CN214356647U

CN214356647U - Take shock absorber support's unmanned aerial vehicle

Info

Publication number: CN214356647U
Application number: CN202021339079.8U
Authority: CN
Inventors: 植雅芳
Original assignee: Guangzhou College of Technology and Business
Current assignee: Guangzhou College of Technology and Business
Priority date: 2020-07-09
Filing date: 2020-07-09
Publication date: 2021-10-08
Anticipated expiration: 2030-07-09

Abstract

The utility model provides an unmanned aerial vehicle with a damping support, which comprises an unmanned aerial vehicle body, wherein four corners of the outer side of the unmanned aerial vehicle body are provided with first chutes, folding support structures can be detachably connected in the first chutes, and pneumatic damping structures are arranged above the folding support structures; unmanned aerial vehicle body outside encircles its week and is equipped with a plurality of shock attenuation strips, just unmanned aerial vehicle body center is equipped with first connecting hole, the couple structure can be dismantled in first connecting hole, first connecting hole all around can dismantle four batteries of connection on the unmanned aerial vehicle body, four batteries supply to rotate for the fan and provide the electric energy. The utility model discloses a pneumatic shock-absorbing structure realizes the shock attenuation effect from top to bottom, utilizes the shock attenuation effect that the side was realized to the shock attenuation strip.

Description

Take shock absorber support's unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field mainly relates to a take shock absorber support's unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

The rotation of current unmanned aerial vehicle through a plurality of fans provides ascending lift to the realization upwards flies.

However, because current unmanned aerial vehicle outer surface shell is made for plastics, and owing to for perpendicular decline when the aircraft descends to have certain dive power downwards, if do not have shock absorber support, both caused the technical problem of unmanned aerial vehicle's damage easily.

SUMMERY OF THE UTILITY MODEL

The utility model provides a take shock absorber support's unmanned aerial vehicle is used for solving providing in the background art because current unmanned aerial vehicle exine shell is made for plastics, and owing to descend for perpendicular when the aircraft descends to have certain dive power downwards, if there is not shock absorber support, both caused the technical problem of unmanned aerial vehicle's damage easily.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle with a shock absorption support comprises an unmanned aerial vehicle body, wherein four corners of the outer side of the unmanned aerial vehicle body are provided with first sliding grooves, a folding supporting structure is detachably connected in the first sliding grooves, and a pneumatic shock absorption structure is arranged above the folding supporting structure;

unmanned aerial vehicle body outside encircles its week and is equipped with a plurality of shock attenuation strips, just unmanned aerial vehicle body center is equipped with first connecting hole, the couple structure can be dismantled in first connecting hole, first connecting hole all around can dismantle four batteries of connection on the unmanned aerial vehicle body, four batteries supply to rotate for the fan and provide the electric energy.

Furthermore, folding bearing structure includes first connecting plate, first connecting plate can be dismantled and connect first spout, just the equal symmetry of lower extreme is equipped with two first connecting rings, two on the first connecting plate first connecting ring middle part is equipped with first rotation pole, first rotation pole can be dismantled and connect the second connecting plate, second connecting plate upper end is equipped with pneumatic shock-absorbing structure, just be equipped with first spring on the first rotation pole, first spring one end can be dismantled and connect first connecting plate, the connection can be dismantled to the first spring other end the second connecting plate.

Further, first connecting plate is type "T" style of calligraphy setting, first connecting plate sliding connection first spout, just first connecting plate middle part is through the bolt detachable connection the unmanned aerial vehicle body.

Further, pneumatic shock-absorbing structure includes first arc, but first arc below dismantlement is connected the second connecting plate, first arc inboard is equipped with two first connecting pipes, two the first connecting pipe inboard is connected through the second connecting pipe, two third connecting pipes, one side can be dismantled to the second connecting pipe and connect two third connecting pipes, be equipped with the check valve on the third connecting pipe, and this third connecting pipe one end is equipped with admission valve, opposite side third connecting pipe one end is equipped with rotary exhaust valve, the inboard sliding connection rubber dish of third connecting pipe, the rubber dish middle part is equipped with head rod, two the second arc can be dismantled to the head rod upper end.

Furthermore, the outer side of the second arc-shaped plate is provided with a metal ring, and the middle part of the metal ring is provided with a rubber block.

Further, the couple structure includes the second connecting rod, second connecting rod sliding connection first connecting hole, the equal screw connection nut of lower extreme, two on the second connecting rod the nut extrusion is connected the unmanned aerial vehicle body, just second connecting rod lower extreme can be dismantled and connect the third connecting plate, third connecting plate below detachable connects the couple.

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

the utility model discloses at first through be equipped with four first spouts in the outside of unmanned aerial vehicle body, four all be equipped with folding supporting structure in the first spout, utilize folding structure more convenient depositing;

when using, the damping strip is unfolded, then the damping effect corresponding to the pneumatic damping structure is carried out on the pneumatic damping structure, meanwhile, the damping strip is used for carrying out protection damping on the side edge, and the damping strip is a foam plate.

Drawings

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

FIG. 2 is a schematic view of the folding support structure of the present invention;

FIG. 3 is a schematic view of the pneumatic shock absorbing structure of the present invention;

fig. 4 is a schematic view of the hook structure of the present invention.

In the figure: 1-unmanned aerial vehicle body, 11-first chute, 12-first connecting hole, 2-folding supporting structure, 21-first connecting plate, 22-first connecting ring, 23-first rotating rod, 24-second connecting plate, 25-first spring, 3-pneumatic damping structure, 31-first arc-shaped plate, 32-first connecting pipe, 33-second connecting pipe, 34-third connecting pipe, 35-one-way valve, 36-air inlet valve, 37-rotary exhaust valve, 38-rubber disc, 381-first connecting rod, 39-second arc-shaped plate, 391-metal ring, 392-rubber block, 4-damping strip, 5-hook structure, 51-second connecting rod, 52-nut, 53-third connecting plate and 54-hook.

Detailed Description

In order to facilitate understanding of the present invention, the present invention will be described more fully with reference to the accompanying drawings, in which several embodiments of the present invention are shown, but the present invention can be implemented in different forms, and is not limited to the embodiments described in the text, but rather, these embodiments are provided to make the disclosure of the present invention more thorough and comprehensive.

In an embodiment, referring to fig. 1-4, an unmanned aerial vehicle with a shock absorption support comprises an unmanned aerial vehicle body 1, wherein four corners of the outer side of the unmanned aerial vehicle body 1 are provided with first sliding grooves 11, a folding support structure 2 is detachably connected in the first sliding grooves 11, and a pneumatic shock absorption structure 3 is arranged above the folding support structure 2;

1 outside of unmanned aerial vehicle body encircles its week and is equipped with a plurality of shock attenuation strips 4, just 1 center of unmanned aerial vehicle body is equipped with first connecting hole 12, connection couple structure 5 can be dismantled to first connecting hole 12, first connecting hole 12 around can dismantle four batteries of connection 13, four on the unmanned aerial vehicle body 1 battery 13 supplies to rotate for the fan and provides the electric energy.

In an embodiment, referring to fig. 1 to 3, the folding supporting structure 2 includes a first connecting plate 21, the first connecting plate 21 is detachably connected to the first chute 11, two first connecting rings 22 are symmetrically disposed at upper and lower ends of the first connecting plate 21, a first rotating rod 23 is disposed in a middle portion of each of the two first connecting rings 22, the first rotating rod 23 is detachably connected to a second connecting plate 24, a pneumatic damping structure 3 is disposed at an upper end of the second connecting plate 24, a first spring 25 is disposed on the first rotating rod 23, one end of the first spring 25 is detachably connected to the first connecting plate 21, and the other end of the first spring 25 is detachably connected to the second connecting plate 24.

In an embodiment, referring to fig. 1 to 3, the first connecting plate 21 is disposed like a "T" shape, the first connecting plate 21 is slidably connected to the first sliding groove 11, and the middle of the first connecting plate 21 is detachably connected to the unmanned aerial vehicle body 1 through a bolt.

In an embodiment, referring to fig. 1 to 3, the pneumatic shock absorption structure 3 includes a first arc plate 31, the second connection plate 24 is detachably connected below the first arc plate 31, two first connection pipes 32 are disposed on the inner side of the first arc plate 31, the inner sides of the two first connection pipes 32 are connected through a second connection pipe 33, the second connection pipe 33 is detachably connected to two third connection pipes 34, a one-way valve 35 is disposed on the third connection pipe 34 on one side, an air inlet valve 36 is disposed at one end of the third connection pipe 34, a rotary exhaust valve 37 is disposed at one end of the third connection pipe 34 on the other side, a rubber disc 38 is slidably connected to the inner side of the third connection pipe 34, a first connection rod 381 is disposed in the middle of the rubber disc 38, and the upper ends of the two first connection rods 381 are detachably connected to the second arc plate 39.

In an embodiment, referring to fig. 1 to 3, a metal ring 391 is disposed outside the second arc-shaped plate 39, and a rubber block 392 is disposed in the middle of the metal ring 391.

In an embodiment, referring to fig. 4, the hook structure 5 includes a second connecting rod 51, the second connecting rod 51 is slidably connected to the first connecting hole 12, the upper end and the lower end of the second connecting rod 51 are both screwed with nuts 52, the two nuts 52 are connected to the unmanned aerial vehicle body 1 in an extruding manner, the lower end of the second connecting rod 51 is detachably connected to a third connecting plate 53, and a hook 54 is detachably connected to the lower side of the third connecting plate 53.

Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various 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 by the appended claims and their equivalents, and thus the embodiments of the invention are intended only as illustrative examples of the invention and no limitation of the invention is intended whatsoever to be construed by the embodiments of the invention.

Claims

1. The utility model provides a take shock absorber support's unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: four corners of the outer side of the unmanned aerial vehicle body (1) are provided with first sliding grooves (11), the first sliding grooves (11) are detachably connected with folding supporting structures (2), and pneumatic shock absorption structures (3) are arranged above the folding supporting structures (2);

unmanned aerial vehicle body (1) outside encircles its week and is equipped with a plurality of shock attenuation strips (4), just unmanned aerial vehicle body (1) center is equipped with first connecting hole (12), connection couple structure (5) can be dismantled in first connecting hole (12), first connecting hole (12) around can dismantle on unmanned aerial vehicle body (1) and connect four battery (13), four battery (13) supply to rotate for the fan and provide the electric energy.

2. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: folding bearing structure (2) include first connecting plate (21), first connecting plate (21) can be dismantled the connection first spout (11), just the equal symmetry of lower extreme is equipped with two first connecting rings (22), two on first connecting plate (21) first connecting ring (22) middle part is equipped with first pivot pole (23), first pivot pole (23) can be dismantled and connect second connecting plate (24), second connecting plate (24) upper end is equipped with pneumatic shock-absorbing structure (3), just be equipped with first spring (25) on first pivot pole (23), connection can be dismantled to first spring (25) one end first connecting plate (21), the connection can be dismantled to first spring (25) other end second connecting plate (24).

3. The unmanned aerial vehicle of claim 2, wherein the unmanned aerial vehicle comprises: first connecting plate (21) are type "T" style of calligraphy and set up, first connecting plate (21) sliding connection first spout (11), just first connecting plate (21) middle part is through the bolt can dismantle the connection unmanned aerial vehicle body (1).

4. The unmanned aerial vehicle of claim 2, wherein the unmanned aerial vehicle comprises: the pneumatic damping structure (3) comprises a first arc-shaped plate (31), the second connecting plate (24) is detachably connected below the first arc-shaped plate (31), two first connecting pipes (32) are arranged on the inner side of the first arc-shaped plate (31), the inner sides of the two first connecting pipes (32) are connected through a second connecting pipe (33), the second connecting pipe (33) is detachably connected with two third connecting pipes (34), one side of the third connecting pipe (34) is provided with a one-way valve (35), and one end of the third connecting pipe (34) is provided with an air inlet valve (36), one end of the third connecting pipe (34) at the other side is provided with a rotary exhaust valve (37), the rubber disc (38) is connected to the inner side of the third connecting pipe (34) in a sliding mode, a first connecting rod (381) is arranged in the middle of the rubber disc (38), and the upper end of the first connecting rod (381) can be detachably connected with a second arc-shaped plate (39).

5. The unmanned aerial vehicle of claim 4, wherein the unmanned aerial vehicle comprises: the outer side of the second arc-shaped plate (39) is provided with a metal ring (391), and the middle part of the metal ring (391) is provided with a rubber block (392).

6. The unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle comprises: couple structure (5) include second connecting rod (51), second connecting rod (51) sliding connection first connecting hole (12), the equal screw connection nut (52) of lower extreme, two on second connecting rod (51) nut (52) extrusion is connected unmanned aerial vehicle body (1), just second connecting rod (51) lower extreme can be dismantled and connect third connecting plate (53), third connecting plate (53) below can be dismantled and connect couple (54).