CN218142121U

CN218142121U - Safety inspection monitoring unmanned aerial vehicle for surface mine

Info

Publication number: CN218142121U
Application number: CN202222661329.5U
Authority: CN
Inventors: 姜丁; 刘晓明; 刘伦; 侯海敬; 王淼; 潘睿; 马恒硕; 明林林; 赵志玮
Original assignee: Liantong Shandong Industry Internet Co ltd
Current assignee: Liantong Shandong Industry Internet Co ltd
Priority date: 2022-10-10
Filing date: 2022-10-10
Publication date: 2022-12-27
Anticipated expiration: 2032-10-10

Abstract

The utility model discloses an open mine safety patrols and examines monitoring unmanned aerial vehicle, including fuselage, horn and fender bracket, the side surface of fuselage runs through and installs the horn, and the one end of horn is fixed with the motor to the flabellum is installed to the output of motor, be connected with the slider in the cavity of fuselage side surface, and be connected with the auto-lock piece in the cavity of fuselage, and the inner wall of fuselage cavity is fixed with the blotter, the surface of horn runs through and installs the unlocking piece, the lower fixed surface of fuselage has the camera. This open mine safety patrols and examines monitoring unmanned aerial vehicle is provided with little impeller and driving plate, makes this device drive the semi-gear rotation through the rotation of little impeller, and the semi-gear drives the driving plate through the tooth piece and carries out reciprocating sliding to drive clean brush board and clear up the filter screen on fender bracket surface, reach the purpose of automatic clearance, be favorable to this device to reduce impurity and push at the filter screen surface, guarantee the flight efficiency of this device.

Description

Safety inspection monitoring unmanned aerial vehicle for surface mine

Technical Field

The utility model relates to an open mine patrols and examines technical field, specifically is an open mine safety patrols and examines monitoring unmanned aerial vehicle.

Background

The mine industry belongs to one of high-risk industries, potential safety hazards are main factors causing accidents, and the potential safety hazards in the production process of enterprises need to be identified and then managed to realize safety management of the enterprises, and monitoring is carried out by using an unmanned aerial vehicle during safety inspection of surface mines;

current unmanned aerial vehicle of patrolling and examining patrols and examines in the sky in mine, because the mining exploitation leads to in the air dust impurity more, based on 5G unmanned aerial vehicle dust keeper as disclosed in publication No. CN214524394U, fix through circular telegram magnet stick and play dirt-proof effect to the dust cover, but it can't clear up impurity automatically, accumulational impurity influences unmanned aerial vehicle's flight efficiency, and then the effect of patrolling and examining is influenced, and current unmanned aerial vehicle is when maintaining, the dismouting of fuselage and horn is comparatively complicated, need rotate the dismouting to both fixed bolts through the instrument, the time of extension maintenance, influence the efficiency of work.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a surface mine safety patrols and examines monitoring unmanned aerial vehicle to the problem of the comparatively complicated efficiency that influences work of dismouting of the efficiency of unmanned aerial vehicle, fuselage and horn is cleared up influence impurity in the unable automation that provides in solving above-mentioned background art.

In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an open mine safety inspection monitoring unmanned aerial vehicle, includes fuselage, horn and fender bracket, the side surface of fuselage runs through installs the horn, and the one end of horn is fixed with the motor to the flabellum is installed to the output of motor, be connected with the slider in the cavity of fuselage side surface, and be connected with the auto-lock piece in the cavity of fuselage to the inner wall of fuselage cavity is fixed with the blotter, the surface of horn runs through installs the unlocking piece, the lower fixed surface of fuselage has the camera, the upper surface of fuselage is connected with the battery, and the upper surface of fuselage runs through installs the fender bracket to the side surface of fender bracket is fixed with the rubber backplate, the side surface of fuselage upper end runs through installs the cardboard, the side surface of fender bracket is connected with little impeller, and the upper end of fender bracket is provided with the mounting bracket to be connected with the half-gear between the upper surface of fender bracket and the top surface of mounting bracket cavity, be connected with the mounting bracket between the upper surface of fender bracket and the top surface of driving bracket cavity, and the both ends of driving bracket are connected with clean brush board through the elasticity rope to the both ends of clean brush board and the surface sliding connection of fender bracket, the surface of clean brush board and the surface of fender bracket are provided with the opening.

Preferably, the fuselage constitutes the block with the horn and is connected, and fuselage and slider constitution sliding connection to be connected with the spring between fuselage and the slider.

By adopting the technical scheme, the machine arm extends into the machine body and then pushes the sliding block and compresses the spring.

Preferably, from the locking piece and the fuselage constitution sliding connection, and be connected with the spring between locking piece and the fuselage to the upper end of locking piece is the arc design, the unlocking piece constitutes sliding connection with the horn, and is connected with the spring between unlocking piece and the horn.

By adopting the technical scheme, the machine arm extends into the machine body and then pushes the sliding block, so that the self-locking block is pushed by the spring to rise and extend into the groove of the machine arm.

Preferably, the inner wall of the cavity of the protection frame is provided with a protrusion, the inner surface of the rubber protection plate is attached to the surface of the machine body, one end of the clamping plate penetrates through the inner wall of the cavity of the protection frame, the clamping plate and the machine body form sliding connection, and a spring is connected between the clamping plate and the machine body.

Adopt above-mentioned technical scheme, promote the one end of cardboard and make its slip and compression spring for the other end of cardboard is kept away from the fender bracket and is carried out the unblock.

Preferably, the small impeller is respectively connected with the protection frame and the mounting frame in a rotating mode, a belt is arranged between the surface of the rotating shaft at the upper end of the small impeller and the surface of the rotating shaft at the upper end of the half gear, and the half gear is respectively connected with the protection frame and the mounting frame in a rotating mode.

By adopting the technical scheme, the small impeller is driven by wind to rotate relative to the protective frame and the mounting frame, and the small impeller drives the half gear to rotate through the belt.

Preferably, the inner wall of driving plate cavity is fixed with the tooth piece, and the driving plate constitutes the meshing with the semi-gear and is connected, the upper surface of fender bracket is provided with the gyro wheel, be connected with the spring between the arch at cleaning brush board both ends and the surface of fender bracket.

By adopting the technical scheme, the semi-gear rotates and then drives the transmission plate to slide through the tooth block, so that the transmission plate drives the cleaning brush plate to slide.

Compared with the prior art, the beneficial effects of the utility model are that: this surface mine safety patrols and examines monitoring unmanned aerial vehicle:

1. the small impeller and the transmission plate are arranged, so that the device drives the half gear to rotate through the rotation of the small impeller, the half gear drives the transmission plate to slide in a reciprocating manner through the tooth block, and the cleaning brush plate is driven to clean the filter screen on the surface of the protective frame, the purpose of automatic cleaning is achieved, the device is beneficial to reducing impurities and pushing the impurities on the surface of the filter screen, and the flying efficiency of the device is ensured;

2. the device is provided with the self-locking block and the sliding block, so that the device is inserted into the machine arm to push the sliding block to slide, the self-locking block rises to be clamped into the groove of the machine arm for fixing, and then the self-locking block is pushed to be quickly unlocked by pressing the unlocking block, so that the time for workers to disassemble and assemble the machine arm is reduced, and the working efficiency is improved;

3. be provided with blotter and rubber backplate, make this device improve the leakproofness of this device through rubber backplate, reduce the probability that external impurity got into power supply mechanism, through the surface of blotter extrusion laminating horn, cushion the vibrations that the horn produced, improve the fastening of the stable increase horn of this device.

Drawings

FIG. 1 is a schematic overall front sectional view of the present invention;

FIG. 2 is a schematic view of the overall sectional view of the present invention;

FIG. 3 is a schematic side sectional view of the present invention;

fig. 4 is the schematic view of the sectional structure of the body and the battery.

In the figure: 1. a body; 2. a boom; 3. a motor; 4. a fan blade; 5. a slider; 6. a self-locking block; 7. a cushion pad; 8. unlocking the block; 9. a camera; 10. a storage battery; 11. a protection frame; 12. a rubber guard plate; 13. clamping a plate; 14. a small impeller; 15. a mounting frame; 16. a half gear; 17. a drive plate; 18. and cleaning the brush plate.

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. 1-4, the present invention provides a technical solution: the utility model provides an open mine safety inspection monitoring unmanned aerial vehicle, including fuselage 1, horn 2, motor 3, flabellum 4, slider 5, from locking piece 6, blotter 7, unblock piece 8, camera 9, battery 10, fender bracket 11, rubber backplate 12, cardboard 13, little impeller 14, mounting bracket 15, semi-gear 16, driving plate 17 and cleaning brush board 18, the side surface of fuselage 1 runs through and installs horn 2, and the one end of horn 2 is fixed with motor 3, and flabellum 4 is installed to motor 3's output, fuselage 1 constitutes the block with horn 2 and is connected, and fuselage 1 constitutes sliding connection with slider 5, and be connected with the spring between fuselage 1 and the slider 5, when using this device, at first make it drive flabellum 4 to rotate through the power supply of battery 10 to motor 3 and fly, rethread camera 9 patrols safely the mine field, blotter 7 of fuselage 1 cavity inner wall will extrude the surface of laminating horn 2, cushion when improving the fastening and reduce the damage.

Be connected with slider 5 in the cavity of 1 side surface of fuselage, and be connected with from locking piece 6 in the cavity of fuselage 1, and the inner wall of 1 cavity of fuselage is fixed with blotter 7, the surface through mounting of horn 2 has unlocking piece 8, the lower fixed surface of fuselage 1 has camera 9, from locking piece 6 and fuselage 1 constitution sliding connection, and be connected with the spring between locking piece 6 and the fuselage 1, and the upper end from locking piece 6 is the arc design, unlocking piece 8 and horn 2 constitute sliding connection, and be connected with the spring between unlocking piece 8 and the horn 2, when the horn 2 is dismantled to needs, press the one end of unlocking piece 8 and make its gliding and compression spring, make the other end of unlocking piece 8 promote from locking piece 6 gliding, make from locking piece 6 no longer with the recess block of horn 2, take horn 2 out afterwards, make slider 5 slide under the promotion of spring again, the internal surface of slider 5 will support and carry out spacing waiting for next time installation to it at the upper surface of self-locking piece 6.

The upper surface of fuselage 1 is connected with battery 10, and the upper surface of fuselage 1 runs through and installs fender bracket 11, and the side surface of fender bracket 11 is fixed with rubber backplate 12, the side surface of fuselage 1 upper end runs through and installs cardboard 13, the inner wall of fender bracket 11 cavity is provided with the arch, the surface of the internal surface laminating fuselage 1 of rubber backplate 12, the inner wall of fender bracket 11 cavity is run through to the one end of cardboard 13, and cardboard 13 and fuselage 1 constitute sliding connection, and be connected with the spring between cardboard 13 and the fuselage 1, when needing to be changed battery 10, press down the one end of cardboard 13, drive the slip of cardboard 13 and compression spring, make the recess that fender bracket 11 cavity inner wall was kept away from to the other end of cardboard 13 unblock, take fender bracket 11 to change battery 10 this moment, when this device is worked, the air drives inside hot-air through the bellied inner wall of fender bracket 11 behind the filter screen of fender bracket 11, improve the heat dispersion of this device.

Side surface of fender bracket 11 is connected with little impeller 14, and the upper end of fender bracket 11 is provided with mounting bracket 15, and be connected with half-gear 16 between the upper surface of fender bracket 11 and the top surface of the 15 cavitys of mounting bracket, little impeller 14 constitutes to rotate with fender bracket 11 and mounting bracket 15 respectively and is connected, and be provided with the belt between the surface of 14 upper ends pivots of little impeller and half-gear 16 upper end pivots, half-gear 16 constitutes to rotate with fender bracket 11 and mounting bracket 15 respectively and is connected, at this device during operation, the direction that the air advances from this device blows to little impeller 14, the air carries out air inlet and air-out from the opening on 11 surfaces of fender bracket at little impeller 14 both ends, make the air drive little impeller 14 rotate, make little impeller 14 drive half-gear 16 through the belt and rotate.

A transmission plate 17 is connected between the upper surface of the protection frame 11 and the top surface of the cavity of the mounting frame 15, two ends of the transmission plate 17 are connected with cleaning brush plates 18 through elastic ropes, two ends of the cleaning brush plates 18 are connected with the surface of the protection frame 11 in a sliding manner, openings are formed in the surfaces of two ends of the small impeller 14 of the protection frame 11, tooth blocks are fixed on the inner wall of the cavity of the transmission plate 17, the transmission plate 17 is meshed with the half gear 16 to be connected, rollers are arranged on the upper surface of the protection frame 11, springs are connected between bulges at two ends of the cleaning brush plates 18 and the surface of the protection frame 11, the transmission plate 17 is driven to slide through the tooth blocks after the half gear 16 rotates, after the half gear 16 rotates for a half circle, the tooth blocks of the half gear 16 are driven to the tooth blocks at the other inner wall of the cavity of the transmission plate 17 to drive the transmission plate 17 to slide reversely, so that the purpose of reciprocating sliding of the transmission plate 17 is achieved, the cleaning brush plates 18 are pulled to slide relative to the surface of the protection frame 11 by the elastic ropes at two ends of the transmission plate 17, the surface of the protection frame 11 is cleaned by the cleaning brush plates 18, and the cleaning brush plates 17, and the surface of the protection frame is not pulled by the springs when the cleaning brush plates 17, and the surface of the cleaning brush plates 17 is not reset spring, and the cleaning brush plates 17.

The working principle is as follows: when using this surface mine safety to patrol and examine monitoring unmanned aerial vehicle, at first drive flabellum 4 rotation for motor 3 circular telegram through battery 10, the air drives little impeller 14 and rotates when flight, and little impeller 14 passes through the belt and drives the rotation of half gear 16, and half gear 16 drives driving plate 17 reciprocating motion through the tooth piece for driving plate 17 drives cleaning brush board 18 and clears up fender bracket 11, has increased holistic practicality.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a surface mine safety patrols and examines monitoring unmanned aerial vehicle, includes fuselage (1), horn (2) and fender bracket (11), its characterized in that: the side surface of the machine body (1) is provided with a machine arm (2) in a penetrating manner, one end of the machine arm (2) is fixed with a motor (3), a fan blade (4) is installed at the output end of the motor (3), a sliding block (5) is connected into the cavity of the side surface of the machine body (1), a self-locking block (6) is connected into the cavity of the machine body (1), a cushion pad (7) is fixed on the inner wall of the cavity of the machine body (1), an unlocking block (8) is installed on the surface of the machine arm (2) in a penetrating manner, a camera (9) is fixed on the lower surface of the machine body (1), a storage battery (10) is connected onto the upper surface of the machine body (1), a protection frame (11) is installed on the upper surface of the machine body (1) in a penetrating manner, a rubber protection plate (12) is fixed onto the side surface of the protection frame (11), a clamping plate (13) is installed on the side surface of the upper end of the machine body (1) in a penetrating manner, a small impeller (14) is connected onto the side surface of the protection frame (11), an installation frame (15) is provided with an installation frame (15), a rope (17) is connected between the upper surface of the transmission plate (11), a semi-gear (16) and a cleaning rope (17) is connected between the upper surface of the transmission plate (17), and the two ends of the cleaning brush plate (18) are connected with the surface of the protective frame (11) in a sliding way, and the surfaces of the protective frame (11) at the two ends of the small impeller (14) are provided with openings.

2. The surface mine safety inspection monitoring unmanned aerial vehicle of claim 1, wherein: fuselage (1) and horn (2) constitute the block and are connected, and fuselage (1) and slider (5) constitute sliding connection to be connected with the spring between fuselage (1) and slider (5).

3. The surface mine safety inspection monitoring unmanned aerial vehicle of claim 1, wherein: from locking piece (6) and fuselage (1) constitution sliding connection, and be connected with the spring between locking piece (6) and fuselage (1) to the upper end of locking piece (6) is the arc design, unlocking piece (8) and horn (2) constitute sliding connection, and are connected with the spring between unlocking piece (8) and horn (2).

4. The safety inspection monitoring unmanned aerial vehicle for surface mines according to claim 1, wherein: the inner wall of fender bracket (11) cavity is provided with the arch, the surface of the internal surface laminating fuselage (1) of rubber backplate (12), the inner wall of fender bracket (11) cavity is run through to the one end of cardboard (13), and cardboard (13) and fuselage (1) constitute sliding connection to be connected with the spring between cardboard (13) and fuselage (1).

5. The surface mine safety inspection monitoring unmanned aerial vehicle of claim 1, wherein: little impeller (14) constitute respectively with fender bracket (11) and mounting bracket (15) and rotate to be connected, and be provided with the belt between the surface of little impeller (14) upper end pivot and the surface of half gear (16) upper end pivot, half gear (16) constitute respectively with fender bracket (11) and mounting bracket (15) and rotate to be connected.

6. The surface mine safety inspection monitoring unmanned aerial vehicle of claim 1, wherein: the inner wall of driving plate (17) cavity is fixed with the tooth piece, and driving plate (17) and semi-gear (16) constitute the meshing and be connected, the upper surface of fender bracket (11) is provided with the gyro wheel, be connected with the spring between the arch at cleaning brush board (18) both ends and the surface of fender bracket (11).