of the storage battery is electrically connected with the input end of the main body, and the bottom of the medicine box is integrated with a flight control expansion mechanism.
[0010] Preferably, the binding structure includes a binding belt buckled on the medicine box, and a belt passing groove is formed in the medicine box and penetrates the binding belt end.
[0011] Preferably, the flight control expansion mechanism comprises a front obstacle avoidance radar, a ground simulation radar, a water pump and a rear obstacle avoidance radar fixed on the bottom of the medicine box.
[0012] Therefore, the unmanned aerial vehicle provided by the present application has the advantages that:
[0013] In the present application, the load mechanism is directly installed on the foot support diagonal brace through the load fixing member, and a modular design is adopted to facilitate quick assembly and disassembly. This design significantly improves the transfer efficiency of the unmanned aerial vehicle, reduces the operation preparation time and maintenance time, and the fasteners adopt a screw connection mode, which facilitates quick disassembly and reinstallation, enabling maintenance personnel to more efficiently perform maintenance and replace parts. This design not only improves the maintenance efficiency, but also reduces the maintenance cost.
[0014] In the present application, the expansion equipment is directly concentrated on the medicine box, reducing the fixed structure of the equipment, not only reducing the number of parts and reducing the weight, but also reducing the manufacturing cost. At the same time, the foot support diagonal brace is directly screwed with the main body, reducing the use of intermediate connecting pieces, further reducing the weight, and relatively simplifying the common plant protection unmanned aerial vehicle.
[0015] 3、In the present application, the anti-surge groove structure inside the medicine box effectively hinders the shaking amplitude of the liquid medicine, so that the liquid level of the liquid medicine stabilizes quickly, reducing the influence on the flight stability of the plant protection unmanned aerial vehicle. At the same time, this structure can also strengthen the strength of the medicine box and reduce deformation. BRIEF DESCRIPTION OF DRAWINGS
[0016] Figure 1 A perspective structural schematic diagram of an unmanned aerial vehicle according to an embodiment of the present application is shown;
[0017] Figure 2 An exploded structural schematic diagram of an unmanned aerial vehicle according to an embodiment of the present application is shown;
[0018] Figure 3 A perspective structural schematic diagram of a medicine box according to an embodiment of the present application is shown;
[0019] Figure 4 A top structural schematic diagram of a medicine box according to an embodiment of the present application is shown.
[0020] LEGEND:
[0021] 1, main body; 2, arm power assembly; 3, foot support diagonal brace; 4, foot support screw; 5, load fixing member; 6, foot support; 7, three-way fixing member; 8, medicine box; 9, battery compartment; 10, storage battery; 11, binding belt; 12, belt passing groove; 13, front obstacle avoidance radar; 14, ground simulation radar; 15, water pump; 16, rear obstacle avoidance radar. DETAILED DESCRIPTION
[0022] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to 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 the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the present application.
[0023] Please refer to Figures 1-4 The present application provides a technical solution: a lightweight and simplified structure of plant protection unmanned aerial vehicle, comprising a main body 1 and a machine arm power assembly 2 installed on the main body 1, the bottom of the main body 1 is provided with two pairs of foot support inclined struts 3 through fasteners, the bottom of each pair of foot support inclined struts 3 is provided with a support structure, and a load mechanism is installed between the two pairs of foot support inclined struts 3 through a load fixing piece 5.
[0024] The machine arm power assembly 2 provides the lift and thrust required for flight. The lightweight design of the machine arm power assembly 2 is crucial to improve the endurance and load capacity of the unmanned aerial vehicle. By optimizing the machine arm folding mechanism, the weight can be significantly reduced, and the space occupation of the machine arm power assembly 2 in the non-running state can be reduced, and the overall performance of the structure can be improved.
[0025] The bottom of the foot support inclined strut 3 is provided with a support structure, which is used to enhance the stability and carrying capacity of the foot support. This design helps to improve the operation ability of the unmanned aerial vehicle on complex terrain and improves the start-stop stability of the unmanned aerial vehicle on complex terrain. Different load mechanisms can be directly installed on the foot support inclined strut 3 through the load fixing piece 5, and the modular design is adopted, which is convenient for quick assembly and disassembly, and improves the transfer efficiency of the unmanned aerial vehicle.
[0026] The load mechanism is used to carry pesticides, fertilizers or other agricultural materials, and the load fixing piece 5 is provided to ensure quick loading and unloading and operational convenience. The load fixing piece 5 is prior art, which is made of high-strength materials (such as aluminum alloy, carbon fiber, etc.) to ensure sufficient structural strength and durability, and is equipped with quick connection and release mechanism, such as buckle, bolt, etc., which is convenient for quick loading and unloading of the load.
[0027] Specifically, as Figure 2As shown, the fastener is a foot screw 4, which is screwed through the main body 1 and connected with the foot brace 3. Through screw connection, the foot screw 4 can conveniently fix the foot brace 3 on the main body 1, and the threaded connection can bear a large load, which is suitable for components such as unmanned aerial vehicle footrests that need to bear a certain weight and impact force. The foot screw 4 can be equipped with anti-loosening measures such as spring washers or lock nuts to prevent the screw from loosening due to vibration during flight. When the foot brace 3 needs to be replaced or repaired, the screw-connected foot screw 4 is convenient for quick disassembly and reinstallation, with the characteristics of simple structure, convenient installation and high reliability. This connection method is suitable for the installation of the footrest of the plant protection unmanned aerial vehicle, which can meet the needs of quick assembly and disassembly, and is convenient for maintenance personnel to operate, achieving the purpose of improving the maintenance efficiency of the unmanned aerial vehicle.
[0028] The support structure includes a foot support 6, and the foot brace 3 and the foot support 6 are fixed through a tee fitting 7.
[0029] The foot support 6 is installed at the bottom of the foot brace 3 and contacts the ground, providing stable support for the unmanned aerial vehicle to prevent it from tipping over during takeoff, landing or parking. The foot support 6 can be replaced with a bent structure or a horizontal bar structure according to the height of the load, so as to maintain a safe ground clearance for the corresponding load.
[0030] The tee fitting 7 can simultaneously connect the foot brace 3 and the foot support 6. This design makes the support structure more stable and can withstand forces in multiple directions. The tee fitting 7 is made of high-strength materials such as aluminum alloy, stainless steel, etc. to ensure sufficient structural strength and durability. Considering the convenience of installation, it is usually equipped with threaded holes or clamping slots for quick installation and disassembly, which not only improves the assembly efficiency, but also facilitates maintenance and replacement of parts.
[0031] Specifically, as shown in Figures 1-4 The load mechanism is a medicine box 8, a battery compartment 9 is formed in the medicine box 8, a storage battery 10 is placed in the battery compartment 9, a binding structure is provided on the medicine box 8 to fix the storage battery 10, the output end of the storage battery 10 is electrically connected with the input end of the main body 1, and the bottom of the medicine box 8 is integrated with a flight control expansion mechanism.
[0032] The battery compartment 9 is integrated inside the medicine box 8 for placing the storage battery 10. This integrated design can effectively utilize space, reduce the complexity of external structure, and facilitate management and maintenance. Through the setting of the binding structure, the storage battery 10 is fixed to ensure that it does not shift or shake during flight, thereby ensuring the stability of power supply.
[0033] The medicine box 8 is designed with anti-surge groove structures at multiple positions, the groove features can effectively hinder the shaking range of the pesticide liquid, make the pesticide liquid surface quickly stabilize, and reduce the influence on the flight of the plant protection unmanned aerial vehicle. Meanwhile, the groove features can also strengthen the structural strength of the medicine box 8 and reduce the deformation of the medicine box 8.
[0034] The bottom of the medicine box 8 is integrated with a flight control expansion mechanism, the integrated design can improve the functionality and adaptability of the unmanned aerial vehicle, so that it can be configured according to different task requirements.
[0035] The binding structure includes a binding belt 11 bolted on the medicine box 8, and the medicine box 8 is formed with a belt passing groove 12 matched with the end of the binding belt 11. The design of the bolt and the belt passing groove 12 makes the binding structure easy to install and disassemble, facilitates the maintenance and replacement of the battery, and the design of the belt passing groove 12 reduces unnecessary weight while ensuring the structural strength, which helps to improve the endurance of the unmanned aerial vehicle, and optimizes the overall structure of the medicine box 8, making it more compact.
[0036] Specifically, as shown in Figure 3 The flight control expansion mechanism includes a front obstacle avoidance radar 13, a ground simulation radar 14, a water pump 15 and a rear obstacle avoidance radar 16 fixed on the bottom of the medicine box 8. The flight control expansion mechanism integrates multiple functional modules on the bottom of the medicine box 8, enhances the autonomous flight capability and operation efficiency of the plant protection unmanned aerial vehicle.
[0037] The front obstacle avoidance radar 13 is used for detecting the front obstacles, providing real-time distance information, helping the unmanned aerial vehicle to avoid obstacles during flight. The ground simulation radar 14 is used for measuring the actual distance between the unmanned aerial vehicle and the ground, ensuring that the unmanned aerial vehicle maintains a stable flight height on different terrains, and improving the uniformity of the spraying operation. The water pump 15 is used for controlling the spraying of pesticides, which can automatically adjust the spraying amount according to the flight speed and height, and improve the operation efficiency. The rear obstacle avoidance radar 16 is used for detecting the rear obstacles, providing real-time distance information, helping the unmanned aerial vehicle to avoid obstacles during flight. Through the front obstacle avoidance radar 13 and the rear obstacle avoidance radar 16, the unmanned aerial vehicle can perceive the surrounding environment in real time, effectively avoid collision, and improve the flight safety.
[0038] The above description of the embodiments enables those skilled in the art to implement or use the present application. Various modifications to these embodiments will be apparent to those skilled in the art, and the general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present application. Therefore, the present application will not be limited to these embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features disclosed herein.
Claims
1. A light-weight and compact structure of plant protection unmanned aerial vehicle, comprising a main body (1) and an arm power assembly (2) mounted on the main body (1), characterized in that, The bottom of the main body (1) is provided with two pairs of foot support braces (3) through fasteners, the bottom of each pair of foot support braces (3) is provided with a support structure, and a load mechanism is arranged between the two pairs of foot support braces (3) through a load fixing piece (5).
2. The light-weight and compact structure of the plant protection unmanned aerial vehicle according to claim 1, characterized in that, The fastener is a foot screw (4), and the foot screw (4) is in threaded connection with the foot support brace (3) penetrating through the main body (1). 3.The unmanned plant-protection aerial vehicle with lightened and simplified structure according to claim 1, wherein The support structure comprises a foot brace (6), and the foot support brace (3) and the foot brace (6) are fixed through a tee fixing piece (7).
4. The light-weight and compact structure of the plant protection unmanned aerial vehicle according to claim 1, characterized in that, The load mechanism is a medicine box (8), a battery compartment (9) is formed in the medicine box (8), a storage battery (10) is arranged in the battery compartment (9), a binding structure for fixing the storage battery (10) is arranged on the medicine box (8), an output end of the storage battery (10) is electrically connected with an input end of the main body (1), and a flight control expansion mechanism is integrated at the bottom of the medicine box (8).
5. The light-weight and compact structure of the plant protection unmanned aerial vehicle according to claim 4, characterized in that, The binding structure comprises a binding belt (11) which is buckled on the medicine box (8), and a belt penetrating groove (12) is formed on the medicine box (8) and is matched with the end of the binding belt (11) penetrating through the binding.
6. The light-weight simplified structure of the plant protection unmanned aerial vehicle according to claim 5, characterized in that, The flight control expansion mechanism comprises a front obstacle avoidance radar (13), a ground simulation radar (14), a water pump (15) and a rear obstacle avoidance radar (16) which are fixed at the bottom of the medicine box (8).