CN212401568U - Vertical take-off and landing fixed wing unmanned aerial vehicle - Google Patents

Vertical take-off and landing fixed wing unmanned aerial vehicle Download PDF

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Publication number
CN212401568U
CN212401568U CN202021120247.4U CN202021120247U CN212401568U CN 212401568 U CN212401568 U CN 212401568U CN 202021120247 U CN202021120247 U CN 202021120247U CN 212401568 U CN212401568 U CN 212401568U
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unmanned aerial
aerial vehicle
fixed
water tank
vehicle main
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刘华琦
刘鲁琦
何坤洲
陈燕
刘华杰
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Xi'an Sanhang Industrial Co ltd
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Xi'an Sanhang Industrial Co ltd
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a vertical take-off and landing fixed wing unmanned aerial vehicle, which improves the spraying adaptability, increases the operability and reduces the use limitation; the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a storage battery, a control chip, a propeller, an empennage, supporting legs and a water tank, wherein the storage battery and the control chip are fixedly installed inside a protective box of the unmanned aerial vehicle main body; still include the water tank, add the pipe, the case lid, a water pump, the connecting piece, the pipe and the shower nozzle of scattering all, the water tank bottom mounting is on unmanned aerial vehicle main part cavity diapire, the case lid rotates with adding the tub top to be connected, the water pump bottom mounting is on unmanned aerial vehicle main part cavity diapire, the water pump passes through the wire intercommunication with control chip, the pipe of scattering all is through a plurality of connecting pieces fixed mounting in unmanned aerial vehicle main part bottom, a plurality of shower nozzles and the intercommunication of the pipe apopore of scattering all.

Description

Vertical take-off and landing fixed wing unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned aerial vehicle's technical field especially relates to a VTOL fixed wing unmanned aerial vehicle.
Background
As is well known, a vertical take-off and landing fixed wing drone is an auxiliary device for pesticide spraying, and is widely used in the field of drones; the existing vertical take-off and landing fixed wing unmanned aerial vehicle comprises an unmanned aerial vehicle main body, a storage battery, a control chip, propellers, an empennage, supporting legs and a water tank, wherein the storage battery and the control chip are fixedly arranged inside a protection box of the unmanned aerial vehicle main body, the storage battery is communicated with the control chip through a signal line, the bottom end of the propeller is fixed at the top end of the unmanned aerial vehicle main body, the propellers are communicated with the control chip through a signal line, the left end of the empennage is fixed at the right end of the unmanned aerial vehicle main body; the existing vertical take-off and landing fixed wing unmanned aerial vehicle is discovered in use, the existing unmanned aerial vehicle is developed rapidly, and the application of the existing unmanned aerial vehicle in agricultural development becomes the trend of the times, and the existing garden trees have poor adaptability and high pesticide spraying limitation due to the fact that the branches and the trunk are high and the artificial pesticide spraying and insect killing can not meet the requirements.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides an improve and spray adaptability increases maneuverability, reduces the VTOL fixed wing unmanned aerial vehicle who uses the limitation.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle, including unmanned aerial vehicle main part, battery, control chip, screw, fin, supporting leg and water tank, battery and control chip fixed mounting are inside unmanned aerial vehicle main part guard box to battery and control chip pass through the signal line intercommunication, and the screw bottom is fixed on unmanned aerial vehicle main part top, and screw and control chip pass through the signal line intercommunication, and the fin left end is fixed at unmanned aerial vehicle main part right-hand member, and a plurality of supporting legs cooperate to be fixed in unmanned aerial vehicle main part bottom; still include the water tank, add the pipe, the case lid, a water pump, the connecting piece, pipe and shower nozzle all disperse, the water tank bottom mounting is on unmanned aerial vehicle main part cavity diapire, the water tank top is provided with and adds the pipe, the case lid rotates with adding the pipe top and is connected, the water pump bottom mounting is on unmanned aerial vehicle main part cavity diapire, the water pump passes through the wire intercommunication with control chip, and water pump input end and water tank working chamber intercommunication, the pipe all disperses is through a plurality of connecting piece fixed mounting in unmanned aerial vehicle main part bottom, be provided with a plurality of apopores on the pipe all disperses, a plurality of shower nozzles and the.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes agitator motor, axle sleeve, (mixing) shaft and stirring rake, and the agitator motor bottom mounting is on the water tank top, and axle sleeve fixed mounting is on the tank roof, (mixing) shaft top and agitator motor bottom output coaxial coupling to the axle sleeve rotates with the coaxial cooperation of (mixing) shaft to be connected, and a plurality of stirring rakes fixed mounting is on the (mixing) shaft, and the stirring rake is located inside the water tank working chamber.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes solar cell panel and mounting, and a plurality of mounting fixed connection are passed through with the fin top in the solar cell panel bottom, and the case lid passes through the wire with the battery and communicates.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes a spacing section of thick bamboo, gag lever post and spring, and gag lever post bottom slidable mounting is in a spacing section of thick bamboo inner chamber, and spring bottom fixed mounting is on a spacing section of thick bamboo inner chamber diapire, and the spring top is fixed in the gag lever post bottom, and the supporting leg bottom mounting is on the gag lever post top.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes light and lamp shade, and the light top is fixed in unmanned aerial vehicle main part bottom to the light passes through the wire intercommunication with control chip, and the lamp shade top is fixed in the light bottom, and inside the light was located the lamp shade.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes level sensor and alarm lamp, and the level sensor bottom mounting is on water tank working chamber diapire, and the alarm lamp bottom mounting is on unmanned aerial vehicle main part top, and weapon level sensor and alarm lamp pass through signal line intercommunication.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes loudspeaker, and the loudspeaker top is fixed in the water tank bottom to loudspeaker and control chip pass through the wire intercommunication.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle still includes the balance plate, and the balance plate top is fixed in a plurality of spacing bobbin ends.
Compared with the prior art, the beneficial effects of the utility model are that: make the pesticide be convenient for add the water tank working chamber through adding the pipe, make the pesticide in the water tank working chamber prevent to rock through the case lid and spill outward, make scattered pipe and unmanned aerial vehicle main part fixed mounting all through a plurality of connecting pieces cooperations, the water pump makes the pesticide in the water tank working chamber carry out the insecticidal processing to ornamental trees and shrubs through scattered pipe and a plurality of shower nozzle cooperation, improves and sprays the adaptability, increases maneuverability, reduces and uses the limitation.
Drawings
Fig. 1 is a schematic front view of the present invention;
fig. 2 is a schematic view of the internal structure of the present invention;
fig. 3 is a partially enlarged schematic view of the present invention;
fig. 4 is a partial left side schematic view of the present invention;
in the drawings, the reference numbers: 1. an unmanned aerial vehicle main body; 2. a storage battery; 3. a control chip; 4. a propeller; 5. a tail wing; 6. supporting legs; 7. a water tank; 8. an addition pipe; 9. a box cover; 10. a water pump; 11. a connecting member; 12. a dispersion pipe; 13. a spray head; 14. a stirring motor; 15. a shaft sleeve; 16. a stirring shaft; 17. a stirring paddle; 18. a solar panel; 19. a fixing member; 20. a limiting cylinder; 21. a limiting rod; 22. a spring; 23. an illuminating lamp; 24. a lamp shade; 25. a liquid level sensor; 26. an alarm lamp; 27. a horn; 28. and a balance plate.
Detailed Description
The following detailed description of the embodiments of the present invention is provided with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
As shown in fig. 1 to 4, the utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, including unmanned aerial vehicle main part 1, battery 2, control chip 3, screw 4, fin 5, supporting leg 6 and water tank 7, battery 2 and control chip 3 fixed mounting are inside unmanned aerial vehicle main part 1 guard box, and battery 2 and control chip 3 communicate through the signal line, screw 4 bottom is fixed on unmanned aerial vehicle main part 1 top, and screw 4 and control chip 3 communicate through the signal line, fin 5 left end is fixed at unmanned aerial vehicle main part 1 right-hand member, a plurality of supporting legs 6 cooperate to be fixed in unmanned aerial vehicle main part 1 bottom; the bottom end of the water tank 7 is fixed on the bottom wall of a cavity of the unmanned aerial vehicle main body 1, the adding pipe 8 is arranged at the top end of the water tank 7, the tank cover 9 is rotatably connected with the top end of the adding pipe 8, the bottom end of the water pump 10 is fixed on the bottom wall of the cavity of the unmanned aerial vehicle main body 1, the water pump 10 is communicated with the control chip 3 through a wire, the input end of the water pump 10 is communicated with a working cavity of the water tank 7, the dispersing pipe 12 is fixedly arranged at the bottom end of the unmanned aerial vehicle main body 1 through a plurality of connecting pieces 11, a plurality of water outlet holes are formed in the dispersing pipe 12, and the plurality of spray heads 13 are communicated with the water outlet holes of; make the pesticide be convenient for add to 7 working chambers of water tank through adding pipe 8, make the pesticide in 7 working chambers of water tank prevent to rock through case lid 9 and spill outward, make pipe 12 and the 1 fixed mounting of unmanned aerial vehicle main part scattered all through the cooperation of a plurality of connecting pieces 11, water pump 10 makes the pesticide in 7 working chambers of water tank carry out the insecticidal processing to ornamental trees and shrubs through the cooperation of pipe 12 and a plurality of shower nozzle 13 scattered all, the improvement sprays the adaptability, increase maneuverability, reduce and use the limitation.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle, still include agitator motor 14, axle sleeve 15, (mixing) shaft 16 and stirring rake 17, 14 bottom end of agitator motor are fixed on the top of water tank 7, axle sleeve 15 is fixed to be installed on the roof of water tank 7, 16 top ends of (mixing) shafts and 14 bottom output coaxial connections of agitator motor, and axle sleeve 15 and 16 coaxial cooperation of (mixing) shaft rotate to be connected, a plurality of stirring rakes 17 are fixed to be installed on (mixing) shaft 16, and stirring rake 17 is located the inside of water tank 7 working chamber; axle sleeve 15 makes the pesticide in the water tank 7 work cavity stir through the cooperation of (mixing) shaft 16 and a plurality of stirring rake 17, makes (mixing) shaft 16 rotate the location through axle sleeve 15, reduces the sediment of pesticide, improves insecticidal stability, reduces and uses the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, still include solar cell panel 18 and mounting 19, the bottom of solar cell panel 18 is connected with the top of empennage 5 through a plurality of mountings 19 are fixed, case lid 9 is communicated with battery 2 through the wire; make solar cell panel 18 fixed mounting through the cooperation of a plurality of mountings 19, make solar energy conversion store in battery 2 through solar cell panel 18, improve resource utilization, increase device duration, improve the adaptability, reduce and use the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, still include a spacing section of thick bamboo 20, gag lever post 21 and spring 22, gag lever post 21 bottom is installed in the inner chamber of a spacing section of thick bamboo 20 slidably, and spring 22 bottom is fixed mounting on the inner chamber bottom wall of a spacing section of thick bamboo 20, and the top of spring 22 is fixed in gag lever post 21 bottom, and the bottom of supporting leg 6 is fixed in gag lever post 21 top; make the device descend through the cooperation of a plurality of springs 22 and cushion, gag lever post 21 and the cooperation of a spacing section of thick bamboo 20 make a spacing section of thick bamboo 20 work spacingly, improve support stability, increase the protection to the device, reduce and use the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, still include light 23 and lamp shade 24, the light 23 top is fixed in the unmanned aerial vehicle main part 1 bottom, and light 23 and control chip 3 pass through the wire and communicate, the lamp shade 24 top is fixed in the light 23 bottom, and the light 23 is located the lamp shade 24 inside; but make device pesticide spray go on night through light 23, make light 23 protect through lamp shade 24, improve work adaptability, reduce and use the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, still include level sensor 25 and alarm lamp 26, the bottom of level sensor 25 is fixed on the bottom wall of the working chamber of water tank 7, the bottom of alarm lamp 26 is fixed on the top of main body 1 of unmanned aerial vehicle, weapon level sensor 25 and alarm lamp 26 are communicated through the signal line; make the pesticide surplus in the water tank 7 working chamber monitor through level sensor 25 and the cooperation of alarm lamp 26, improve maneuverability, increase and use the convenience, reduce and use the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, still include loudspeaker 27, the top of loudspeaker 27 is fixed in the bottom of water tank 7, and loudspeaker 27 and control chip 3 are communicated through the wire; through setting up loudspeaker 27 and driving the animal, prevent that the pesticide from spraying the harm of killing to the animal, improve the adaptability, reduce and use the limitation.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, which also comprises a balance plate 28, wherein the top end of the balance plate 28 is fixed at the bottom ends of a plurality of limiting cylinders 20; the balance plate 28 increases the starting stability of the device, increases the adaptability and reduces the use limitation.
The utility model discloses a VTOL fixed wing unmanned aerial vehicle, it is at the during operation, at first through adding 8 and adding full pesticides in with 7 cavitys of water tank, later make 4 drive arrangement of screw and rise through control chip 3 control, then start loudspeaker 27, water pump 10 and agitator motor 14 through control chip 3, later stir the pesticide through (mixing) shaft 16 and a plurality of stirring rake 17, then make a plurality of shower nozzles 13 spray the pesticide through water pump 10 can.
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle, the installation mode, the connection mode or the setting mode are common mechanical modes, and the installation mode, the connection mode or the setting mode can be implemented as long as the beneficial effects can be achieved; the utility model discloses a VTOL fixed wing unmanned aerial vehicle's water pump 10 and agitator motor 14 are purchase on the market, and this industry technical staff only need according to its subsidiary instructions install and operate can.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.

Claims (8)

1. A vertical take-off and landing fixed wing unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), a storage battery (2), a control chip (3), a propeller (4), an empennage (5), supporting legs (6) and a water tank (7), wherein the storage battery (2) and the control chip (3) are fixedly installed inside a protection box of the unmanned aerial vehicle main body (1), the storage battery (2) and the control chip (3) are communicated through a signal line, the bottom end of the propeller (4) is fixed at the top end of the unmanned aerial vehicle main body (1), the propeller (4) is communicated with the control chip (3) through a signal line, the left end of the empennage (5) is fixed at the right end of the unmanned aerial vehicle main body (1), and a plurality of supporting legs (; the unmanned aerial vehicle is characterized by further comprising a water tank (7), an adding pipe (8), a tank cover (9), a water pump (10), a connecting piece (11), a uniform scattering pipe (12) and spray heads (13), the bottom end of the water tank (7) is fixed on the bottom wall of the cavity of the unmanned aerial vehicle main body (1), the top end of the water tank (7) is provided with the adding pipe (8), the tank cover (9) is rotatably connected with the top end of the adding pipe (8), the bottom end of the water pump (10) is fixed on the bottom wall of the cavity of the unmanned aerial vehicle main body (1), the water pump (10) is communicated with the control chip (3) through a lead, the input end of the water pump (10) is communicated with the working cavity of the water tank (7), the uniform scattering pipe (12) is fixedly installed at the bottom end of the unmanned aerial vehicle main body (1) through the connecting pieces (11), the.
2. The VTOL fixed wing UAV of claim 1, further comprising a stirring motor (14), a shaft sleeve (15), a stirring shaft (16) and stirring paddles (17), wherein the bottom end of the stirring motor (14) is fixed on the top end of the water tank (7), the shaft sleeve (15) is fixedly installed on the top wall of the water tank (7), the top end of the stirring shaft (16) is coaxially connected with the bottom output end of the stirring motor (14), the shaft sleeve (15) is coaxially matched with the stirring shaft (16) to be rotatably connected, the stirring paddles (17) are fixedly installed on the stirring shaft (16), and the stirring paddles (17) are located inside the working cavity of the water tank (7).
3. The VTOL fixed wing UAV of claim 2, further comprising a solar panel (18) and a plurality of fasteners (19), wherein the bottom of the solar panel (18) is fixedly connected with the top of the empennage (5) through the plurality of fasteners (19), and the box cover (9) is communicated with the storage battery (2) through a wire.
4. The VTOL fixed wing UAV of claim 3, further comprising a limiting cylinder (20), a limiting rod (21) and a spring (22), wherein the bottom end of the limiting rod (21) is slidably mounted in the inner cavity of the limiting cylinder (20), the bottom end of the spring (22) is fixedly mounted on the bottom wall of the inner cavity of the limiting cylinder (20), the top end of the spring (22) is fixed at the bottom end of the limiting rod (21), and the bottom end of the supporting leg (6) is fixed at the top end of the limiting rod (21).
5. The VTOL fixed wing UAV of claim 4, further comprising an illumination lamp (23) and a lampshade (24), wherein the top end of the illumination lamp (23) is fixed at the bottom end of the UAV main body (1), the illumination lamp (23) is communicated with the control chip (3) through a wire, the top end of the lampshade (24) is fixed at the bottom end of the illumination lamp (23), and the illumination lamp (23) is positioned inside the lampshade (24).
6. The VTOL fixed wing UAV of claim 5, further comprising a liquid level sensor (25) and a warning lamp (26), wherein the bottom end of the liquid level sensor (25) is fixed on the bottom wall of the working cavity of the water tank (7), the bottom end of the warning lamp (26) is fixed on the top end of the UAV main body (1), and the weapon liquid level sensor (25) and the warning lamp (26) are communicated through a signal line.
7. The VTOL fixed wing UAV of claim 6, further comprising a speaker (27), wherein the top of the speaker (27) is fixed at the bottom of the water tank (7), and the speaker (27) is connected with the control chip (3) through a wire.
8. The VTOL fixed wing UAV of claim 7, further comprising a balancing plate (28), wherein the top end of the balancing plate (28) is fixed at the bottom end of the plurality of position-limiting cylinders (20).
CN202021120247.4U 2020-06-16 2020-06-16 Vertical take-off and landing fixed wing unmanned aerial vehicle Active CN212401568U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116749866A (en) * 2023-08-22 2023-09-15 常州星宇车灯股份有限公司 Vertical take-off and landing lighting auxiliary system of aerocar and aerocar

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116749866A (en) * 2023-08-22 2023-09-15 常州星宇车灯股份有限公司 Vertical take-off and landing lighting auxiliary system of aerocar and aerocar

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