CN211996188U

CN211996188U - Stabilizing structure of unmanned aerial vehicle cloud platform

Info

Publication number: CN211996188U
Application number: CN201922116455.0U
Authority: CN
Inventors: 李明; 刘波
Original assignee: Shenzhen Kaidafeng Precision Metal Products Co ltd
Current assignee: Shenzhen Kaidafeng Precision Metal Products Co ltd
Priority date: 2019-11-28
Filing date: 2019-11-28
Publication date: 2020-11-24
Anticipated expiration: 2029-11-28

Abstract

The utility model discloses an unmanned aerial vehicle cloud platform stable structure, including the base, fixed mounting has the gasbag on the base, and fixed mounting has the supporting seat on the gasbag, and fixed mounting has the barrel on the base, and fixed mounting has the bracing piece on the supporting seat, and the bracing piece slides with the barrel and sets up, is provided with the spacing groove in the barrel, and fixed mounting has the stopper on the bracing piece, and stopper and spacing groove slide and set up, are provided with the plate groove on the supporting seat, and the plate inslot slides and is provided with the linkage plate, and fixed mounting has the cloud platform body on. Adopt the gasbag structure, compare traditional spring shock attenuation, at aerial more stable, can not be like the spring, when receiving the air current interference, just rock, and the gasbag when unmanned aerial vehicle descends, through inside gaseous compression, can provide sufficient shock attenuation effect, barrel and bracing piece can ensure that the shock attenuation direction is vertical direction, when stopper and spacing groove can prevent the shock attenuation, the condition of breaking away appears in base and supporting seat.

Description

Stabilizing structure of unmanned aerial vehicle cloud platform

Technical Field

The utility model relates to an unmanned aerial vehicle cloud platform technical field specifically is a stable structure of unmanned aerial vehicle cloud platform.

Background

The stability of unmanned aerial vehicle cloud platform self structure is the important performance index of cloud platform performance, and it is directly influencing the steady image effect of cloud platform, and reasonable stable cloud platform structure has very big effect to improving unmanned aerial vehicle operation performance.

Present cloud platform structure is comparatively perfect, can guarantee when receiving air current or vibrations influence, and the camera is stable shooting as far as, but when no man descends, can produce the collision with ground, and this kind of collision has surpassed the shock attenuation scope of cloud platform itself, so need add shock-absorbing structure in addition to guarantee that when unmanned aerial vehicle descends, the camera has sufficient buffer capacity.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a stable structure of unmanned aerial vehicle cloud platform to solve unmanned aerial vehicle shock attenuation protection problem to the camera when descending.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle cloud platform stable structure, includes the base, fixed mounting has the gasbag on the base, fixed mounting has the supporting seat on the gasbag, fixed mounting has the barrel on the base, fixed mounting has the bracing piece on the supporting seat, the bracing piece slides with the barrel and sets up, be provided with the spacing groove in the barrel, fixed mounting has the stopper on the bracing piece, the stopper slides with the spacing groove and sets up, be provided with the board groove on the supporting seat, the board inslot slides and is provided with the linking plate, fixed mounting has the cloud platform body on the linking plate.

Preferably, the two sides of the supporting seat are provided with inner cavities, and the inner wall of each inner cavity is fixedly embedded with a threaded sleeve and a square sleeve.

Preferably, the thread of the threaded sleeve is internally provided with a threaded knob.

Preferably, a square block is arranged in the square sleeve in a sliding mode, a square groove is formed in the connecting plate, and the square block and the square groove are arranged in a sliding mode.

Preferably, the square block is provided with a rotating groove, the threaded knob is fixedly provided with a rotating block, and the rotating block and the rotating groove are rotatably arranged.

Preferably, the inner cavity is internally and fixedly provided with a limiting rod, the limiting rod is provided with a limiting sleeve in a sliding manner, and the limiting sleeve is connected with the square block through a support.

Preferably, the base is fixedly provided with a side plate, and the side plate is provided with a built-in hole.

Compared with the prior art, the beneficial effects of the utility model are that: the air bag structure is adopted, compared with the traditional spring shock absorption, the air bag structure is more stable in the air, can not shake like a spring when being disturbed by air flow, and can provide enough shock absorption effect through the compression of internal gas when the unmanned aerial vehicle lands;

the barrel and the supporting rod can ensure that the damping direction is vertical, and when the limiting block and the limiting groove can prevent damping, the base and the supporting seat are disengaged.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a partially enlarged schematic view of the barrel and the support rod of the present invention;

fig. 3 is an enlarged schematic view of the inner cavity structure of the present invention.

In the figure: 1. a base; 11. an air bag; 12. a supporting seat; 13. a barrel; 14. a support bar; 15. a limiting groove; 16. a limiting block; 17. a plate groove; 18. a connector tile; 19. the holder body; 2. an inner cavity; 21. a threaded sleeve; 22. a square sleeve; 23. a threaded knob; 24. a square block; 25. a rotating groove; 26. rotating the block; 3. a square groove; 4. a limiting rod; 41. a limiting sleeve; 5. a side plate; 51. a hole is arranged inside.

Detailed Description

Referring to fig. 1 and fig. 2, the present invention provides a technical solution: the utility model provides a stable structure of unmanned aerial vehicle cloud platform, the on-line screen storage device comprises a base 1, fixed mounting has gasbag 11 on the base 1, fixed mounting has supporting seat 12 on the gasbag 11, fixed mounting has barrel 13 on the base 1, fixed mounting has bracing piece 14 on the supporting seat 12, bracing piece 14 slides with barrel 13 and sets up, be provided with spacing groove 15 in the barrel 13, fixed mounting has stopper 16 on the bracing piece 14, stopper 16 slides with spacing groove 15 and sets up, be provided with board groove 17 on the supporting seat 12, it is provided with joint board 18 to slide in board groove 17, fixed mounting has cloud platform body 19 on the joint board 18.

Referring to fig. 1 and 3, the inner cavity 2 is disposed on both sides of the supporting seat 12, and a threaded sleeve 21 and a square sleeve 22 are fixedly embedded in the inner wall of the inner cavity 2.

Referring to fig. 1 and 3, the threaded knob 23 is disposed in the threaded sleeve 21, and compared with a bolt which can be manually installed without a tool, the threaded sleeve 21 and the threaded knob 23 are made of stainless steel.

Referring to fig. 1 and 3, the square sleeve 22 is slidably provided with a square block 24, the connecting plate 18 is provided with a square groove 3, and the square block 24 is slidably provided with the square groove 3.

Referring to fig. 1 and 3, square block 24 is last to be provided with and to rotate groove 25, and fixed mounting has turning block 26 on the screw knob 23, and turning block 26 rotates with rotation groove 25 and sets up, and square block 24, turning block 26, gag lever post 4 and stop collar 41 are made by plastic material, reduce screw thread pivoted distance, and simultaneously, also guarantee the stability of cloud platform body 19 installation, simultaneously, can not increase the burden for unmanned aerial vehicle flight.

Referring to fig. 1 and 3, a limiting rod 4 is fixedly installed in the inner cavity 2, a limiting sleeve 41 is slidably arranged on the limiting rod 4, and the limiting sleeve 41 is connected with the square block 24 through a bracket.

Referring to fig. 1, fixed mounting has sideboard 5 on the base 1, is provided with built-in hole 51 on sideboard 5, and the base 1 of being convenient for is fixed with unmanned aerial vehicle, and base 1 and supporting seat 12 are made by high strength light plastic material, can not cause unmanned aerial vehicle's flight burden.

The utility model discloses when concrete implementation: when the holder body 19 needs to be disassembled and overhauled, the threaded knob 23 is rotated to generate threaded displacement with the threaded sleeve 21, the rotating block 26 rotates in the rotating groove 25 to ensure that the square block 24 can move, the limiting sleeve 41 slides on the limiting rod 4 to ensure that the square block 24 cannot rotate after being pushed into the inner cavity 2, and the connecting plate 18 is separated from the plate groove 17 after the square block 24 is separated from the square groove 3, so that the disassembly and overhaul of the holder body 19 are completed;

when the shock attenuation is descended to needs, through the gas compression in the gasbag 11 for cloud platform body 19 has a buffering effect when descending, and barrel 13 and bracing piece 14 relative slip can have a spacing effect, make the shock attenuation scope for sliding from top to bottom, and stopper 16 slides in spacing groove 15, makes when the shock attenuation, the condition of slippage can not appear.

Claims

1. The utility model provides a stable structure of unmanned aerial vehicle cloud platform, includes base (1), its characterized in that: fixed mounting has gasbag (11) on base (1), fixed mounting has supporting seat (12) on gasbag (11), fixed mounting has barrel (13) on base (1), fixed mounting has bracing piece (14) on supporting seat (12), bracing piece (14) slide with barrel (13) and set up, be provided with spacing groove (15) in barrel (13), fixed mounting has stopper (16) on bracing piece (14), stopper (16) slide with spacing groove (15) and set up, be provided with board groove (17) on supporting seat (12), it is provided with linking plate (18) to slide in board groove (17), fixed mounting has cloud platform body (19) on linking plate (18).

2. The stabilizing structure of an unmanned aerial vehicle holder of claim 1, wherein: both sides of the supporting seat (12) are provided with inner cavities (2), and threaded sleeves (21) and square sleeves (22) are fixedly embedded in the inner walls of the inner cavities (2).

3. The stabilizing structure of an unmanned aerial vehicle holder of claim 2, wherein: the thread knob (23) is arranged in the thread of the thread sleeve (21).

4. The stabilizing structure of an unmanned aerial vehicle holder of claim 3, wherein: the square sleeve (22) is internally provided with a square block (24) in a sliding manner, the connecting plate (18) is provided with a square groove (3), and the square block (24) and the square groove (3) are arranged in a sliding manner.

5. The stabilizing structure of an unmanned aerial vehicle holder of claim 4, wherein: the square block (24) is provided with a rotating groove (25), the thread knob (23) is fixedly provided with a rotating block (26), and the rotating block (26) and the rotating groove (25) are rotatably arranged.

6. The stabilizing structure of an unmanned aerial vehicle holder of claim 4, wherein: the inner cavity (2) is internally and fixedly provided with a limiting rod (4), the limiting rod (4) is provided with a limiting sleeve (41) in a sliding manner, and the limiting sleeve (41) is connected with the square block (24) through a support.

7. The stabilizing structure of an unmanned aerial vehicle holder of claim 1, wherein: the base (1) is fixedly provided with a side plate (5), and the side plate (5) is provided with a built-in hole (51).