An agricultural drone for spraying

Abstract

The utility model belongs to the technical field of agricultural unmanned plane, concretely is an agricultural unmanned plane that carries out spraying, including unmanned plane body, is hung with the spraying frame subassembly on unmanned plane body, the spraying frame subassembly includes the suspension frame and sets up the spraying pipe on the suspension frame, be equipped with a plurality of spray heads on the spraying pipe, the suspension frame includes the support and the hanger, the support and the hanger are hinged and connect, the hanger can rotate around the support, and the hinged place is connected with the rotary disc, the hanger and the spraying pipe are detachable and connect, the utility model discloses through the suspension frame and the spraying pipe hinged type connection to make the spraying pipe can rotate relative to the suspension frame to change the angle of spraying, adjust according to the angle of spraying required, to reach the multi -angle spraying process.

Description

Technical Field

[0001] This utility model relates to the field of agricultural drone technology, specifically an agricultural drone for spraying. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously by an onboard computer, either completely or intermittently. In agricultural planting, pesticides need to be sprayed on crops. Manual spraying is inefficient, so UAVs are often used to spray pesticides to improve efficiency.

[0003] When using existing spraying agricultural drones, traditional spraying agricultural drones often have multiple nozzles on the drone, but the angle of the nozzles is fixed and cannot be adjusted according to actual needs.

[0004] Therefore, an agricultural drone for spraying was designed based on the above-mentioned technical problems. Utility Model Content

[0005] To address the problem that the angle of the nozzles on existing agricultural spraying drones is fixed and cannot be adjusted according to actual needs, this utility model proposes an agricultural spraying drone.

[0006] The technical solution adopted by this utility model to solve its technical problem is an agricultural drone for spraying, including a drone body, on which a spraying frame assembly is suspended. The spraying frame assembly includes a suspension frame and a spraying pipe mounted on the suspension frame. The spraying pipe is provided with multiple nozzles. The suspension frame includes a bracket and a hanger. The bracket and the hanger are hinged together. The hanger can rotate around the bracket. A rotating disk is connected at the hinge. The hanger and the spraying pipe are detachably connected.

[0007] Working principle: There are generally two types of spraying drones in the existing technology. One type uses a canister to be added directly to the drone to achieve spraying. However, this often results in a short working time due to weight issues. Therefore, the existing technology involves connecting a pipe to the drone for spraying. However, when spraying multiple crops, it is impossible to adjust the spraying angle according to the angle of the crops. Therefore, this application solves the problem by setting up a suspension frame. The spray pipe is placed on the suspension frame and connected to the suspension frame by a hinge. This allows the spray pipe to rotate relative to the suspension frame, thereby changing the angle of the nozzles on the spray pipe.

[0008] Preferably, the drone body has multiple legs at its bottom, and the legs are evenly spaced around the spray frame assembly, which makes landing more stable and protects the safety of the spray frame assembly.

[0009] Preferably, the bracket is a frame structure, the hanging bracket includes two uprights, the two uprights are arranged in parallel, the two uprights are respectively hinged to the frame of the bracket, the rotating disk is connected to a servo motor, the servo motor drives the uprights to rotate along the bracket, and the spray pipe is arranged on the two uprights.

[0010] Preferably, both of the uprights are provided with mounting slots, and the spray pipe is inserted into the mounting slots for easy and quick installation of the spray pipe.

[0011] Preferably, the drone body includes a fuselage and a propeller assembly mounted on the fuselage. The propeller assembly includes multiple flight frames, with a propeller located on the outermost side of each flight frame.

[0012] Preferably, the flight frame is detachably connected to the fuselage, and there are eight flight frames, which makes the flight more stable.

[0013] Preferably, a protective shell is provided at the upper end of the connection between the flight frame and the fuselage. The protective shell is a two-layer disc structure, and the brackets are evenly distributed and inserted in the middle of the protective shell, making the bracket structure more stable.

[0014] Preferably, the frame structure of the bracket includes multiple side strips, which are detachably connected to facilitate the installation and disassembly of the bracket.

[0015] The advantages of this utility model are:

[0016] This invention uses a hinged connection between the suspension frame and the spray pipe, allowing the spray pipe to rotate relative to the suspension frame, thereby changing the spray angle and facilitating adjustment according to the desired spray angle.

[0017] 2. The drone body of this utility model is provided with multiple support legs at the bottom. The support legs are located around the spray frame assembly, which makes the landing more stable and protects the safety of the spray frame assembly.

[0018] 3. Both of the two uprights of this utility model are provided with mounting grooves, and the spray pipe is inserted into the mounting grooves for convenient and quick installation of the spray pipe.

[0019] 4. The upper end of the connection between the flight frame and the fuselage of the present invention is provided with a protective shell. The protective shell is a two-layer disc structure. The brackets are evenly distributed and inserted in the middle of the protective shell, making the bracket structure more stable. Attached Figure Description

[0020] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0021] Figure 1 This is a schematic diagram of the structure of this utility model;

[0022] Figure 2 This is a schematic diagram of the structure of this utility model;

[0023] Figure 3 This is a schematic diagram of the structure of this utility model.

[0024] In the diagram: 1. UAV body; 2. Sprayer frame assembly; 3. Spray pipe; 4. Nozzle; 5. Support legs; 6. Protective shell; 101. Fuselage; 102. Propeller assembly; 103. Flight frame; 104. Propeller; 201. Suspension frame; 202. Bracket; 203. Hanger; 204. Rotary disc; 205. Stand; 206. Mounting slot. Detailed Implementation

[0025] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0026] Please see Figures 1 to 3 As shown, an agricultural drone for spraying includes a drone body 1, on which a spraying frame assembly 2 is suspended. The spraying frame assembly 2 includes a suspension frame 201 and a spray pipe 3 mounted on the suspension frame 201. The spray pipe 3 is provided with multiple nozzles 4. The suspension frame 201 includes a bracket 202 and a hanging frame 203. The bracket 202 and the hanging frame 203 are hinged together. The hanging frame 203 can rotate around the bracket 202. A rotating disk 204 is connected to the hinge. The hanging frame 203 is detachably connected to the spray pipe 3.

[0027] In another embodiment, the bottom of the drone body 1 is provided with multiple legs 5, and the legs 5 are evenly spaced around the spray frame assembly 2. The legs 5 are arranged in a triangle around the spray frame assembly 2, which ensures the stability of landing while reducing its own weight. At the same time, because they are arranged around the spray frame assembly, the landing is more stable and the safety of the spray frame assembly 2 is protected.

[0028] In another embodiment, the support 202 is a frame structure, the hanger 203 includes two uprights 205, which are arranged in parallel and are respectively hinged to the frame of the support 202. The rotating disk 204 is connected to a servo motor, which drives the uprights 205 to rotate along the support 202. The spray pipe 3 is mounted on the two uprights 205. The UAV body 1 is equipped with a PLC controller, which is electrically connected to the remote control board and the servo motor, thereby facilitating convenient operation and changes of the nozzles 4 during flight.

[0029] In another embodiment, both of the uprights 205 are provided with mounting grooves 206. The center shape of the mounting grooves 206 is matched with the shape of the spray pipe 3. The spray pipe 3 is inserted from the side of one mounting groove 206 into the other mounting groove 206, thereby forming a stable mounting groove 206 for the spray pipe 3, which is convenient for installation and removal.

[0030] In another embodiment, the drone body 1 includes a fuselage 101 and a propeller assembly 102 mounted on the fuselage 101. The propeller assembly 102 includes eight flight frames 103. The outermost of each flight frame 103 is equipped with a propeller 104. The flight frames 103 are detachably connected to the fuselage 101 by a threaded connection. This detachable connection makes installation more convenient and facilitates replacement when the propeller 104 or flight frame 103 malfunctions, reducing operating costs. Furthermore, the use of eight flight frames 103 enhances flight stability.

[0031] In another embodiment, a protective shell 6 is provided at the upper end of the connection between the flight frame 103 and the fuselage 101. The protective shell 6 is a two-layer disc structure. The brackets 202 are evenly distributed and inserted in the middle of the protective shell 6, making the structure of the brackets 202 more stable.

[0032] In another embodiment, the frame structure of the bracket 202 includes multiple side strips, which are detachably connected by snap-fit ​​connections, facilitating the installation and removal of the bracket 202.

[0033] Usage: This application uses the suspension frame 201 to set up the spray pipe 3 on the suspension frame 201. The spray pipe 3 and the suspension frame 201 are connected by a hinge and a servo motor is connected to the rotating disk 204. The servo motor is controlled to rotate by the control remote control board, thereby controlling the rotation of the rotating disk 204, so that the spray pipe 3 can rotate relative to the suspension frame 201, thereby changing the angle of the nozzle 4 on the spray pipe 3. At the same time, since most parts of this application are detachable, it is convenient to install and replace parts. When the flight frame 103 has a problem, it can be directly replaced. Moreover, most parts are detachable, which is convenient for storage and transportation.

[0034] In the description of this specification, references to terms such as "an embodiment," "example," "specific example," etc., indicate that a specific feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0035] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model.

Claims

1. An agricultural drone for spraying, comprising a drone body (1), characterized in that: The drone body (1) is equipped with a spray frame assembly (2). The spray frame assembly (2) includes a suspension frame (201) and a spray pipe (3) on the suspension frame (201). The spray pipe (3) is equipped with multiple nozzles (4). The suspension frame (201) includes a bracket (202) and a hanging frame (203). The bracket (202) and the hanging frame (203) are hinged together. The hanging frame (203) can rotate around the bracket (202). A rotating disk (204) is connected at the hinge. The hanging frame (203) is detachably connected to the spray pipe (3).

2. The agricultural drone for spraying according to claim 1, characterized in that: The drone body (1) has multiple legs (5) at its bottom, and the legs (5) are evenly spaced around the spray frame assembly (2).

3. The agricultural drone for spraying according to claim 1, characterized in that: The bracket (202) is a frame structure. The hanging bracket (203) includes two uprights (205). The two uprights (205) are arranged in parallel. The two uprights (205) are respectively hinged to the frame of the bracket (202). The rotating disk (204) is connected to a servo motor. The servo motor can drive the uprights (205) to rotate along the bracket (202). The spray pipe (3) is arranged on the two uprights (205).

4. An agricultural drone for spraying according to claim 3, characterized in that: Both of the uprights (205) are provided with mounting grooves (206), and the spray pipe (3) is inserted into the mounting grooves (206).

5. An agricultural drone for spraying according to claim 1, characterized in that: The unmanned aerial vehicle (UAV) body (1) includes a fuselage (101) and a propeller assembly (102) mounted on the fuselage (101). The propeller assembly (102) includes multiple flight frames (103), and each flight frame (103) has a propeller (104) on its outermost side.

6. An agricultural drone for spraying according to claim 5, characterized in that: The flight frame (103) is detachably connected to the fuselage (101), and there are 8 flight frames (103).

7. An agricultural drone for spraying according to claim 6, characterized in that: The upper end of the connection between the flight frame (103) and the fuselage (101) is provided with a protective shell (6). The protective shell (6) is a two-layer disc structure. The flight frame (103) is evenly distributed and inserted in the middle of the protective shell (6).

8. An agricultural drone for spraying according to claim 3, characterized in that: The frame structure of the bracket (202) includes multiple side strips, which are detachably connected.

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