Unmanned aerial vehicle spraying experiment device

Abstract

The utility model discloses an unmanned aerial vehicle spraying experiment device, relates to the technical field of unmanned aerial vehicle experiment equipment, and mainly aims to provide an unmanned aerial vehicle spraying experiment device capable of simulating and detecting the spraying effect of an unmanned aerial vehicle. According to the main technical scheme, the unmanned aerial vehicle spraying experiment device comprises a ventilation wall component, each single fan component is installed on a connecting frame, each single fan component comprises a shell, a fan body and a honeycomb rectifier, the fan body is arranged at one end of the shell, and the honeycomb rectifier is arranged at the other end of the shell; the support component comprises a support body, a cantilever component and a motor, one end of the cantilever component is mounted on the upper portion of the support body, the other end of the cantilever component is connected with rotor blades of the unmanned aerial vehicle, the motor is mounted on the cantilever component and used for driving the rotor blades to rotate, and the ventilation wall component is arranged on the side face of the support body. The device is mainly used for detecting the plant protection unmanned aerial vehicle.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) experimental equipment technology, and in particular to a UAV spraying experimental device. Background Technology

[0002] In recent years, drones have become an important part of the agricultural industry, which has developed rapidly. Rotary-wing drones are widely used in agricultural plant protection, and they have greatly improved agricultural production efficiency by accurately spraying pesticides and monitoring crop growth.

[0003] As drones are an emerging industry, there are many gaps in drone testing, especially for agricultural drones, where testing equipment is almost non-existent. Existing agricultural drones mainly consist of the drone itself, a pesticide tank, and a nozzle. The drone carries the pesticide tank, and the pesticide solution inside is sprayed downwards through the nozzle to spray crops. However, accurately detecting and judging the impact of different types of drone rotors on the spraying effect, as well as the impact of the drone's flight altitude, flight speed, ambient wind speed, and wind direction on the spraying effect, is a challenge for existing agricultural drones. Utility Model Content

[0004] In view of this, the present invention provides a drone spraying experimental device, the main purpose of which is to provide a drone spraying experimental device that can simulate and detect the spraying effect of drones.

[0005] To achieve the above objectives, this utility model mainly provides the following technical solutions:

[0006] This utility model embodiment provides a drone spraying experimental device, the device comprising:

[0007] A wind wall component, comprising a connecting frame and multiple single fan components, each single fan component being mounted on the connecting frame, each single fan component comprising a housing, a fan body, and a honeycomb rectifier, the fan body being disposed at one end of the housing, and the honeycomb rectifier being disposed at the other end of the housing;

[0008] The support component includes a support body, a cantilever component, and a motor. One end of the cantilever component is mounted on the upper part of the support body, and the other end is connected to the rotor blade of the UAV. The motor is mounted on the cantilever component and is used to drive the rotor blade to rotate. The wind wall component is disposed on the side of the support body.

[0009] Furthermore, the housing includes a first mounting section, a second mounting section, and a shrinking and pressurizing section. The two ends of the shrinking and pressurizing section are respectively connected to the first mounting section and the second mounting section. The fan body is disposed in the first mounting section, and the cellular rectifier is disposed in the second mounting section.

[0010] Furthermore, the shrinking and pressurizing section includes a first connecting housing, a second connecting housing, and an extension housing. The two ends of the first connecting housing are respectively connected to the first mounting section and the extension housing, and the two ends of the second connecting housing are respectively connected to the extension housing and the second mounting section.

[0011] Furthermore, the first connecting housing and the second connecting housing have a square cross-sectional shape at one end and a circular cross-sectional shape at the other end.

[0012] Furthermore, the cantilever component includes a first connecting rod and a second connecting rod. The first connecting rod is detachably connected to the bracket body, and the other end is detachably connected to the second connecting rod. The motor is mounted on the second connecting rod.

[0013] Furthermore, a nozzle is mounted on the lower part of the rotor blade.

[0014] Furthermore, the support body includes a fixed frame and a lifting rod. The fixed frame is placed on the ground and has a sliding track. Both ends of the lifting rod are installed in the sliding track.

[0015] Furthermore, the bracket body also includes a fixing bolt, one end of which passes through the sliding rail and is threaded to the lifting rod.

[0016] This utility model proposes a drone spraying experimental device. The wind wall component provides simulated ambient wind speed and direction for drone flight. The wind wall component includes a connecting frame and multiple single-fan components. Each single-fan component is mounted on the connecting frame and includes a housing, a fan body, and a honeycomb rectifier. The fan body is located at one end of the housing, and the honeycomb rectifier is located at the other end. A support component adjusts the rotor speed and height. The support component includes a support body, a cantilever component, and a motor. One end of the cantilever component is mounted on the upper part of the support body, and the other end is connected to the drone's rotor blades. The motor is mounted on the cantilever component to drive the rotor blades to rotate. The wind wall component is located on the side of the support body. Compared to existing technologies, conventional agricultural drones mainly include a drone body, a pesticide tank, and... The spray nozzle, carried by the drone itself, sprays the pesticide solution downwards onto crops. However, accurately detecting and judging the impact of different types of drone rotors on the spraying effect, as well as the influence of the drone's flight altitude, flight speed, ambient wind speed, and wind direction, is a challenge for existing agricultural drones. In this technical solution, the drone's rotor blades are raised and fixed by a support frame and cantilever components. Simultaneously, the direction and angle of the rotor blades are adjusted according to the angle of the cantilever components, and the motor adjusts the rotor blade speed. A windbreak component is set on the side of the support frame to provide simulated ambient wind speed and direction. Then, the rotor blades and spraying effect are detected by detection equipment, thereby achieving the technical effect of quickly and accurately detecting the spraying effect of the drone's rotor blades in a flight mode simulating a real environment under the action of the windbreak component. Attached Figure Description

[0017] Figure 1 A three-dimensional structural schematic diagram of a drone spraying experimental device provided for an embodiment of this utility model;

[0018] Figure 2 A three-dimensional structural schematic diagram of a windbreak component provided for an embodiment of this utility model;

[0019] Figure 3 A three-dimensional structural schematic diagram of a single fan component provided for an embodiment of this utility model;

[0020] Figure 4 A cross-sectional structural schematic diagram of a single fan component provided for an embodiment of this utility model;

[0021] Figure 5 A three-dimensional structural schematic diagram of a support component provided for an embodiment of this utility model;

[0022] Figure 6A schematic diagram of a rotor blade mounting structure provided for an embodiment of this utility model;

[0023] Figure 7 A schematic diagram of the usage state of another drone spraying experimental device provided in an embodiment of this utility model. Detailed Implementation

[0024] The present invention will now be described in further detail with reference to the accompanying drawings and embodiments.

[0025] like Figures 1 to 7 As shown, this utility model embodiment provides a drone spraying experimental device, which includes:

[0026] The wind wall component 1 includes a connecting frame 11 and multiple single fan components. Each single fan component is mounted on the connecting frame 11. Each single fan component includes a housing 12, a fan body 13, and a honeycomb rectifier 14. The fan body 13 is disposed at one end of the housing 12, and the honeycomb rectifier 14 is disposed at the other end of the housing 12.

[0027] The support component 2 includes a support body, a cantilever component, and a motor 23. One end of the cantilever component is installed on the upper part of the support body, and the other end is connected to the rotor blade 9 of the UAV. The motor 23 is installed on the cantilever component and is used to drive the rotor blade 9 to rotate. The wind wall component 1 is disposed on the side of the support body.

[0028] This utility model proposes a drone spraying experimental device. The wind wall component 1 provides simulated ambient wind speed and direction for drone flight. The wind wall component 1 includes a connecting frame 11 and multiple single-fan components. Each single-fan component is mounted on the connecting frame 11 and includes a housing 12, a fan body 13, and a honeycomb rectifier 14. The fan body 13 is located at one end of the housing 12, and the honeycomb rectifier 14 is located at the other end of the housing 12. The support component 2 adjusts the rotor speed and altitude. The support component 2 includes a support body, a cantilever component, and a motor 23. One end of the cantilever component is mounted on the upper part of the support body, and the other end is connected to the drone's rotor blades 9. The motor 23 is mounted on the cantilever component and drives the rotor blades 9 to rotate. The wind wall component 1 is located on the side of the support body. Compared with existing technologies... Existing agricultural drones mainly consist of the drone body, a pesticide tank, and a nozzle. The drone body carries the pesticide tank, and the pesticide solution inside is sprayed downwards through the nozzle to spray crops. However, accurately detecting and judging the impact of different types of drone rotors on the spraying effect, as well as the impact of the drone's flight altitude, flight speed, ambient wind speed, and wind direction on the spraying effect, is a challenge for existing agricultural drones. In this technical solution, the drone's rotor blades 9 are raised and fixed by the support body and cantilever component. At the same time, the direction and angle of the rotor blades 9 are adjusted according to the angle of the cantilever component, and the motor 23 adjusts the rotation speed of the rotor blades 9. The wind wall component 1 is set on the side of the support component 2 to provide simulated ambient wind speed and direction, thereby achieving the technical effect of quickly and accurately detecting the spraying effect of the drone's rotor blades 9 in a flight mode that simulates a real environment under the action of the wind wall component 1.

[0029] The aforementioned wind wall component 1 serves to provide simulated ambient wind speed and direction for drone flight. The wind wall component 1 includes a connecting frame 11 and multiple individual fan components. Each individual fan component is mounted on the connecting frame 11 and includes a housing 12, a fan body 13, and a honeycomb rectifier 14. The fan body 13 is located at one end of the housing 12, and the honeycomb rectifier 14 is located at the other end of the housing 12. The connecting frame 11 is used to fix the multiple individual fan components. The connecting frame 11 is made of stainless steel and has multiple square holes. The fan components are mounted on a single hole, forming a wind wall from multiple individual fan components. Wheels are installed at the bottom of the connecting frame 11 for easy movement. The square hole has a side length of at least 1 meter. The housing 12 has open ends; the fan body 13 is mounted at one end of the housing 12, and the honeycomb rectifier 14 is mounted at the other end. The fan body 13 rotates to provide airflow. Different blade types can be replaced to adapt to varying wind speeds. Furthermore, the fan body 13 uses frequency conversion and other methods to adjust its speed. The airflow is rectified after passing through the housing 12 and the honeycomb rectifier 14. The rear air output is provided; the function of the support component 2 is to adjust the rotor speed and height. The support component 2 includes a support body, a cantilever component, and a motor 23. One end of the cantilever component is installed on the upper part of the support body, and the other end is connected to the rotor blade 9 of the UAV. The motor 23 is installed on the cantilever component and is used to drive the rotor blade 9 to rotate. The wind wall component 1 is located on the side of the support body and the side of the support component 2. The position and number of wind wall components 1 can be set as needed. The support body is made of stainless steel, and the cantilever component is installed on the upper part of the support body. A motor 23 is mounted on the lower part of the arm component, and the lower part of the motor 23 is connected to the rotor blade 9 for driving the rotor blade 9 to rotate. In this technical solution, the rotor blade 9 of the UAV is raised and fixed by the support body and the cantilever component. At the same time, the direction and angle of the rotor blade 9 are adjusted according to the angle of the cantilever component, and the motor 23 adjusts the rotational speed of the rotor blade 9. The wind wall component 1 is set on the side of the support component 2 to provide simulated environmental wind speed and direction, thereby achieving the technical effect of quickly and accurately detecting the spraying effect of the UAV rotor blade 9 in a flight mode simulating a real environment under the action of the wind wall component 1. Figure 7 As shown, two wind wall components 1 are respectively installed at the rear and side of the support component 2. One wind wall component 1 simulates the flight speed of the drone, and the other wind wall component 1 simulates the ambient wind speed.

[0030] Furthermore, the housing 12 includes a first mounting section 121, a second mounting section 122, and a shrinking and pressurizing section. The two ends of the shrinking and pressurizing section are respectively connected to the first mounting section 121 and the second mounting section 122. The fan body 13 is disposed in the first mounting section 121, and the honeycomb rectifier 14 is disposed in the second mounting section 122. In this embodiment, the housing 12 is further defined. The first mounting section 121 and the second mounting section 122 are square shells. The fan body 13 is installed in the hole of the first mounting section 121, and the honeycomb rectifier 14 is installed in the hole of the second mounting section 122. The two ends of the shrinking and pressurizing section are respectively fixedly connected to the first mounting section 121 and the second mounting section 122. Specifically, the shrinking and pressurizing section includes a first connecting housing 123, a second connecting housing 124, and an extension housing 125. The two ends of the first connecting housing 123 are respectively connected to the first mounting section 121 and the extension housing 125, and the two ends of the second connecting housing 124 are respectively connected to the extension housing 125 and the second mounting section 122. One end of the first connecting housing 123 and the second connecting housing 124 is cut off. The first connecting housing 123 has a square shape on one side and a circular cross-section on the other. The square cross-section of the first connecting housing 123 is connected to the first mounting section 121, and the circular cross-section of the first connecting housing 123 is connected to the extension housing 125. The square cross-section of the second connecting housing 124 is connected to the second mounting section 122, and the circular cross-section of the second connecting housing 124 is connected to the extension housing 125. The extension housing 125 is a cylindrical housing 12 and has a hollow structure. When the fan body 13 blows air, the air passes through the first mounting section 121, the first connecting housing 123, and the extension housing 125, causing the air to be compressed and pressurized. After being rectified by the second connecting housing 124 and the honeycomb rectifier 14, the air is then output to the rotor blade 9, thereby achieving the technical effect of improving the straightness and uniformity of the blown airflow.

[0031] Furthermore, the cantilever component includes a first connecting rod 221 and a second connecting rod 222. The first connecting rod 221 is detachably connected to the bracket body, and the other end is detachably connected to the second connecting rod 222. The motor 23 is mounted on the second connecting rod 222. In this embodiment, the cantilever component is further defined. One end of the first connecting rod 221 is bolted to the bracket body, and the other end is bolted to the side of the second connecting rod 222. The first connecting rod 221 is horizontally arranged, and the second connecting rod 222 is perpendicular to the first connecting rod 221. A motor 23 is installed at the other end of the second connecting rod 222. The output end of the motor 23 is connected to the rotor blade 9 to drive the rotor blade 9 to rotate. Optionally, a connector is provided at the connection position of the first connecting rod 221 and the second connecting rod 222. The connector can adjust the orientation of the second connecting rod 222, thereby achieving the technical effect of adjusting the angle of the rotor blade 9. Optionally, a nozzle 3 is added. The function of the nozzle 3 is to simulate the working state of the plant protection drone during spraying operations. The nozzle 3 is installed on the lower part of the rotor blade 9, and a liquid pipe is connected to the nozzle 3. The nozzle 3 can spray liquid, thereby achieving the technical effect of conveniently simulating the flight and spraying effect in a real environment.

[0032] Furthermore, the support body includes a fixed frame 211 and a lifting rod 212. The fixed frame 211 is placed on the ground and has a sliding rail 213. Both ends of the lifting rod 212 are installed in the sliding rail 213. In this embodiment, the support body is further defined. The fixed frame 211 is placed on the ground, and the lower part of the fixed frame 211 is provided with wheels. The sliding rail 213 is provided in the middle position of the fixed frame 211. Both ends of the lifting rod 212 are inserted into the sliding rail 213. The lifting rod 212 is located in the middle position of the support body. The support body also includes a fixing bolt. One end of the fixing bolt passes through the sliding rail 213 and is threaded to the lifting rod 212. When the lifting rod 212 moves to a set position, the fixing bolt is rotated, and the fixing bolt moves towards the position of the sliding rail 213, fixing the lifting rod 212 in the set position of the sliding rail 213, thereby achieving the technical effect of conveniently fixing the lifting rod 212. Optionally, such as... Figure 6 As shown, the fixed frame 211 is provided with multiple sliding rails 213 and lifting rods 212. The sliding rails 213 are arranged along the extension direction of the fixed rods on the fixed frame 211, thereby achieving the technical effect of facilitating the installation of cantilever components. Specifically, the fixed frame 211 is composed of multiple fixed rods, and each fixed rod has a sliding rail 213 on its surface. Multiple cantilever components can be installed on the sliding rails 213 as needed.

[0033] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this utility model should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the protection scope of the claims.

Claims

1. A drone spraying experimental device, characterized in that, include: A wind wall component, comprising a connecting frame and multiple single fan components, each single fan component being mounted on the connecting frame, each single fan component comprising a housing, a fan body, and a honeycomb rectifier, the fan body being disposed at one end of the housing, and the honeycomb rectifier being disposed at the other end of the housing; The support component includes a support body, a cantilever component, and a motor. One end of the cantilever component is mounted on the upper part of the support body, and the other end is connected to the rotor blade of the UAV. The motor is mounted on the cantilever component and is used to drive the rotor blade to rotate. The wind wall component is disposed on the side of the support body.

2. The drone spraying experimental device according to claim 1, characterized in that, The housing includes a first mounting section, a second mounting section, and a shrinking and pressurizing section. The two ends of the shrinking and pressurizing section are respectively connected to the first mounting section and the second mounting section. The fan body is disposed in the first mounting section, and the cellular rectifier is disposed in the second mounting section.

3. The drone spraying experimental device according to claim 2, characterized in that, The shrinking and pressurizing section includes a first connecting housing, a second connecting housing, and an extension housing. The two ends of the first connecting housing are respectively connected to the first mounting section and the extension housing, and the two ends of the second connecting housing are respectively connected to the extension housing and the second mounting section.

4. The drone spraying experimental device according to claim 3, characterized in that, The first connecting shell and the second connecting shell have a square cross-section at one end and a circular cross-section at the other end.

5. A drone spraying experimental apparatus according to any one of claims 1 to 4, characterized in that, The cantilever component includes a first connecting rod and a second connecting rod. The first connecting rod is detachably connected to the bracket body, and the other end is detachably connected to the second connecting rod. The motor is mounted on the second connecting rod.

6. The drone spraying experimental device according to claim 5, characterized in that, Also includes: The nozzle is mounted on the lower part of the rotor blade.

7. The drone spraying experimental device according to claim 5, characterized in that, The support body includes a fixed frame and a lifting rod. The fixed frame is placed on the ground and has a sliding track. The two ends of the lifting rod are installed in the sliding track.

8. The drone spraying experimental device according to claim 7, characterized in that, The bracket body also includes a fixing bolt, one end of which passes through the sliding rail and is threaded to the lifting rod.

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