CN214383415U

CN214383415U - Unmanned aerial vehicle survey and drawing data acquisition device

Info

Publication number: CN214383415U
Application number: CN202120568813.6U
Authority: CN
Inventors: 信小伟
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-03-19
Filing date: 2021-03-19
Publication date: 2021-10-12
Anticipated expiration: 2031-03-19

Abstract

The utility model discloses an unmanned aerial vehicle surveying and mapping data acquisition device, including the unmanned aerial vehicle body, the center department of unmanned aerial vehicle body bottom is through connecting block fixedly connected with concave frame, the right side fixedly connected with guard box of concave frame, the bottom fixedly connected with servo motor of guard box inner chamber, servo motor's output fixedly connected with pivot, the utility model discloses a set up servo motor and pivot, can drive the camera rotation, adjust the angle of camera, through setting up locating piece, logical groove, push pedal, first pressure spring, gag lever post and spacing hole, can conveniently dismantle the camera, charge and copy data for the camera, through setting up above structure, possess the advantage of conveniently dismantling the camera, solved current unmanned aerial vehicle's camera most all be fixed mounting in the frame, inconvenient camera dismantlement, and the inconvenience is brought to charging and copying data in the camera.

Description

Unmanned aerial vehicle survey and drawing data acquisition device

Technical Field

The utility model relates to a mapping equipment technical field specifically is an unmanned aerial vehicle survey and drawing data acquisition device.

Background

Along with the rapid development of electronic technology, unmanned aerial vehicle is at remote control, the time of endurance, flight quality has had obvious breakthrough, become the new aviation remote sensing means that has risen in recent years, generally thought to have good development prospect by the remote sensing world, people adopt unmanned aerial vehicle to carry out survey and drawing data collection to the topography at present usually, and data collection need use the camera usually, its camera of current unmanned aerial vehicle is mostly fixed mounting in the frame, inconvenient camera is dismantled, bring inconvenience for charging and copying the data in the camera, for this reason we propose an unmanned aerial vehicle survey and drawing data collection system, solve the problem that proposes more than.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle mapping data collection system possesses the advantage that conveniently dismantles the camera, has solved that its camera of current unmanned aerial vehicle is fixed mounting mostly in the frame, and inconvenient camera dismantles, the problem of inconvenience is brought for charging and copying the data in the camera.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle surveying and mapping data acquisition device comprises an unmanned aerial vehicle body, wherein a concave frame is fixedly connected at the center of the bottom of the unmanned aerial vehicle body through a connecting block, a protection box is fixedly connected at the right side of the concave frame, a servo motor is fixedly connected at the bottom of an inner cavity of the protection box, a rotating shaft is fixedly connected at the output end of the servo motor, the left side of the rotating shaft penetrates through the concave frame and is rotatably connected with the left side of the inner cavity of the concave frame through a bearing, a mounting plate is fixedly connected at the bottom of the rotating shaft, a groove is formed in the bottom of the mounting plate, a positioning block is inserted into an inner cavity of the groove, a camera is fixedly connected at the bottom of the positioning block, through grooves are formed in the tops of the left side and the right side of the positioning block, the inner cavity of each through groove is movably connected with a push plate, and first pressure springs are fixedly connected at the tops and bottoms of opposite sides of the two push plates, two one side that first pressure spring is relative and the junction fixed connection who leads to groove inner chamber, two the equal fixedly connected with gag lever post in top of the push pedal back of the body one side mutually, the spacing hole that the cooperation gag lever post used is all seted up to groove inner chamber's the left and right sides, two one side that the gag lever post was carried on the back mutually all runs through logical groove and pegs graft with the internal surface in spacing hole.

Preferably, the equal fixedly connected with landing leg in four corners of unmanned aerial vehicle body bottom, the bottom fixedly connected with sleeve of landing leg, telescopic inner chamber swing joint has the loop bar, the bottom fixedly connected with backup pad of loop bar.

Preferably, the bottom of the push plate is fixedly connected with a sliding block, the bottom of the inner cavity of the through groove is provided with a sliding groove matched with the sliding block for use, and the outer surface of the sliding block is connected with the inner surface of the sliding groove in a sliding mode.

Preferably, the top of the loop bar left and right sides all fixedly connected with guide block, the guide way that the cooperation guide block used is all seted up to the left and right sides of sleeve inner chamber, the surface of guide block and the internal surface sliding connection of guide way.

Preferably, the top of the inner cavity of the sleeve is fixedly connected with a second pressure spring, and the bottom of the second pressure spring is fixedly connected with the top of the sleeve rod.

Preferably, two equal fixedly connected with push rods in the bottom of push pedal one side of the back of the body mutually, two the one side that the push rod carried on the back mutually all runs through logical groove and extends to the outside that leads to the groove.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a set up servo motor and pivot, it is rotatory to drive the camera, adjust the angle of camera, through setting up the locating piece, lead to the groove, the push pedal, a pressure spring, gag lever post and spacing hole, can conveniently dismantle the camera, charge and copy data for the camera, through setting up above structure, possess the advantage that conveniently dismantles the camera, it all is fixed mounting in the frame mostly to have solved current its camera of unmanned aerial vehicle, inconvenient camera dismantles, the problem of inconvenience is brought for charging and copying the data in the camera.

2. The utility model can support the unmanned aerial vehicle body by arranging the supporting legs, the sleeves, the loop bars and the supporting plates;

the sliding block and the sliding groove are arranged, so that the moving of the push plate can be guided, and the moving of the push plate is supported;

the guide block and the guide groove are arranged, so that the movement of the loop bar can be guided, and the movement of the loop bar is limited;

the movement of the loop bar can be buffered by arranging the second pressure spring;

through setting up the push rod, can conveniently promote the push pedal.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a partial enlarged view of the point A in FIG. 1;

FIG. 3 is a partial enlarged view of the point B in the structure of FIG. 1;

fig. 4 is a perspective view of the concave frame structure of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a female frame; 3. a protective box; 4. a servo motor; 5. a rotating shaft; 6. mounting a plate; 7. a groove; 8. positioning blocks; 9. a camera; 10. a through groove; 11. pushing the plate; 12. a first pressure spring; 13. a limiting rod; 14. a limiting hole; 15. a support leg; 16. a sleeve; 17. a loop bar; 18. a support plate; 19. a slider; 20. a chute; 21. a guide block; 22. a guide groove; 23. a second pressure spring; 24. a push rod.

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, an unmanned aerial vehicle surveying and mapping data acquisition device comprises an unmanned aerial vehicle body 1, a concave frame 2 is fixedly connected at the center of the bottom of the unmanned aerial vehicle body 1 through a connecting block, a protection box 3 is fixedly connected at the right side of the concave frame 2, a servo motor 4 is fixedly connected at the bottom of an inner cavity of the protection box 3, a rotating shaft 5 is fixedly connected at the output end of the servo motor 4, the left side of the rotating shaft 5 penetrates through the concave frame 2 and is rotatably connected with the left side of the inner cavity of the concave frame 2 through a bearing, a mounting plate 6 is fixedly connected at the bottom of the rotating shaft 5, a groove 7 is formed at the bottom of the mounting plate 6, a positioning block 8 is inserted into the inner cavity of the groove 7, a camera 9 is fixedly connected at the bottom of the positioning block 8, through grooves 10 are formed at the tops of the left side and the right side of the positioning block 8, push plates 11 are movably connected with push plates 11, and first pressure springs 12 are fixedly connected at the tops and the bottoms of the opposite sides of the two push plates 11, the opposite sides of the two first pressure springs 12 are fixedly connected with the connecting part of the inner cavity of the through groove 10, the tops of the opposite sides of the two push plates 11 are fixedly connected with limit rods 13, the left side and the right side of the inner cavity of the groove 7 are respectively provided with limit holes 14 matched with the limit rods 13 for use, the opposite sides of the two limit rods 13 are respectively penetrated through the through groove 10 and are inserted into the inner surfaces of the limit holes 14, the camera 9 can be driven to rotate by arranging a servo motor 4 and a rotating shaft 5, the angle of the camera 9 can be adjusted, the camera 9 can be conveniently disassembled by arranging a positioning block 8, the through groove 10, the push plates 11, the first pressure springs 12, the limit rods 13 and the limit holes 14, the camera 9 is charged and data can be copied, by arranging the structure, the camera has the advantage of being convenient to disassemble, the problem that most of the existing unmanned aerial vehicle is fixedly installed on a frame and is inconvenient to disassemble the camera, and the inconvenience is brought to charging and copying data in the camera.

Please refer to fig. 1 and 3, the equal fixedly connected with landing leg 15 in four corners of unmanned aerial vehicle body 1 bottom, the bottom fixedly connected with sleeve 16 of landing leg 15, the inner chamber swing joint of sleeve 16 has loop bar 17, and the bottom fixedly connected with backup pad 18 of loop bar 17 can support unmanned aerial vehicle body 1 through setting up landing leg 15, sleeve 16, loop bar 17 and backup pad 18.

Referring to fig. 1 and 2, a sliding block 19 is fixedly connected to the bottom of the pushing plate 11, a sliding groove 20 used in cooperation with the sliding block 19 is formed in the bottom of the inner cavity of the through groove 10, the outer surface of the sliding block 19 is slidably connected with the inner surface of the sliding groove 20, and the sliding block 19 and the sliding groove 20 are arranged to guide the movement of the pushing plate 11 and support the movement of the pushing plate 11.

Referring to fig. 1 and 3, the top of the left side and the top of the right side of the loop bar 17 are fixedly connected with guide blocks 21, the left side and the right side of the inner cavity of the sleeve 16 are respectively provided with guide grooves 22 matched with the guide blocks 21, the outer surface of each guide block 21 is slidably connected with the inner surface of each guide groove 22, and the guide blocks 21 and the guide grooves 22 are arranged to guide the movement of the loop bar 17 and limit the movement of the loop bar 17.

Referring to fig. 1 and 3, a second compression spring 23 is fixedly connected to the top of the inner cavity of the sleeve 16, the bottom of the second compression spring 23 is fixedly connected to the top of the loop bar 17, and the movement of the loop bar 17 can be buffered by the arrangement of the second compression spring 23.

Referring to fig. 1, 2 and 4, push rods 24 are fixedly connected to the bottoms of the two push plates 11 on the opposite sides, the two push rods 24 on the opposite sides penetrate through the through groove 10 and extend to the outer side of the through groove 10, and the push plates 11 can be conveniently pushed by arranging the push rods 24.

When the unmanned aerial vehicle is used, when the angle of the camera 9 needs to be adjusted when the unmanned aerial vehicle body 1 flies, the peripheral switch of the servo motor 4 is started, the servo motor 4 is enabled to rotate, the servo motor 4 drives the rotating shaft 5 to rotate, the rotating shaft 5 drives the mounting plate 6 to rotate, the mounting plate 6 drives the camera 9 to rotate, the angle of the camera 9 is adjusted, when the unmanned aerial vehicle body 1 lands, the supporting plate 18 is firstly contacted with the ground, the sleeve rod 17 is driven to move upwards on the inner surface of the sleeve 16 through the reaction force, the movement of the sleeve rod 17 is buffered through the action of the second pressure spring 23, the unmanned aerial vehicle body 1 is further buffered, when the camera 9 needs to be disassembled, the push rod 24 is pressed, the push rod 24 is enabled to move towards the middle, the push rod 24 drives the push plate 11 to move towards the middle through the guide of the sliding block 19 and the sliding groove 20, the push plate 11 drives the limit rod 13 to move towards the middle, make gag lever post 13 break away from spacing hole 14, take off camera 9, through setting up above structure, possess the advantage that the convenience was dismantled to the camera, solved that its camera of current unmanned aerial vehicle is mostly fixed mounting in the frame, inconvenient camera dismantlement gets off, brings inconvenient problem for charging and the data of copying in the camera.

The control mode of the present application is automatically controlled by a controller, the control circuit of the controller can be realized by simple programming by those skilled in the art, and the present application is common knowledge in the field, and the present application mainly protects the mechanical device, so the control mode and the circuit connection are not explained in detail in the present application.

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 an unmanned aerial vehicle survey and drawing data collection system, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that a concave frame (2) is fixedly connected at the center of the bottom of an unmanned aerial vehicle body (1) through a connecting block, a protective box (3) is fixedly connected on the right side of the concave frame (2), a servo motor (4) is fixedly connected at the bottom of an inner cavity of the protective box (3), a rotating shaft (5) is fixedly connected at the output end of the servo motor (4), the left side of the rotating shaft (5) penetrates through the concave frame (2) and is rotatably connected with the left side of the inner cavity of the concave frame (2) through a bearing, a mounting plate (6) is fixedly connected at the bottom of the rotating shaft (5), a groove (7) is formed at the bottom of the mounting plate (6), a positioning block (8) is inserted into an inner cavity of the groove (7), a camera (9) is fixedly connected at the bottom of the positioning block (8), through grooves (10) are formed at the tops of the left side and the right side of the positioning block (8), and a push plate (11) is movably connected with an inner cavity of the through groove (10), two the top and the first pressure spring of the equal fixedly connected with in bottom (12), two of one side that push pedal (11) is relative one side and the junction fixed connection who leads to groove (10) inner chamber, two push pedal (11) back of the body the equal fixedly connected with gag lever post (13) in top of one side that backs on the back, spacing hole (14) that cooperation gag lever post (13) used are all seted up to the left and right sides of recess (7) inner chamber, two one side that gag lever post (13) carried on the back mutually all runs through logical groove (10) and pegs graft with the internal surface in spacing hole (14).

2. The unmanned aerial vehicle mapping data collection system of claim 1, wherein: the equal fixedly connected with landing leg (15) in four corners of unmanned aerial vehicle body (1) bottom, the bottom fixedly connected with sleeve (16) of landing leg (15), the inner chamber swing joint of sleeve (16) has loop bar (17), the bottom fixedly connected with backup pad (18) of loop bar (17).

3. The unmanned aerial vehicle mapping data collection system of claim 1, wherein: the bottom fixedly connected with slider (19) of push pedal (11), spout (20) that cooperation slider (19) used are seted up to the bottom of logical groove (10) inner chamber, the surface of slider (19) and the internal surface sliding connection of spout (20).

4. The unmanned aerial vehicle mapping data collection system of claim 2, wherein: the equal fixedly connected with guide block (21) in top of loop bar (17) left and right sides, guide way (22) that cooperation guide block (21) used are all seted up to the left and right sides of sleeve (16) inner chamber, the surface of guide block (21) and the internal surface sliding connection of guide way (22).

5. The unmanned aerial vehicle mapping data collection system of claim 2, wherein: the top of the inner cavity of the sleeve (16) is fixedly connected with a second pressure spring (23), and the bottom of the second pressure spring (23) is fixedly connected with the top of the loop bar (17).

6. The unmanned aerial vehicle mapping data collection system of claim 1, wherein: two equal fixedly connected with push rod (24) in the bottom of push pedal (11) one side that backs on the back, two one side that push rod (24) carried on the back all runs through logical groove (10) and extends to the outside that leads to groove (10).