CN218112987U

CN218112987U - Special highway patrol unmanned aerial vehicle for group fog weather

Info

Publication number: CN218112987U
Application number: CN202221895437.2U
Authority: CN
Inventors: 刘壮
Original assignee: Gaozhesai Technology Nantong Co ltd
Current assignee: Gaozhesai Technology Nantong Co ltd
Priority date: 2022-07-21
Filing date: 2022-07-21
Publication date: 2022-12-23
Anticipated expiration: 2032-07-21

Abstract

The utility model discloses a special highway inspection unmanned aerial vehicle of group's fog day relates to unmanned air vehicle technique field, the reciprocating impact tunnel drilling machine comprises a machine body, the equal fixedly connected with support frame in bottom both sides of fuselage, the bottom fixedly connected with dead lever of support frame, the bottom fixedly connected with spring of dead lever, the bottom fixedly connected with stabilizer blade of spring, the top fixedly connected with cabin of fuselage, the top swing joint in cabin has the pivot, the top fixedly connected with dust-proof housing of pivot. This special highway of group's fog sky gas patrols unmanned aerial vehicle can transmit the wing with the heat that the motor produced through hollow rotating shaft and the breather pipe that set up the through-hole, thereby avoids smoke and dust and ashes and drop of water to combine with the drop of water evaporation on the wing, has not only solved the overheated problem that produces of motor, has avoided the trouble that unmanned aerial vehicle patrols when the conflagration takes place for group's fog sky gas moreover to appear, has strengthened the practicality of device.

Description

Special highway patrol unmanned aerial vehicle for cluster fog weather

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a special highway patrol unmanned aerial vehicle of group's fog day.

Background

The unmanned aerial vehicle is relatively fast to develop in recent years, and has the advantages of relatively low cost, good maneuverability, convenient use and the like, so that the unmanned aerial vehicle has extremely wide application prospects in civil fields such as aerial photography, geological survey, high-voltage transmission line inspection, oil field pipeline inspection, highway management, forest fire prevention inspection, toxic gas investigation, drug enforcement, emergency rescue, rescue and the like, has low visibility in cluster fog weather, and is very easy to cause accidents on highways; therefore, the special highway patrol unmanned aerial vehicle is often adopted to patrol on the highway, so that accidents can be found in time, and information can be fed back to patrol personnel on the highway in time to treat the accidents.

When the existing highway patrol unmanned aerial vehicle has a fire disaster due to a traffic accident on a patrol highway, smoke dust and ash generated by the fire disaster are easy to fall on the surface of a wing in the process that the unmanned aerial vehicle is in a circling state on site; and the wing surface produces the drop of water easily in group fog weather, and smoke and dust and ashes combine and closely adhere to at the wing surface with the drop of water for not only the wing rotates the resistance grow, leads to wing weight uneven distribution moreover easily, thereby influences unmanned aerial vehicle's equilibrium.

Therefore, it is necessary to provide a highway patrol unmanned aerial vehicle dedicated to foggy weather to solve the above problems.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model aims to provide a special highway patrol unmanned aerial vehicle for foggy weather, which aims to solve the problem that smoke dust and ash generated by fire easily fall on the surface of a wing when the unmanned aerial vehicle is in a spiral process on site when the existing patrol highway proposed in the background technology is in fire due to a traffic accident; and the wing surface produces the drop of water easily in group fog weather, and smoke and dust and ashes combine and closely adhere to on the wing surface with the drop of water not only make the rotor rotate the resistance grow, lead to rotor weight uneven distribution moreover easily to influence the problem of unmanned aerial vehicle's equilibrium.

(II) technical scheme

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a special highway of group's fog sky gas patrols unmanned aerial vehicle, includes the fuselage, the equal fixedly connected with support frame in bottom both sides of fuselage, the bottom fixedly connected with dead lever of support frame, the bottom fixedly connected with spring of dead lever, the bottom fixedly connected with stabilizer blade of spring, the top fixedly connected with cabin of fuselage, the top swing joint in cabin has the pivot, the top fixedly connected with dust shell of pivot, the inside one side fixedly connected with inner deck of dust shell, the opposite side fixedly connected with monitoring device of dust shell, inner deck bottom fixedly connected with fan, inner deck top fixedly connected with air outlet, the one end fixedly connected with camera lens of inner deck is kept away from to monitoring device, the equal fixedly connected with horn in four corners department of fuselage, the one end fixedly connected with protecting sheathing of fuselage is kept away from to the horn, the inside fixedly connected with motor room of protecting sheathing, the bottom fixedly connected with motor of motor room, the hollow pivot of output fixedly connected with of motor. The top end of the hollow rotating shaft is fixedly connected with a connector, and the outer portion of the connector is fixedly connected with a wing.

Preferably, the outer side of the spring is sleeved with a sleeve, and the bottom end of the sleeve is fixedly connected with the support leg.

Preferably, the air outlet is located at the top end of the monitoring device, one end of the air outlet is located at the top end of the inner chamber, and the other end of the air outlet is located above the lens.

Preferably, a through hole is formed in the outer side of one end, located inside the motor chamber, of the hollow rotating shaft.

Preferably, the insides of the wings are fixedly connected with vent pipes.

Preferably, one end of the vent pipe, which is far away from the wing, extends into the connector and is communicated with the interior of the hollow rotating shaft.

Preferably, the number of the wings is multiple, and the wings are distributed on the outer side of the connector in an annular array.

(III) advantageous effects

Compared with the prior art, the utility model provides a special highway patrol unmanned aerial vehicle of group's fog day possesses following beneficial effect:

1. this special highway patrol unmanned aerial vehicle of group's fog day gas can be with the heat transfer to the wing that the motor produced through hollow rotating shaft and the breather pipe that set up to have the through-hole, thereby avoid smoke and dust and ashes and drop of water to combine with the drop of water evaporation on the wing, not only solved the overheated problem that produces of motor, the trouble that unmanned aerial vehicle patrol when having avoided group's fog day gas to take place the conflagration moreover appears has strengthened the practicality of device.

2. This special highway of group fog day gas patrols unmanned aerial vehicle through set up the fan in the inner deck, transmits away the wind that the fan produced through the air outlet, and the condition that the water smoke influences the shooting has appeared on not only having avoided group fog day gas lens in the air blow of air outlet in camera lens the place ahead, can avoid tiny granule such as dust to adhere to on the camera lens moreover.

3. This special highway of group's fog sky patrols unmanned aerial vehicle through set up the spring in support frame below, can avoid receiving great impact force when falling to the ground, thereby causes the condition of harm leading to unmanned aerial vehicle's trouble to unmanned aerial vehicle inner structure.

Drawings

Fig. 1 is a schematic front view of the structure of the unmanned aerial vehicle of the present invention;

fig. 2 is a schematic perspective view of the structure of the unmanned aerial vehicle of the present invention;

fig. 3 is a schematic sectional view of the leg structure of the unmanned aerial vehicle of the present invention;

fig. 4 is a schematic sectional view of the inner cabin structure of the unmanned aerial vehicle of the present invention;

figure 5 is the utility model discloses the cross-sectional schematic view of unmanned aerial vehicle motor room structure.

In the figure: 1. a body; 2. a support frame; 3. fixing the rod; 4. a sleeve; 5. a spring; 6. a support leg; 7. a nacelle; 8. a rotating shaft; 9. a dust-proof shell; 10. a lens; 11. an inner chamber; 12. a fan; 13. an air outlet; 14. a horn; 15. a protective housing; 16. a hollow rotating shaft; 17. a connector; 18. an airfoil; 19. a motor; 20. a through hole; 21. a motor chamber; 22. a breather pipe; 23. and a monitoring device.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1-5, a highway patrol unmanned aerial vehicle special for cluster fog comprises a body 1, wherein two sides of the bottom end of the body 1 are fixedly connected with a support frame 2, the bottom end of the support frame 2 is fixedly connected with a fixed rod 3, the bottom end of the fixed rod 3 is fixedly connected with a spring 5, the body 1 can be prevented from being subjected to large impact force when falling to the ground, the internal structure of the unmanned aerial vehicle is damaged, and the unmanned aerial vehicle is prevented from being broken down, the bottom end of the spring 5 is fixedly connected with a support leg 6, the top end of the body 1 is fixedly connected with a cabin 7, the top end of the cabin 7 is movably connected with a rotating shaft 8, the top end of the rotating shaft 8 is fixedly connected with a dustproof shell 9, one side of the interior of the dustproof shell 9 is fixedly connected with an inner cabin 11, the other side of the dustproof shell 9 is fixedly connected with a monitoring device 23, the bottom end of the inner cabin 11 is fixedly connected with a fan 12, wind generated by the fan 12 is transmitted out through an air outlet 13, wind of the air outlet 13 in front of the body 10 is prevented from affecting the condition that water mist is generated by fine particles such as dust and a hollow motor 16 is connected with a hollow motor cabin 11, and a motor cabin 13 is connected with a motor 14, thereby evaporate the drop of water on wing 18 and avoid smoke and dust and ember to combine with the drop of water, the problem of motor 19 overheat production has not only been solved, and the trouble that unmanned aerial vehicle patrol appears when having avoided group fog day gas to break out a fire, the practicality of device has been strengthened, the top fixedly connected with connector 17 of hollow rotating shaft 16, the outside fixedly connected with wing 18 of connector 17, sleeve 4 has been cup jointed in the outside of spring 5, the bottom and the stabilizer blade 6 fixed connection of sleeve 4, its one end is located the top of monitoring device 23 in air outlet 13 is located interior cabin 11 top, the other end of air outlet 13 is located camera lens 10 top, the one end outside that hollow rotating shaft 16 is located motor room 21 inside is equipped with through-hole 20, the equal fixedly connected with breather pipe 22 in inside of wing 18, the one end that breather pipe 22 kept away from wing 18 all stretches into connector 17 and communicates with hollow rotating shaft 16 is inside, wing 18 has a plurality ofly, a plurality of wings 18 are in the outside connector 17 and are the annular array and distribute.

The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.

The working principle is as follows: open motor 19 when group's fog weather needs to use this unmanned aerial vehicle and make unmanned aerial vehicle lift off, then open monitoring device 23 and fan 12 again, control unmanned aerial vehicle and fly to the area that needs to observe, thereby the drop of water appears easily before group's fog weather camera lens 10 and influence the shooting, and fan 12's rotation can blow off wind from the position of air outlet 13, the wind that blows off not only can weather the drop of water but also can avoid some dust and particulate matter to adhere to on camera lens 10, if need adjust the steerable pivot 8 of shooting angle and rotate and then drive camera lens 10 and remove, when patrolling the conflagration that takes place because of the car accident on the road, hollow shaft 16 that has through-hole 20 and breather pipe 22 can transmit the heat that motor 19 produced to wing 18, thereby the drop of water evaporation on the wing 18 avoids smoke and dust and ashes and the combination of drop of water, the overheated problem of producing of motor 19 has not only been solved, and the trouble that the patrol appearance when having avoided group's fog weather to take place the conflagration, the inside spring 5 of sleeve 4 has avoided the impact force to cause the condition of harm to fuselage 1 inner structure when falling to the ground of unmanned aerial vehicle.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims

1. The utility model provides a special highway patrol unmanned aerial vehicle of group's fog day, includes fuselage (1), its characterized in that: the dust-proof device is characterized in that both sides of the bottom end of the machine body (1) are fixedly connected with a support frame (2), the bottom end of the support frame (2) is fixedly connected with a fixed rod (3), the bottom end of the fixed rod (3) is fixedly connected with a spring (5), the bottom end of the spring (5) is fixedly connected with a support leg (6), the top end of the machine body (1) is fixedly connected with a cabin (7), the top end of the cabin (7) is movably connected with a rotating shaft (8), the top end of the rotating shaft (8) is fixedly connected with a dust-proof shell (9), one side of the inner part of the dust-proof shell (9) is fixedly connected with an inner cabin (11), the other side of the dust-proof shell (9) is fixedly connected with a monitoring device (23), the bottom end of the inner cabin (11) is fixedly connected with an air outlet (13), the monitoring device (23) is far away from one end of the inner cabin (11) is fixedly connected with an inner cabin (10), four corners of the machine body (1) are fixedly connected with machine arms (14), one end of the machine arms (14) far away from the machine body (1) is fixedly connected with a protective shell (15), the inner part of the protective shell (15) is fixedly connected with a motor chamber (21), and the motor chamber (19) is fixedly connected with a hollow motor output end of the motor (19), and a motor chamber (19) is fixedly connected with a motor (16), the top end of the hollow rotating shaft (16) is fixedly connected with a connector (17), and the outer portion of the connector (17) is fixedly connected with a wing (18).

2. The unmanned aerial vehicle for patrolling expressway special for foggy weather according to claim 1, wherein: the outer side of the spring (5) is sleeved with a sleeve (4), and the bottom end of the sleeve (4) is fixedly connected with the support legs (6).

3. The unmanned aerial vehicle for patrolling expressway special for foggy weather according to claim 1, wherein: the air outlet (13) is positioned at the top end of the monitoring device (23), one end of the air outlet is positioned at the top end of the inner chamber (11), and the other end of the air outlet (13) is positioned above the lens (10).

4. The unmanned aerial vehicle for patrolling expressway special for group fog weather of claim 1, which is characterized in that: and a through hole (20) is formed in the outer side of one end, positioned in the motor chamber (21), of the hollow rotating shaft (16).

5. The unmanned aerial vehicle for patrolling expressway special for group fog weather of claim 1, which is characterized in that: the insides of the wings (18) are fixedly connected with vent pipes (22).

6. The unmanned aerial vehicle for patrolling expressway special for foggy weather of claim 5, wherein: one end of the vent pipe (22) far away from the wing (18) extends into the connector (17) and is communicated with the inside of the hollow rotating shaft (16).

7. The unmanned aerial vehicle for patrolling expressway special for foggy weather according to claim 1, wherein: the number of the wings (18) is multiple, and the wings (18) are distributed on the outer side of the connector (17) in an annular array.