CN213768991U

CN213768991U - Equipment is dodged to high altitude inspection unmanned aerial vehicle danger

Info

Publication number: CN213768991U
Application number: CN202022977550.2U
Authority: CN
Inventors: 黄煜栋; 蔡吸礼; 金文兵
Original assignee: Hangzhou Polytechnic
Current assignee: Hangzhou Polytechnic
Priority date: 2020-12-08
Filing date: 2020-12-08
Publication date: 2021-07-23
Anticipated expiration: 2030-12-08

Abstract

The utility model discloses an unmanned aerial vehicle danger equipment of dodging is tourd in high altitude relates to the unmanned aerial vehicle field, which comprises a mounting bas, the bottom side of mount pad is provided with four damper, four damper's bottom fixed mounting has same transparent protecting crust, rotate on the bottom inner wall of transparent protecting crust and install the pivot, the top fixed mounting of pivot has the carousel. The utility model discloses it is rational in infrastructure, when starting servo motor, can drive ranging module and rotate, and then can 360 degrees automatic measure with the distance of barrier, in time send signal reminds the operator to dodge, can start the rotating electrical machines when dodging, the rotating electrical machines operation can drive the paddle and rotate at a high speed, thereby can promote unmanned aerial vehicle and carry out the quick barrier of dodging, prevent to hit, convenient and practical, when rotating knob, can drive four L shape installation pieces and remove, thereby can install the device on the unmanned aerial vehicle of equidimension not, the practicality of device has been improved.

Description

Equipment is dodged to high altitude inspection unmanned aerial vehicle danger

Technical Field

The utility model relates to an unmanned aerial vehicle field, in particular to high altitude inspection unmanned aerial vehicle danger dodges equipment.

Background

The unmanned aircraft is an unmanned aircraft operated by radio remote control equipment or a self program control device, is widely applied to the fields of military affairs, scientific research and life, can replace ground transportation means at disaster sites such as fire disasters, earthquakes and the like, arrives at places with severe environment to check conditions for rescue, can also carry out data acquisition and exploration in the aspects of weather and space, and can also be used in the aspects of nuclear radiation detection, aerial photography, aviation prospecting, traffic patrol, public security monitoring and the like.

Unmanned aerial vehicle is generally operated unmanned aerial vehicle's flight path by the operator in flight, nevertheless because unmanned aerial vehicle tours the in-process of flight at the high altitude, may meet some barriers, and the operator can be difficult to the actual flight situation of accurate observation unmanned aerial vehicle on ground, leads to unmanned aerial vehicle to hit the barrier easily and cause the damage, for this reason, this application discloses an unmanned aerial vehicle danger avoiding equipment is tourd at the high altitude satisfies people's demand.

SUMMERY OF THE UTILITY MODEL

An object of this application is to provide an unmanned aerial vehicle danger of patrolling in high altitude dodges equipment to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above purpose, the present application provides the following technical solutions: the utility model provides an unmanned aerial vehicle danger equipment of dodging patrols in high altitude, includes the mount pad, the bottom side of mount pad is provided with four damper, four damper's bottom fixed mounting has same transparent protecting crust, rotate on the bottom inner wall of transparent protecting crust and install the pivot, the top fixed mounting of pivot has the carousel, the top side fixed mounting of carousel has ranging module, the bottom of pivot extends to fixed mounting has the rotating electrical machines outside the transparent protecting crust and, the output drive of rotating electrical machines is connected with the paddle, fixed mounting has servo motor and processing module on the bottom inner wall of transparent protecting crust, servo motor passes through linkage subassembly drive carousel and rotates.

Borrow by above-mentioned structure, when starting servo motor, can drive the carousel and range finding module rotates through the linkage subassembly, can 360 degrees automatic measure and the distance of barrier, in time send out signal and remind the operator to dodge, can start the rotating electrical machines when dodging, the rotating electrical machines operation can drive the paddle and rotate at a high speed to can promote unmanned aerial vehicle to carry out quick obstacle of dodging, prevent to hit and fall convenient and practical.

Preferably, the linkage assembly comprises a linkage gear fixedly installed at the output end of the servo motor, a plurality of teeth are uniformly arranged on the peripheral side of the turntable, and the linkage gear is meshed with the teeth.

Further, through the setting of linkage subassembly, can drive the carousel and rotate when starting servo motor, also can carry out the regulation and control of rotational speed simultaneously.

Preferably, the shock-absorbing assembly comprises a fixed sleeve fixedly mounted at the bottom side of the mounting seat, a telescopic column is movably sleeved in the fixed sleeve, and the bottom end of the telescopic column is fixedly mounted on the top side of the transparent protective shell.

Preferably, a damping spring is arranged in the fixed sleeve, and two ends of the damping spring are respectively and fixedly connected with the inner wall of the top of the fixed sleeve and the top end of the telescopic column.

Through damper assembly and damping spring's setting, to the vibration that the device caused when can effectively reducing unmanned aerial vehicle flight, improved the range finding precision and the life of device.

Preferably, a linkage cavity is formed in the mounting seat, a disc is arranged in the linkage cavity, four connecting rods are rotatably mounted on the top side of the disc, a moving rod is rotatably mounted at one end of each connecting rod, and each moving rod extends to the outer portion of the mounting seat and is fixedly provided with an L-shaped mounting piece.

Further, through the setting of disc, connecting rod, carriage release lever and L shape installation piece, can install the device on the unmanned aerial vehicle of equidimension not, improved the practicality of device.

Preferably, a rotating rod is fixedly installed on the bottom side of the disc, and the bottom end of the rotating rod extends out of the installation seat and is fixedly provided with an adjusting knob.

Furthermore, the position of the L-shaped mounting piece can be adjusted through the arrangement of the adjusting knob and the rotating rod, and the L-shaped mounting piece is convenient and labor-saving.

Preferably, two mounting holes are formed in the top sides of the four L-shaped mounting pieces.

Further, through the setting of mounting hole, can be convenient for install fixed mounting on unmanned aerial vehicle.

To sum up, the utility model discloses a technological effect and advantage:

1. the utility model has reasonable structure, when the servo motor is started, the linkage gear can be driven to rotate, the linkage gear can drive the turntable to rotate through a plurality of teeth, the turntable rotates to drive the distance measuring module to rotate, and further the distance between the distance measuring module and an obstacle can be automatically measured by 360 degrees, a signal is sent out in time to remind an operator to avoid, the rotating motor can be started when avoiding, the rotating motor can drive the blades to rotate at high speed, so that the unmanned aerial vehicle can be pushed to quickly avoid the obstacle, the collision is prevented, and the device is convenient and practical;

2. the utility model discloses in, through damping spring's setting, to the vibration that the device caused when can effectively reducing unmanned aerial vehicle flight, improved the range finding precision and the life of device, when rotating adjust knob, can drive the disc through the bull stick and rotate, the disc rotates and drives four connecting rods and rotate, and then can drive four carriage release levers and four L shape installation pieces and remove to can install the device on the unmanned aerial vehicle of equidimension not, improve the practicality of device.

Drawings

In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative efforts.

Fig. 1 is a schematic perspective view of an embodiment of the present application;

FIG. 2 is a schematic diagram of an internal structure of a transparent protective shell according to an embodiment of the present application;

FIG. 3 is a schematic cross-sectional front view of an embodiment of the present application;

FIG. 4 is a partially enlarged view of FIG. 3;

fig. 5 is a schematic top view cross-sectional structure of an embodiment of the present application.

In the figure: 1. a mounting seat; 2. a transparent protective shell; 3. a servo motor; 4. a rotating shaft; 5. a turntable; 6. a distance measurement module; 7. a rotating electric machine; 8. a paddle; 9. a processing module; 10. a linkage gear; 11. fixing the sleeve; 12. a telescopic column; 13. a damping spring; 14. a disc; 15. a connecting rod; 16. a travel bar; 17. an L-shaped mounting tab; 18. and adjusting a knob.

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.

Example (b): referring to fig. 1-5, the high altitude patrol unmanned aerial vehicle danger avoiding device comprises a mounting base 1, wherein the mounting base 1 can be any one of the existing base structures, such as a metal plate. The bottom side of mount pad 1 is provided with four damper, and four damper's bottom fixed mounting has same transparent protecting crust 2, and transparent protecting crust 2 can be any one kind of transparent casing that has now, for example ya keli transparent shell. Rotate on the bottom inner wall of transparent protecting crust 2 and install pivot 4, the top fixed mounting of pivot 4 has carousel 5, the top side fixed mounting of carousel 5 has ranging module 6, the bottom of pivot 4 extends to transparent protecting crust 2 outer and fixed mounting has rotating electrical machines 7, the output drive of rotating electrical machines 7 is connected with paddle 8, fixed mounting has servo motor 3 and processing module 9 on the bottom inner wall of transparent protecting crust 2, servo motor 3 drives carousel 5 through the linkage subassembly and rotates.

Borrow by above-mentioned structure, when starting servo motor 3, can drive carousel 5 and ranging module 6 through the linkage subassembly and rotate, can 360 degrees automatic measure and the distance of barrier, in time send out signal and remind the operator to dodge, can start rotating electrical machines 7 when dodging, rotating electrical machines 7 operation can drive 8 high-speed rotations of paddle to can promote unmanned aerial vehicle to carry out quick barrier of dodging, prevent to hit and fall convenient and practical.

As a preferred embodiment of the present embodiment, the linkage assembly includes a linkage gear 10 fixedly installed at an output end of the servo motor 3, a plurality of teeth are uniformly arranged on a peripheral side of the turntable 5, and the linkage gear 10 is engaged with the plurality of teeth. The advantage that sets up like this is, when servo motor 3 moves, can drive linkage gear 10 and rotate, and linkage gear 10 rotates and can drive carousel 5 through a plurality of teeth and rotate, also can carry out the regulation and control of rotational speed simultaneously.

As a preferred embodiment of the present embodiment, the shock-absorbing assembly comprises a fixed sleeve 11 fixedly mounted on the bottom side of the mounting base 1, a telescopic column 12 is movably sleeved in the fixed sleeve 11, and the bottom end of the telescopic column 12 is fixedly mounted on the top side of the transparent protective shell 2. The benefit of setting up like this is, when unmanned aerial vehicle flight produces vibrations, can make flexible post 12 reciprocate in fixed sleeve 11, avoids rigid connection to take place synchronous oscillation.

As a preferred embodiment of this embodiment, a damping spring 13 is disposed in the fixed sleeve 11, and both ends of the damping spring 13 are fixedly connected to the top inner wall of the fixed sleeve 11 and the top end of the telescopic column 12, respectively. The benefit that sets up like this is, under damping spring 13's elasticity effect, to the vibration that the device caused when can effectively reducing unmanned aerial vehicle flight, has improved the range finding precision and the life of device.

As a preferred embodiment of the present embodiment, a linkage cavity is formed in the mounting base 1, a disk 14 is disposed in the linkage cavity, four connecting rods 15 are rotatably mounted on the top side of the disk 14, a moving rod 16 is rotatably mounted at one end of each of the four connecting rods 15, and one end of each of the four moving rods 16 extends out of the mounting base 1 and is fixedly mounted with an L-shaped mounting piece 17. The benefit that sets up like this is, when disc 14 rotates, can drive four connecting rods 15 and rotate, and then can drive four carriage release levers 16 and four L shape installation pieces 17 and remove to can install the device on the unmanned aerial vehicle of equidimension not, improve the practicality of device.

As a preferred embodiment of the present embodiment, a rotating rod is fixedly mounted on the bottom side of the disc 14, and the bottom end of the rotating rod extends out of the mounting base 1 and is fixedly mounted with an adjusting knob 18. This has the advantage that when the adjustment knob 18 is turned, the disc 14 is rotated by the turning bar, and the position of the L-shaped mounting piece 17 can be adjusted.

As a preferred embodiment of the present embodiment, two mounting holes are opened on the top sides of the four L-shaped mounting pieces 17. The benefit of setting up like this is, can be convenient for with device fixed mounting on unmanned aerial vehicle.

This practical theory of operation:

when starting servo motor 3, can drive linkage gear 10 and rotate, linkage gear 10 rotates and can drive carousel 5 through a plurality of tooth and rotate, carousel 5 rotates and drives ranging module 6 and rotates, and then can 360 degrees automatic measure and the distance of barrier, in time signals remind the operator to dodge, can start rotating electrical machines 7 when dodging, rotating electrical machines 7 operation can drive 8 high-speed rotations of paddle, thereby can promote unmanned aerial vehicle to carry out quick barrier of dodging, prevent to hit, convenient and practical.

Through damping spring 13's setting, can effectively reduce the vibration that causes the device when unmanned aerial vehicle flies, improved the range finding precision and the life of device, when rotating adjust knob 18, can drive disc 14 through the bull stick and rotate, disc 14 rotates and drives four connecting rods 15 and rotate, and then can drive four movable rods 16 and four L shape installation pieces 17 and remove to can install the device on the unmanned aerial vehicle of equidimension not, improve the practicality of device.

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 an equipment is dodged to high altitude inspection unmanned aerial vehicle danger, includes mount pad (1), its characterized in that: the utility model discloses a solar energy remote monitoring device, including mount pad (1), bottom side of mount pad (1) is provided with four damper, four damper's bottom fixed mounting has same transparent protecting crust (2), rotate on the bottom inner wall of transparent protecting crust (2) and install pivot (4), the top fixed mounting of pivot (4) has carousel (5), the top side fixed mounting of carousel (5) has ranging module (6), the bottom of pivot (4) extends to transparent protecting crust (2) are outer and fixed mounting has rotating electrical machines (7), the output drive of rotating electrical machines (7) is connected with paddle (8), fixed mounting has servo motor (3) and processing module (9) on the bottom inner wall of transparent protecting crust (2), servo motor (3) rotate through linkage subassembly drive carousel (5).

2. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 1, characterized in that: the linkage assembly comprises a linkage gear (10) fixedly installed at the output end of the servo motor (3), a plurality of teeth are uniformly arranged on the peripheral side of the turntable (5), and the linkage gear (10) is meshed with the teeth.

3. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 1, characterized in that: the damping assembly comprises a fixed sleeve (11) fixedly installed on the bottom side of the installation base (1), a telescopic column (12) is movably sleeved in the fixed sleeve (11), and the bottom end of the telescopic column (12) is fixedly installed on the top side of the transparent protection shell (2).

4. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 3, wherein: the damping device is characterized in that a damping spring (13) is arranged in the fixed sleeve (11), and two ends of the damping spring (13) are fixedly connected with the inner wall of the top of the fixed sleeve (11) and the top end of the telescopic column (12) respectively.

5. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 1, characterized in that: linkage chamber has been seted up in mount pad (1), the linkage intracavity is provided with disc (14), four connecting rods (15), four are installed in the top side rotation of disc (14) the one end of connecting rod (15) is all rotated and is installed carriage release lever (16), four the one end of carriage release lever (16) all extends to mount pad (1) is outer and fixed mounting has L shape installation piece (17).

6. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 5, wherein: the bottom side of the disc (14) is fixedly provided with a rotating rod, and the bottom end of the rotating rod extends out of the mounting base (1) and is fixedly provided with an adjusting knob (18).

7. The high altitude patrol unmanned aerial vehicle danger avoiding equipment according to claim 5, wherein: two mounting holes are formed in the top sides of the four L-shaped mounting pieces (17).