CN213008736U

CN213008736U - Aircraft for patrolling illegal parking vehicle

Info

Publication number: CN213008736U
Application number: CN202021856095.4U
Authority: CN
Inventors: 韩洋
Original assignee: 刘佳丽
Current assignee: Zhongshuzhi Technology (Taiyuan) Co.,Ltd.
Priority date: 2020-08-31
Filing date: 2020-08-31
Publication date: 2021-04-20
Anticipated expiration: 2030-08-31

Abstract

The utility model discloses an aircraft for patrolling illegal parking vehicles, which comprises an aircraft main body, a motor A is arranged at the middle position of the bottom of the aircraft main body, an installation bin B is arranged outside the motor A, a protection cover A is arranged outside the installation bin B, a protection cover B is arranged outside the protection cover A, a protection cover C is arranged outside the protection cover B, limiting grooves A are symmetrically arranged at the middle positions of two ends inside the limiting grooves A, limiting grooves B are symmetrically arranged at the middle positions of two ends inside the protection cover C, limiting rods are arranged at the middle positions of the tops of two ends of the protection cover C, and the output end of the motor A is provided with a rotating shaft A; the utility model discloses the device makes the device have shock-absorbing function under the cooperation through mount pad, articulated slab, interior sleeve pipe, spring B, outer tube, spacing ring, connecting rod and slider, when falling to the ground fast, provides certain cushion effect, reduces the injury to internals.

Description

Aircraft for patrolling illegal parking vehicle

Technical Field

The utility model relates to an aircraft technical field specifically is an aircraft of vehicle inspection usefulness of violating the parking.

Background

For the current illegal parking, the inevitable problem caused by less parking spaces relative to the number of vehicles is solved, along with the increase of the urbanization process, the road complexity is improved, the difficulty of manual inspection of a traffic police and the energy required to be consumed are higher, the unmanned aerial vehicle is an aircraft which is dynamic, controllable, can carry various task equipment to execute various tasks and can be repeatedly used, the aircraft is used for carrying the camera shooting device, the daily patrol work of the traffic police can be realized, the patrol of regional roads and illegal parking conditions can be quickly completed only by controlling the aircraft through the control equipment and the monitoring equipment in a certain region, a series of defect problems of manual patrol can be effectively avoided, the patrol efficiency is improved, and the waste of human resources and time cost is reduced;

the prior device has the following defects:

1. an aircraft may fail when landing because it falls too quickly due to improper handling, causing damage to parts inside the aircraft.

2. When the camera device is not used, dust may be accumulated on the surface of the camera, and the camera device may be scraped during storage, thereby affecting the definition during shooting.

3. The existing camera equipment is mostly fixedly installed, and can be shot only by adjusting the angle of the aircraft, so that the difficulty of operation is increased, and the vehicle is not easy to shoot.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an aircraft for the patrol of the illegal parking vehicles, which aims to solve the problem that the parts in the aircraft are damaged and break down because the aircraft falls too fast due to improper operation when falling to the ground in the background technology; when the camera equipment is not used, dust can be accumulated on the surface of the camera, and the camera equipment can be scraped and bumped during storage, so that the definition can be influenced during shooting; the existing camera equipment is mostly fixedly installed, and can be shot only by adjusting the angle of an aircraft, so that the difficulty of operation is increased, and the problem of shooting a vehicle is not easy.

In order to achieve the above object, the utility model provides a following technical scheme: an aircraft for patrolling illegal parking vehicles comprises an aircraft body, wherein a motor A is arranged at the middle position of the bottom of the aircraft body, an installation bin B is arranged outside the motor A, a protection cover A is arranged outside the installation bin B, a protection cover B is arranged outside the protection cover A, a protection cover C is arranged outside the protection cover B, limiting grooves A are symmetrically arranged at the middle positions of two ends inside the protection cover B, limiting grooves B are symmetrically arranged at the middle positions of two ends inside the protection cover C, limiting rods are arranged at the middle positions of the tops of two ends of the protection cover C, the output end of the motor A is provided with a rotating shaft A, an installation frame is arranged at the bottom of the rotating shaft A, a motor B is arranged at one end of the installation frame, a rotating shaft B is arranged at the output end of the motor B, an infrared camera is arranged outside the rotating shaft B, the bottom of the infrared camera is provided with a high-definition camera, four corners of the bottom of the aircraft body are provided with mounting seats, the bottom of each mounting seat is hinged with a hinged plate, the bottom of each hinged plate is provided with an inner sleeve, the top of the outer side of the inner sleeve is provided with a limiting ring, the bottom of the inner sleeve is sleeved with an outer sleeve, the outer sleeves and the limiting rings are directly sleeved with springs B, the bottoms of the two groups of outer sleeves are provided with mounting plates, the top of each mounting plate is provided with a chute, a slide block is arranged inside the chute and matched with the slide block, the top of the slide block is provided with a connecting rod, the top of the connecting rod is hinged with the aircraft body, the bottom of each mounting plate is provided with a support frame, the middle parts of two ends of the, a spring A is sleeved between the pressing block and the mounting bin A.

Preferably, a protection bin is arranged outside the motor B.

Preferably, one end of the spring A is in a circular arc structure.

Preferably, the bottoms of the protective covers A and B are provided with clamping blocks.

Preferably, the support frame is made of an L-shaped frame structure.

Preferably, the mounting frame is made of a U-shaped frame structure.

Compared with the prior art, the beneficial effects of the utility model are that: an aircraft for the inspection of the illegal vehicle;

1. under the matching of the mounting seat, the hinged plate, the inner sleeve, the spring B, the outer sleeve, the limiting ring, the connecting rod and the sliding block, the device has a damping function, and provides a certain buffering force when falling to the ground quickly, so that the damage to internal parts is reduced;

2. the camera shooting device in the camera is protected by matching the protective cover A, the limiting groove A, the protective cover B, the limiting rod, the limiting groove B and the protective cover C, and dust is prevented from falling onto the surface of the camera under the condition of nonuse;

3. under the cooperation through motor A, pivot A, motor B and pivot B, make camera equipment can adjust the position, made things convenient for and shot the vehicle, reduced the operation degree of difficulty.

Drawings

Fig. 1 is a side cross-sectional view of the present invention;

fig. 2 is a side view of the present invention;

FIG. 3 is a front view of the present invention;

FIG. 4 is a side cross-sectional view of the bottom of the aircraft body of the present invention;

fig. 5 is a schematic structural view of the installation bin a of the present invention;

fig. 6 is an enlarged schematic view of the structure a of fig. 1 according to the present invention;

fig. 7 is an enlarged schematic view of the structure B of fig. 1 according to the present invention; .

In the figure: 1. an aircraft body; 2. a motor A; 3. installing a bin A; 4. installing a frame; 5. a high-definition camera; 6. an infrared camera; 7. a support frame; 8. a rotating shaft A; 9. a connecting rod; 10. a protective cover A; 11. installing a bin B; 12. mounting a plate; 13. a chute; 14. a slider; 15. a rotating shaft B; 16. a limiting groove A; 17. a protective cover B; 18. a limiting rod; 19. a limiting groove B; 20. a protective cover C; 21. a pressing block; 22. a motor B; 23. a spring A; 24. a mounting seat; 25. a hinge plate; 26. an inner sleeve; 27. a spring B; 28. an outer sleeve; 29. a limit ring.

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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-7, the present invention provides an embodiment: an aircraft for patrolling illegal parking vehicles comprises an aircraft body 1, a motor A2 is arranged at the middle position of the bottom of the aircraft body 1, a mounting bin B11 is arranged outside a motor A2, a protective cover A10 is arranged outside a mounting bin B11, a protective cover B17 is arranged outside a protective cover A10, a protective cover C20 is arranged outside the protective cover B17, limiting grooves A16 are symmetrically arranged at the middle positions of two ends inside the protective cover B17, limiting grooves B19 are symmetrically arranged at the middle positions of two ends inside the protective cover C20, limiting rods 18 are arranged at the middle positions of the tops of two ends of the protective cover C20, a rotating shaft A8 is arranged at the output end of a motor A2, a mounting frame 4 is arranged at one end of the mounting frame 4, a rotating shaft B15 is arranged at the output end of a motor B22, an infrared camera 6 is arranged at the outer side of the rotating shaft B15, a high-definition camera 5 is arranged at the bottom of, four corners department of aircraft main part 1 bottom is provided with mount pad 24, the bottom of mount pad 24 articulates there is articulated plate 25, the bottom of articulated plate 25 is provided with interior sleeve pipe 26, the top in interior sleeve pipe 26 outside is provided with spacing ring 29, the bottom cover of interior sleeve pipe 26 is equipped with outer tube 28, outer tube 28 directly overlaps with spacing ring 29 and is equipped with spring B27, the bottom of two sets of outer tube 28 is provided with mounting panel 12, the top of mounting panel 12 is provided with spout 13, the inside of spout 13 is provided with slider 14, spout 13 and slider 14 looks adaptation, the top of slider 14 is provided with connecting rod 9, the top of connecting rod 9 is articulated with aircraft main part 1, the bottom of mounting panel 12 is provided with support frame 7, the centre symmetry at aircraft main part 1 bottom both ends is provided with installation storehouse A3, the inside both sides of installation storehouse A3 are provided with presses the briquetting 21.

The aircraft main body 1, the motor A2, the high-definition camera 5, the infrared camera 6 and the motor B22 in the device are the prior art, and the composition structure and the connection mode of the device are completely the same as those of the prior device.

Further, a protection cabin is arranged outside the motor B22 to protect the motor and prevent the motor from rotating.

Furthermore, one end of the spring A23 is of an arc structure, so that clamping is convenient.

Furthermore, the bottoms of the protective cover A10 and the protective cover B17 are provided with clamping blocks which support the protective cover B17 and the protective cover C20.

Further, the support frame 7 is made of an L-shaped frame structure, and supports the device body.

Further, the installation frame 4 is made for U style of calligraphy frame structure, makes things convenient for infrared camera 6 to adjust the position.

The working principle is as follows: the electric parts of the device are all powered by the storage battery, when shooting is carried out, a worker takes off the aircraft body 1 through remote control, the motor A2 is started to drive the rotating shaft A8 to rotate, the mounting frame 4 is enabled to rotate together, the infrared camera 6 can observe the periphery, the angle of the infrared camera 6 is adjusted through the motor B22 to observe the peripheral vehicles, and when illegal vehicles are found, the illegal vehicles are shot through the high-definition camera 5;

when the aircraft falls, the support frame 7 falls on the ground, the aircraft body 1 is pressed downwards to transmit force to the mounting seat 24, the mounting seat 24 is transmitted to the hinged plate 25 and the inner sleeve 26, the inner sleeve 26 slides in the outer sleeve 28, the spring B27 contracts and presses downwards to provide a buffering effect for the aircraft body 1, and the connecting rod 9 moves along the sliding groove 13 through the sliding block 14 to also provide a certain buffering effect.

When not using, pull-down protection casing C20, gag lever post 18 extrudees pressing block 21, and spring A23 shrink makes pressing block 21 shrink to both sides, and gag lever post 18 breaks away from spring A23, and protection casing B17 and protection casing C20 fall down, and the fixture block card on protection casing A10 is on spacing groove A16, and the fixture block card on protection casing B17 plays the guard action on spacing groove B19 to inside camera device.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims

1. An aircraft for the patrol of a parked vehicle, comprising an aircraft body (1), characterized in that: the aircraft is characterized in that a motor A (2) is arranged at the middle position of the bottom of the aircraft main body (1), an installation bin B (11) is arranged outside the motor A (2), a protection cover A (10) is arranged outside the installation bin B (11), a protection cover B (17) is arranged outside the protection cover A (10), a protection cover C (20) is arranged outside the protection cover B (17), limiting grooves A (16) are symmetrically arranged at the middle positions of the two ends inside the protection cover B (17), limiting grooves B (19) are symmetrically arranged at the middle positions of the two ends inside the protection cover C (20), limiting rods (18) are arranged at the middle positions of the tops of the two ends of the protection cover C (20), a rotating shaft A (8) is arranged at the output end of the motor A (2), an installation frame (4) is arranged at the bottom of the rotating shaft A (8), and a motor B (22) is arranged at one end of, the output of motor B (22) is provided with pivot B (15), the outside of pivot B (15) is provided with infrared camera (6), the bottom of infrared camera (6) is provided with high definition camera (5), the four corners department of aircraft main part (1) bottom is provided with mount pad (24), the bottom of mount pad (24) articulates there is articulated slab (25), the bottom of articulated slab (25) is provided with interior sleeve pipe (26), the top in interior sleeve pipe (26) outside is provided with spacing ring (29), the bottom cover of interior sleeve pipe (26) is equipped with outer tube (28), outer tube (28) and spacing ring (29) direct cover are equipped with spring B (27), two sets of the bottom of outer tube (28) is provided with mounting panel (12), the top of mounting panel (12) is provided with spout (13), the inside of spout (13) is provided with slider (14), spout (13) and slider (14) looks adaptation, the top of slider (14) is provided with connecting rod (9), the top and aircraft main part (1) of connecting rod (9) are articulated, the bottom of mounting panel (12) is provided with support frame (7), the centre symmetry at aircraft main part (1) bottom both ends is provided with installation storehouse A (3), the inside both sides of installation storehouse A (3) are provided with presses briquetting (21), it is equipped with spring A (23) to overlap between pressing briquetting (21) and installation storehouse A (3).

2. An aircraft for the patrol of an illicit vehicle according to claim 1, characterized in that: and a protection bin is arranged outside the motor B (22).

3. An aircraft for the patrol of an illicit vehicle according to claim 1, characterized in that: one end of the spring A (23) is of a circular arc structure.

4. An aircraft for the patrol of an illicit vehicle according to claim 1, characterized in that: and clamping blocks are arranged at the bottoms of the protective cover A (10) and the protective cover B (17).

5. An aircraft for the patrol of an illicit vehicle according to claim 1, characterized in that: the support frame (7) is made of an L-shaped frame structure.

6. An aircraft for the patrol of an illicit vehicle according to claim 1, characterized in that: the mounting frame (4) is made of a U-shaped frame structure.