A high-altitude UAV spraying efficiency enhancement device and UAV

By using culverts, wind masks, and air ducts in the drone spraying device, combined with collecting components and adaptive nozzles to solve the problem of waste of coatings in the drone high -air spray operation, it has achieved efficient, accurate and accurate Spray effect.

CN119018350BActive Publication Date: 2025-01-28山西观复智能科技有限公司

Patent Information

Application Number
CN202411526804.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-10-30
Publication Date
2025-01-28
Estimated Expiration
2044-10-30

AI Technical Summary

Technical Problem

During the high-altitude spraying operation, the spray paint is blown away due to the wind field interference caused by the rotation of the paddle, causing a lot of waste.

Method used

Designed a high -altitude drone spraying efficiency device, including culverts, wind masks, and air ducts. By generating the wind curtain to offset the wind farm interference generated by the drone itself, it is equipped with collecting components and adaptive nozzles to improve spray coating Efficiency and coating utilization.

Benefits of technology

Effectively prevent the impact of the wind farm generated by the drone on the coating sprayed by the nozzle, reduce the waste of paint, improve the spray coating efficiency and coating utilization rate, and achieve precise control of the spray trajectory and coating distribution.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to a high-altitude UAV spraying efficiency enhancement device and a UAV, and relates to the technical field of unmanned spraying devices, which include a fuselage, a spraying assembly, a collecting assembly and an offset assembly. The fuselage is provided with a plurality of blades, which are evenly arranged around the vertical axis direction of the fuselage, and the blades are rotatably connected to the top of the fuselage; the spraying assembly is provided on the fuselage and used for spraying paint; the collecting assembly is provided on the spraying assembly and used for collecting the paint dripping during spraying; the offset assembly is provided on the fuselage and located above the spraying assembly, and the offset assembly is used to generate a wind curtain to resist the wind field interference caused by the rotation of the UAV's own blades. The present application has the effect of improving the utilization rate of sprayed paint.
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Description

Technical Field

[0001] The present application relates to the technical field of unmanned spraying devices, and in particular to a high-altitude UAV spraying efficiency enhancement device and a UAV. Background Art

[0002] In the fields of building exterior wall repair, large-scale facility maintenance, etc., the demand for using drones for high-altitude spraying operations has gradually become prominent. This efficient and safe method has brought revolutionary changes to traditional manual or hanging basket spraying.

[0003] At present, the general spraying device is to use a drone to drive an automatic spray gun to move to the construction site, and then start the automatic spray gun, which sprays the paint on the construction site, thereby easily improving the spraying efficiency.

[0004] However, because the rotation of the drone's own blades generates a large wind field, the automatic spray gun is affected by the wind force when it is opened for spraying operations, and the sprayed paint will be blown away by the wind generated by the drone itself, resulting in a large amount of waste of spray paint. Summary of the invention

[0005] In order to improve the utilization rate of spray paint, the present application provides a high-altitude UAV spray efficiency enhancement device and a UAV.

[0006] On the one hand, the present application provides a high-altitude drone spraying efficiency enhancement device, which adopts the following technical solution:

[0007] A high-altitude unmanned aerial vehicle spraying efficiency enhancement device, comprising:

[0008] A fuselage, wherein a plurality of propeller blades are arranged uniformly around a vertical axis of the fuselage, and the propeller blades are rotatably connected to the top of the fuselage;

[0009] A spraying assembly, arranged on the fuselage and used for spraying paint;

[0010] A collecting component is arranged on the spraying component and is used to collect the paint dripping during spraying;

[0011] Offsetting components, including:

[0012] A ducted fan, wherein the ducted fan is fixedly connected to the fuselage;

[0013] A wind shield, the wind shield is fixedly connected to the fuselage and is located on the spray assembly, one end of the wind shield is open, and the open end is arranged toward the flight direction of the fuselage; wherein the wind shield is used to generate a wind curtain to resist the wind field interference generated by the rotation of the UAV's own blades;

[0014] An air duct pipe, two ends of which are respectively connected to the duct fan and the wind hood.

[0015] By adopting the above technical solution, when the fuselage moves to the designated position, the duct fan supplies air to the wind hood through the duct pipe, and the wind hood blows air above the spray assembly to produce a wind curtain, which counteracts the wind field generated by the drone itself. Then, the spray assembly sprays the designated position, thereby effectively preventing the wind field generated by the drone from affecting the paint sprayed from the nozzle. During the spraying process, the collecting assembly collects the paint dripping during spraying to prevent paint waste, thereby improving the spraying efficiency and paint utilization rate.

[0016] Optionally, the opening end of the wind shield is duckbill-shaped, and the width direction of the wind shield is arranged parallel to the plane where the blades are located.

[0017] By adopting the above technical solution, the duckbill-shaped narrowing design can enhance the concentration and speed of the airflow, forming a more stable and powerful wind curtain, which can more effectively resist the wind field interference caused by the rotation of the drone blades. This directional wind curtain helps to maintain stable air flow in the spraying operation area, thereby easily reducing the impact of airflow turbulence on the spraying effect, and thus easily improving the spraying efficiency.

[0018] Optionally, the spraying assembly includes:

[0019] A nozzle, the nozzle is fixedly connected to the fuselage and is located below the wind shield;

[0020] An automatic spray gun, the automatic spray gun is fixedly connected to the fuselage, and the input end of the automatic spray gun is connected to an external storage tank;

[0021] A spray pipe, wherein the spray pipe is fixedly connected to the fuselage, and two ends of the spray pipe are respectively connected to the input end of the nozzle and the output end of the automatic spray gun.

[0022] By adopting the above technical solution, paint is supplied to the automatic spray gun through an external storage tank, and the automatic spray gun transports the paint to the nozzle through the spray pipe. Under the action of pressure, the paint is sprayed from the nozzle. By combining the precise position setting of the nozzle and the precise control of the automatic spray gun, precise control of the spraying trajectory and paint distribution is achieved, thereby reducing deviations and waste in the spraying process, and further improving the uniformity and consistency of the coating.

[0023] Optionally, the collection component includes:

[0024] The collecting box has an open top and a baffle fixedly connected to the open end, the baffle and the collecting box form a feed inlet, the collecting box is connected to a discharge pipe, and the discharge pipe is provided with a valve;

[0025] A wetting portion, disposed on the collection box and used to increase the humidity of the paint in the collection box;

[0026] The stirring part is arranged in the collecting box and is used for stirring the coating.

[0027] By adopting the above technical scheme, during the spraying process, part of the paint accumulates at the nozzle mouth, and the paint drips into the collection box through the feed port. Due to the strong wind at high altitude, the small amount of paint in the collection box is easy to dry up, and the infiltration part increases the humidity of the paint in the collection box to prevent the paint from drying up. After accumulating for a period of time, the stirring part stirs the paint in the collection box. The appropriate humidity and uniform mixing state help to extend the shelf life of the paint and reduce the failure of the paint due to drying, agglomeration, etc., so that it is easy to recycle the paint, thereby improving the utilization rate of the paint.

[0028] Optionally, the wetting portion includes:

[0029] An infrared sensor is fixedly connected to the side wall of the collection box and is located at the feed inlet of the collection box;

[0030] A controller, fixedly connected to the collection box and electrically connected to the infrared sensor;

[0031] A spray nozzle, fixedly connected to the baffle plate and located at the feed inlet of the collection box;

[0032] A water tank, fixedly connected to the collection tank and connected to the spray nozzle via a connecting pipe;

[0033] The water pump is connected in series to the connecting pipe and is electrically connected to the controller, and the controller is used to control the start and stop of the water pump.

[0034] By adopting the above technical solution, when the paint passes through the feed port, the infrared sensor outputs a displacement signal between the inner wall of the collection box and the baffle to the controller. The controller responds to the displacement signal output by the infrared sensor and controls the water pump to start. The water pump draws water from the water tank and transports it to the spray nozzle through the connecting pipe. The spray nozzle sprays water mist onto the inner wall of the collection box. The water flow flushes the inner wall of the collection box, which can prevent the paint from drying on the inner wall of the collection box. By timely increasing the humidity of the paint, the waste of paint caused by drying is reduced, making it easy to recycle the paint, thereby improving the utilization rate of the paint.

[0035] Optionally, the stirring unit includes:

[0036] The guide plate is arc-shaped, and one end of the guide plate is fixedly connected to the inner wall of the collecting box near the feed inlet;

[0037] A rotating plate, which is L-shaped and rotatably connected to the inner wall of the collection box, wherein the curved end of the rotating plate is located between the guide plate and the inner wall of the collection box;

[0038] A spring, one end of which is fixedly connected to the inner wall of the collection box, and the other end of which is fixedly connected to the rotating plate, wherein the spring is in a stretched state in an initial state;

[0039] A first induction block, fixedly connected to the curved end of the rotating plate;

[0040] A second induction block is fixedly connected to the guide plate and electrically connected to the controller, wherein when the compression amount of the spring is at a limit value, the first induction block abuts against the second induction block;

[0041] A motor, fixedly connected to the baffle and electrically connected to the controller;

[0042] The stirring rod is coaxially fixedly connected to the output shaft of the motor and is located in the collecting box.

[0043] By adopting the above technical solution, the paint drips onto the inner wall of the collection box through the feed port, flows along the inner wall of the collection box, flows through the guide plate and enters the rotating plate. When the paint accumulates to a set amount, the spring is squeezed, the compression amount of the spring increases, the spring accumulates elastic force, the rotating plate rotates, and the paint is poured to the bottom of the collection box;

[0044] When the rotating plate rotates, the sensing block 1 abuts against the sensing block 2, and the sensing block 2 outputs a sensing signal to the controller. The controller controls the output shaft of the motor to rotate, and the output shaft of the motor drives the stirring rod to rotate. The stirring rod stirs the paint, which can prevent the paint from static stratification, thereby improving the mixing efficiency.

[0045] Optionally, the nozzle is an adaptive nozzle.

[0046] By adopting the above technical solution, the adaptive nozzle can monitor and adjust the spraying parameters in real time through the built-in intelligent control system, and can accurately control the spraying amount of paint, avoiding waste and excessive use of paint, thereby helping to reduce the cost of spraying operations and easily reducing the impact on the environment.

[0047] Optionally, a fixing clamp is fixedly installed between the air duct pipe and the spray pipe.

[0048] By adopting the above technical solution, a stable connection between the air duct pipe and the spray pipe is ensured, thereby easily preventing the pipe from loosening or falling off due to vibration or external force impact during flight, thereby improving the stability of the device.

[0049] Optionally, threads are provided at both ends of the spray pipe, and the two ends of the spray pipe are threadedly connected to the input end of the nozzle and the output end of the automatic spray gun respectively through the threads.

[0050] By adopting the above technical solution, the threaded connection design makes the installation and disassembly process simple and quick. The operator can quickly connect the nozzle and automatic spray gun to the spray pipe, or replace and repair them as needed, thereby improving work efficiency.

[0051] On the other hand, the present application provides a drone, comprising the above-mentioned high-altitude drone spraying efficiency enhancement device.

[0052] By adopting the above technical solutions, the UAV can cover a large area in a short time due to its high-altitude flight capability and the optimization of the spraying efficiency enhancement device, thereby significantly improving the efficiency of the spraying operation.

[0053] In summary, the present application includes at least one of the following beneficial technical effects:

[0054] By setting up ducted fans, wind hoods and air ducts, the wind curtain counteracts the wind field generated by the drone itself, thereby effectively preventing the wind field generated by the drone from affecting the paint sprayed from the nozzle, thereby improving the spraying efficiency and paint utilization rate;

[0055] By setting the nozzle, automatic spray gun wind cover and spray pipe, the precise position setting of the nozzle and the precise control of the automatic spray gun are combined to achieve precise control of the spray trajectory and paint distribution, thereby reducing the deviation and waste in the spraying process, and thus improving the uniformity of the coating;

[0056] By providing a collecting box, a wetting part and a stirring part, it is easy to recycle the paint dripping during spraying, thereby improving the paint utilization rate. BRIEF DESCRIPTION OF THE DRAWINGS

[0057] Figure 1 It is a schematic diagram of the structure of an embodiment of the present application;

[0058] Figure 2 It is a schematic diagram of the partial structure of the spraying assembly in the embodiment of the present application;

[0059] Figure 3 is a cross-sectional view of a collection assembly in an embodiment of the present application;

[0060] Figure 4 yes Figure 3 Magnified view at A in the middle.

[0061] Description of reference numerals:

[0062] 1. Body; 11. Blade; 2. Offset assembly; 21. Ducted fan; 22. Wind hood; 23. Duct pipe; 231. Fixing clamp; 3. Spray assembly; 31. Nozzle; 32. Automatic spray gun; 33. Spray pipe; 4. Collecting assembly; 41. Collecting box; 411. Baffle; 412. Discharge pipe; 42. Wetting part; 421. Infrared sensor; 422. Controller; 423. Spray nozzle; 424. Water tank; 425. Water pump; 43. Stirring part; 431. Guide plate; 432. Rotating plate; 433. Spring; 434. Sensor block 1; 435. Sensor block 2; 436. Motor; 437. Stirring rod; 438. Stirring rod. DETAILED DESCRIPTION

[0063] The following is combined with Figure 1-4 This application is described in further detail.

[0064] The present application embodiment discloses a high-altitude drone spraying efficiency enhancement device. Figure 1 and Figure 2 A high-altitude UAV spraying efficiency enhancement device includes a fuselage 1, an offset component 2, a spraying component 3 and a collecting component 4. The fuselage 1 is provided with a plurality of blades 11, and the plurality of blades 11 are evenly arranged around the vertical axis direction of the fuselage 1, and the blades 11 are rotatably connected to the top of the fuselage 1; the offset component 2 is provided on the fuselage 1, and is used to generate a wind curtain to resist the wind field interference generated by the rotation of the UAV's own blades 11; the spraying component 3 is provided on the fuselage 1, and is located below the offset component 2, and the spraying component 3 is used to spray paint; the collecting component 4 is provided on the spraying component 3, and is used to collect the paint dripping during spraying.

[0065] When in use, the drone is started, the blades 11 rotate to generate lift, thereby driving the fuselage 1 to rise, and the fuselage 1 is controlled to move to a specified position through the control platform, and then the offset component 2 is started, the offset component 2 generates a wind curtain to resist the wind field interference caused by the rotation of the drone's own blades 11. Under the action of the offset component 2, the spraying component 3 sprays paint on the specified position. During the spraying process, the collecting component 4 collects the paint dripping during the spraying, thereby effectively preventing the wind field generated by the drone from affecting the paint sprayed from the nozzle 31, thereby improving the spraying efficiency and paint utilization rate.

[0066] Reference Figure 1 The compensation assembly 2 includes a ducted fan 21, a wind cover 22 and an air duct pipe 23. The ducted fan 21 is fixedly connected to the fuselage 1. One end of the wind cover 22 is open, and the open end is duckbill-shaped. The width direction of the wind cover 22 is parallel to the plane where the blades 11 are located.

[0067] Reference Figure 1The wind shield 22 is fixedly connected to the fuselage 1 and is located on the side of the fuselage 1 away from the ducted fan 21. The opening end of the wind shield 22 is arranged toward the flight direction of the fuselage 1. The wind shield 22 is used to generate a wind curtain to resist the wind field interference caused by the rotation of the UAV's own blades 11. The plane where the ducted fan 21 and the wind shield 22 are located is arranged parallel to the plane where the blades 11 are located.

[0068] Reference Figure 1 The two ends of the air duct pipe 23 are respectively connected to the duct fan 21 and the wind cover 22, and the air duct pipe 23, the duct fan 21 and the wind cover 22 are coaxially arranged.

[0069] During use, when the fuselage 1 moves to the specified position, the ducted fan 21 is started, the ducted fan 21 inhales air, and the air enters the wind hood 22 along the air duct pipe 23. The wind hood 22 blows air above the spray assembly 3 to produce a wind curtain. The wind curtain counteracts and offsets the wind field generated by the drone itself, thereby effectively preventing the wind field generated by the drone from affecting the paint sprayed from the nozzle 31, thereby improving the spraying efficiency and paint utilization rate.

[0070] Reference Figure 1 The spray assembly 3 includes a nozzle 31, an automatic spray gun 32 and a spray pipe 33. The nozzle 31 is fixedly connected to the fuselage 1 and is located below the wind hood 22. In the embodiment of the present application, the nozzle 31 is an adaptive nozzle.

[0071] Reference Figure 1 The automatic spray gun 32 is fixedly connected to the fuselage 1 and is located on the side of the fuselage 1 away from the nozzle 31. The input end of the automatic spray gun 32 is connected to the external storage tank. An automatic valve is provided in the automatic spray gun 32, and the automatic valve automatically opens and closes according to the pressure in the automatic spray gun 32.

[0072] Reference Figure 1 The spray pipe 33 is fixedly connected to the fuselage 1, and threads are arranged at both ends of the spray pipe 33, and the two ends of the spray pipe 33 are respectively threadedly connected with the input end of the nozzle 31 and the output end of the automatic spray gun 32 through threads. A fixing clamp 231 is fixedly installed between the air duct 23 and the spray pipe 33, and the fixing clamp 231 is located on the side close to the nozzle 31.

[0073] When in use, the adaptive nozzle and the automatic spray gun 32 are connected to the spray pipe 33, and the paint is supplied to the automatic spray gun 32 through an external storage tank. The automatic valve automatically opens according to the pressure in the automatic spray gun 32, and the paint is transported from the spray pipe 33 to the adaptive nozzle. Through the built-in intelligent control system, the adaptive nozzle monitors and adjusts the spray parameters in real time, accurately controls the spray amount of the paint, and realizes precise control of the spray trajectory and paint distribution, thereby reducing deviations and waste in the spraying process, and thus improving the spraying efficiency and paint utilization.

[0074] Reference Figures 2 to 4 The collecting assembly 4 includes a collecting box 41, an infiltration portion 42 and a stirring portion 43. The collecting box 41 is in a rectangular box shape, and a side wall in the length direction is inclined. The cross-section of the collecting box 41 in the vertical direction is a right-angled trapezoid.

[0075] Reference Figure 2 and Figure 3 The collecting box 41 is installed on the spraying pipe 33 and is located below the nozzle 31. The top of the collecting box 41 is open, and a baffle 411 is fixedly connected to the open end. The baffle 411 is in a rectangular plate shape, and the baffle 411 and the collecting box 41 form a feed inlet. The bottom of the collecting box 41 is connected to a discharge pipe 412, and the discharge pipe 412 is provided with a valve.

[0076] Reference Figure 3 The infiltration part 42 includes an infrared sensor 421, a controller 422, a spray nozzle 423, a water tank 424 and a water pump 425. The infrared sensor 421 is fixedly connected to the side wall of the collection box 41 and is located near the feed port of the collection box 41. The infrared sensor 421 is arranged opposite to the baffle 411.

[0077] Reference Figure 3 The spray nozzle 423 is fixedly connected to the baffle 411 and is located at the feed port of the collection box 41. The spray nozzle 423 is perpendicular to the side wall of the inclined collection box 41. The water tank 424 is fixedly connected to the collection box 41 and is located at one end away from the inclined side of the collection box 41. It is connected to the spray nozzle 423 through a connecting pipe. The water pump 425 is connected in series to the connecting pipe and is electrically connected to the controller 422. The controller 422 is used to control the start and stop of the water pump 425.

[0078] Reference Figure 3 and Figure 4 The stirring part 43 includes a guide plate 431, a rotating plate 432, a spring 433, an induction block 1 434, an induction block 2 435, a motor 436 and a stirring rod 437. The guide plate 431 is arc-shaped, and one end is fixedly connected to the inner wall of the collecting box 41 near the feed inlet. The guide plate 431 and the inner wall of the collecting box 41 form a groove-shaped space, and the open end is arranged toward the bottom of the collecting box 41.

[0079] Reference Figure 3 and Figure 4 The rotating plate 432 is L-shaped and is rotatably connected to the inner wall of the collecting box 41. The bent end of the rotating plate 432 is located in the groove-shaped space formed by the guide plate 431 and the inner wall of the collecting box 41. One end of the spring 433 is fixedly connected to the inner wall of the collecting box 41, and the other end is fixedly connected to the rotating plate 432. In the initial state, the spring 433 is in a stretched state.

[0080] Reference Figure 3 and Figure 4The sensing block 1 434 is fixedly connected to the curved end of the rotating plate 432, and the sensing block 2 435 is fixedly connected to the guide plate 431 and electrically connected to the controller 422, wherein when the compression amount of the spring 433 is at the limit value, the sensing block 1 434 abuts against the sensing block 2 435.

[0081] Reference Figure 3 and Figure 4 The motor 436 is fixedly connected to the baffle 411 and electrically connected to the controller 422. The stirring rod 437 is vertically arranged, and the stirring rod 437 is coaxially fixedly connected to the output shaft of the motor 436 and is located in the collection box 41. A plurality of auxiliary stirring rods 438 are fixedly connected to one end of the stirring rod 437 away from the motor 436, and the plurality of auxiliary stirring rods 438 are evenly arranged around the axis direction of the stirring rod 437.

[0082] When in use, during the spraying process, part of the paint accumulates at the nozzle 31, and the paint drips from the feed port to the inner wall of the collection box 41. The infrared sensor 421 detects the dripping of the paint, and the infrared sensor 421 outputs a displacement signal between the inner wall of the collection box 41 and the baffle 411 to the controller 422. The controller 422 responds to the displacement signal output by the infrared sensor 421 and controls the water pump 425 to start. The water pump 425 extracts water from the water tank 424 and transports it to the spray nozzle 423 through the connecting pipe. The spray nozzle 423 sprays water mist onto the inner wall of the collection box 41. The water flow washes the inner wall of the collection box 41, which can prevent the paint from drying on the inner wall of the collection box 41.

[0083] The water flow is mixed with the paint and flows along the guide plate 431 into the rotating plate 432. When the water accumulates to a set amount, the spring 433 is squeezed, the rotating plate 432 rotates, and the paint is poured to the bottom of the collection box 41. Under the elastic force of the spring 433, the rotating plate 432 is reset.

[0084] When the rotating plate 432 rotates, the sensing block 1 434 abuts against the sensing block 2 435, and the sensing block 2 435 outputs a sensing signal to the controller 422. The controller 422 controls the output shaft of the motor 436 to rotate. The output shaft of the motor 436 drives the stirring rod 437 to rotate, and drives the auxiliary stirring rod 438 to rotate, so as to stir the paint, thereby preventing the paint from being statically stratified, thereby improving the mixing efficiency and mixing quality.

[0085] The implementation principle of the high-altitude UAV spraying efficiency enhancement device of the embodiment of the present application is as follows: when the fuselage 1 moves to the specified position, the ducted fan 21 is started, the ducted fan 21 inhales air, and the air enters the wind hood 22 along the air duct pipe 23, and the wind hood 22 blows air above the spraying assembly 3 to generate a wind curtain, and the wind curtain counteracts and offsets the wind field generated by the UAV itself, thereby effectively preventing the wind field generated by the UAV from affecting the paint sprayed from the nozzle 31;

[0086] Then, the paint is supplied to the automatic spray gun 32 through an external storage tank, and the automatic valve automatically opens according to the pressure in the automatic spray gun 32, and the paint is transported from the spray pipe 33 to the adaptive nozzle. Through the built-in intelligent control system, the adaptive nozzle monitors and adjusts the spraying parameters in real time, accurately controls the spraying amount of the paint, and realizes accurate control of the spraying trajectory and paint distribution, thereby reducing deviation and waste in the spraying process;

[0087] During the spraying process, part of the paint accumulates at the nozzle 31, and the paint drips from the feed port to the inner wall of the collection box 41. The wetting part 42 detects whether the paint drips, and when the paint drips on the inner wall of the collection box 41, the wetting part 42 rinses the inner wall of the collection box 41 to prevent the paint from drying on the inner wall of the collection box 41;

[0088] When the set amount is accumulated, the mixture of water and paint is poured to the bottom of the collection box 41, and the stirring part 43 stirs the paint to prevent the paint from being statically stratified, thereby improving the mixing efficiency and mixing quality, and further improving the spraying efficiency and paint utilization rate.

[0089] An embodiment of the present application also discloses a UAV, including a high-altitude UAV spraying efficiency enhancement device. The effects of the above-mentioned high-altitude UAV spraying efficiency enhancement device are also possessed by a UAV having the above-mentioned turbine disc high-altitude UAV spraying efficiency enhancement device, so they will not be repeated herein.

[0090] The above are all preferred embodiments of the present application, and the protection scope of the present application is not limited thereto. Therefore, any equivalent changes made according to the structure, shape, and principle of the present application should be included in the protection scope of the present application.

Claims

1. A high-altitude UAV spraying efficiency enhancement device, characterized in that: include: A fuselage (1), wherein a plurality of propeller blades (11) are arranged on the fuselage (1), the plurality of propeller blades (11) are evenly arranged around a vertical axis of the fuselage (1), and the propeller blades (11) are rotatably connected to the top end of the fuselage (1); A spraying assembly (3), arranged on the body (1) and used for spraying paint; A collecting component (4) is arranged on the spraying component (3) and is used to collect paint dripping during spraying; Offsetting components (2), including: A ducted fan (21), the ducted fan (21) being fixedly connected to the fuselage (1); A wind shield (22), the wind shield (22) being fixedly connected to the fuselage (1) and being located on the spray assembly (3), one end of the wind shield (22) being open, and the open end being arranged toward the flight direction of the fuselage (1); wherein the wind shield (22) is used to generate a wind curtain to resist wind field interference generated by the rotation of the propeller blades (11) of the drone itself; An air duct pipe (23), two ends of the air duct pipe (23) being respectively connected to the duct fan (21) and the air hood (22); The collecting component (4) comprises: The collecting box (41) has an open top, and a baffle (411) is fixedly connected to the open end, the baffle (411) and the collecting box (41) form a feed inlet, the collecting box (41) is connected to a discharge pipe (412), and the discharge pipe (412) is provided with a valve; A wetting portion (42) is disposed on the collection box (41) and is used to increase the humidity of the paint in the collection box (41); A stirring portion (43) is disposed in the collecting box (41) and is used to stir the coating; The infiltration portion (42) comprises: An infrared sensor (421) is fixedly connected to a side wall of the collection box (41) and is located at a feed inlet of the collection box (41); A controller (422) fixedly connected to the collection box (41) and electrically connected to the infrared sensor (421); A spray nozzle (423) fixedly connected to the baffle (411) and located at the feed inlet of the collection box (41); A water tank (424) is fixedly connected to the collection tank (41) and is in communication with the spray nozzle (423) via a connecting pipe; A water pump (425) is connected in series to the connecting pipe and is electrically connected to the controller (422), wherein the controller (422) is used to control the start and stop of the water pump (425); The stirring part (43) comprises: The guide plate (431) is arc-shaped, and one end of the guide plate is fixedly connected to the inner wall of the collection box (41) near the feed inlet; A rotating plate (432) is L-shaped and is rotatably connected to the inner wall of the collection box (41); the curved end of the rotating plate (432) is located between the guide plate (431) and the inner wall of the collection box (41); A spring (433), one end of which is fixedly connected to the inner wall of the collection box (41), and the other end of which is fixedly connected to the rotating plate (432); in an initial state, the spring (433) is in a stretched state; A first induction block (434) fixedly connected to the curved end of the rotating plate (432); A second induction block (435) is fixedly connected to the guide plate (431) and electrically connected to the controller (422), wherein when the compression amount of the spring (433) is at a limit value, the first induction block (434) abuts against the second induction block (435); a motor (436) fixedly connected to the baffle (411) and electrically connected to the controller (422); The stirring rod (437) is coaxially fixedly connected to the output shaft of the motor (436) and is located in the collection box (41).

2. The high-altitude UAV spraying efficiency enhancement device according to claim 1 is characterized in that: The opening end of the wind shield (22) is in a duckbill shape, and the width direction of the wind shield (22) is arranged parallel to the plane where the blade (11) is located.

3. The high-altitude UAV spraying efficiency enhancement device according to claim 1 is characterized in that: The spraying assembly (3) comprises: A nozzle (31), the nozzle (31) being fixedly connected to the fuselage (1) and located below the wind shield (22); An automatic spray gun (32), the automatic spray gun (32) being fixedly connected to the fuselage (1), and an input end of the automatic spray gun (32) being connected to an external storage tank; A spray pipe (33), the spray pipe (33) being fixedly connected to the fuselage (1), and two ends of the spray pipe (33) being respectively connected to an input end of the nozzle (31) and an output end of the automatic spray gun (32).

4. The high-altitude UAV spraying efficiency enhancement device according to claim 3 is characterized in that: The nozzle (31) is an adaptive nozzle.

5. The high-altitude UAV spraying efficiency enhancement device according to claim 3 is characterized in that: A fixing clamp (231) is fixedly installed between the air duct pipe (23) and the spray pipe (33).

6. The high-altitude UAV spraying efficiency enhancement device according to claim 3 is characterized in that: Both ends of the spray pipe (33) are provided with threads, and the two ends of the spray pipe (33) are respectively threadedly connected to the input end of the nozzle (31) and the output end of the automatic spray gun (32) through the threads.

7. A drone, characterized in that: It comprises a high-altitude unmanned aerial vehicle spraying efficiency enhancement device as described in any one of claims 1-6.

Citation Information

Patent Citations

  • Unmanned Aerial Vehicle Equipped with Injection Nozzle and Method for Repairing Concrete Structure

    JP6403174B1

  • Air curtain-type spray drift prevention apparatus and method for plant protection unmanned aerial vehicle

    WO2021109455A1

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