CN211364934U

CN211364934U - Wing buffering protector for unmanned aerial vehicle

Info

Publication number: CN211364934U
Application number: CN201921350446.1U
Authority: CN
Inventors: 杨迎港
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-08-20
Filing date: 2019-08-20
Publication date: 2020-08-28
Anticipated expiration: 2029-08-20

Abstract

The utility model discloses a wing buffering protector for unmanned aerial vehicle, including unmanned aerial vehicle body, buffer spring and fixture block, the wing body is installed in the outside of unmanned aerial vehicle body, and the outside of wing body has seted up the mounting groove, the outside of wing body is provided with the guard plate, buffer spring connects in the outside of guard plate, and the inboard of guard plate is connected with torsion spring, the shifting chute has been seted up to the inside of guard plate, and the internal connection of shifting chute has compression spring, compression spring's the outside is connected with the regulating block, the fixture block is installed in the outside of regulating block, and the downside of regulating block is provided with the regulation pole, the outside of adjusting the pole is connected with coupling spring. The outer side of the protection plate of the wing buffering protection device for the unmanned aerial vehicle is connected with a buffer plate through a buffer spring, the buffer plate is made of rubber, the buffer plate made of rubber is combined with the buffer spring, the impact force can be buffered, and the wing body is protected.

Description

Wing buffering protector for unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle correlation technique field specifically is a wing buffering protector for unmanned aerial vehicle.

Background

Unmanned aerial vehicle is the general name of unmanned vehicles, utilizes radio remote control equipment and self-contained program control, and along with unmanned aerial vehicle correlation technique rapid development, the unmanned aerial vehicle kind also increases gradually, and the usage characteristics are also comparatively bright, according to different use occasion and service function, unmanned aerial vehicle's preparation size, quality and flying height etc. all have great difference.

However, the existing unmanned aerial vehicle still has a deficiency in the use process, the unmanned aerial vehicle is an unmanned aerial vehicle, flight deviation always exists by utilizing remote control operation, when the unmanned aerial vehicle scratches or collides with foreign objects, wings can be damaged, the flight stability of the unmanned aerial vehicle is influenced, and the existing unmanned aerial vehicle does not have a device for protecting the wings.

Therefore, we propose a wing buffering protector for unmanned aerial vehicles to solve the above-mentioned problems.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a wing buffering protector for unmanned aerial vehicle to current unmanned aerial vehicle does not have the device of protecting the wing on solving the existing market that above-mentioned background art provided, the impaired problem that can influence unmanned aerial vehicle's flight of wing.

In order to achieve the above object, the utility model provides a following technical scheme: a wing buffering and protecting device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body, a buffer spring and a clamping block, wherein the wing body is arranged on the outer side of the unmanned aerial vehicle body, the outer side of the wing body is provided with a mounting groove, the outer side of the wing body is provided with a protection plate, the buffer spring is connected with the outer side of the protection plate, and the inner side of the protection plate is connected with a torsion spring, the inner part of the protection plate is provided with a moving groove, the inner part of the moving groove is connected with a compression spring, the outer side of the compression spring is connected with an adjusting block, the clamping block is arranged on the outer side of the adjusting block, an adjusting rod is arranged at the lower side of the adjusting block, a connecting spring is connected at the outer side of the adjusting rod, a limiting block is arranged at the upper side of the adjusting block, and the outside of stopper is provided with the spacing groove, the inboard at the guard plate is seted up to the spacing groove, buffer spring's the outside is connected with the buffer board.

Preferably, adjust the pole and pass through connecting spring and guard plate constitution elastic construction, and the downside that the side of going up of adjusting the pole and regulating block is the arc structure to adjust pole and the mutual laminating of regulating block.

Preferably, the depression section of each protection plate is of a U-shaped structure, the width of the inner side face of each protection plate is larger than that of the outer side face of the wing body, and the adjacent 2 protection plates are connected through torsion springs.

Preferably, the buffer board is made of rubber, and buffer springs are uniformly distributed between the inner side face of the buffer board and the outer side face of the protection board.

Preferably, the main section of regulating block is right trapezoid, and regulating block and guard plate are sliding connection to regulating block and fixture block structure as an organic whole, the position and the size of fixture block all coincide each other with the mounting groove simultaneously.

Compared with the prior art, the beneficial effects of the utility model are that: the wing buffer protection device for the unmanned aerial vehicle,

(1) the outer side of the protection plate is connected with a buffer plate through a buffer spring, the buffer plate is made of rubber, and the buffer plate made of rubber is combined with the buffer spring to buffer the impact force and protect the wing body;

(2) the inside of guard plate is provided with the fixture block, and fixture block and regulating block can advance the fixture block card into the mounting groove that the wing body outside was seted up through compression spring's effect, realize that the guard plate is fixed with being connected of unmanned aerial vehicle body, and the later stage can push up the regulation pole, and control regulation pole promotes the regulating block and removes to promote the fixture block and remove and break away from with the mounting groove and be connected, remove being connected of guard plate and wing body, this design is convenient for carry out the dismouting to protector.

Drawings

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

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

fig. 3 is an enlarged schematic view of a portion a of fig. 2 according to the present invention;

fig. 4 is the utility model discloses guard plate and stopper junction side cut open structure schematic diagram.

In the figure: 1. an unmanned aerial vehicle body; 2. a wing body; 3. adjusting a rod; 4. a connecting spring; 5. mounting grooves; 6. a protection plate; 7. a buffer spring; 8. a buffer plate; 9. a moving groove; 10. a compression spring; 11. an adjusting block; 12. a clamping block; 13. a limiting block; 14. a limiting groove; 15. a torsion spring.

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: a wing buffering and protecting device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a wing body 2, an adjusting rod 3, a connecting spring 4, a mounting groove 5, a protection plate 6, a buffer spring 7, a buffer plate 8, a moving groove 9, a compression spring 10, an adjusting block 11, a clamping block 12, a limiting block 13, a limiting groove 14 and a torsion spring 15, wherein the wing body 2 is installed on the outer side of the unmanned aerial vehicle body 1, the mounting groove 5 is formed in the outer side of the wing body 2, the protection plate 6 is arranged on the outer side of the wing body 2, the buffer spring 7 is connected to the outer side of the protection plate 6, the torsion spring 15 is connected to the inner side of the protection plate 6, the moving groove 9 is formed in the protection plate 6, the compression spring 10 is connected to the inner side of the moving groove 9, the adjusting block 11 is connected to the outer side of the compression spring, the outside of adjusting pole 3 is connected with coupling spring 4, and the upside of regulating block 11 is provided with stopper 13, and stopper 13's the outside is provided with spacing groove 14, and spacing groove 14 is seted up in the inboard of guard plate 6, and the outside of buffer spring 7 is connected with buffer board 8.

In the embodiment, the adjusting rod 3 and the protection plate 6 form an elastic structure through the connecting spring 4, the upper side surface of the adjusting rod 3 and the lower side surface of the adjusting block 11 are both arc-shaped structures, the adjusting rod 3 and the adjusting block 11 are mutually attached, and the position of the adjusting block 11 can be controlled by controlling the movement of the adjusting rod 3;

the depression section of each protection plate 6 is of a U-shaped structure, the width of the inner side face of each protection plate 6 is larger than that of the outer side face of each wing body 2, the adjacent 2 protection plates 6 are connected through torsion springs 15, the wing bodies 2 are conveniently placed on the inner sides of the protection plates 6, the protection plates 6 are used for protecting the wing bodies 2, and the protection plates 6 can be folded;

the buffer plate 8 is made of rubber, and the buffer springs 7 are uniformly distributed between the inner side surface of the buffer plate 8 and the outer side surface of the protection plate 6, so that the impact force can be buffered, and the damage to the wing body 2 can be reduced;

the main section of regulating block 11 is right trapezoid, and regulating block 11 is sliding connection with guard plate 6 to regulating block 11 and fixture block 12 structure as an organic whole, the position and the size of fixture block 12 all coincide each other with mounting groove 5 simultaneously, the position of regulating block 11 is convenient for adjust, makes 11 horizontal migration of regulating block, thereby drives fixture block 12 and removes, removes being connected of fixture block 12 and mounting groove 5, is convenient for dismantle whole device.

The working principle is as follows: when the wing buffering and protecting device for the unmanned aerial vehicle is used, firstly, a user firstly moves the whole device into a working area, as shown in figure 1, the whole protecting device is firstly installed on the outer side of an unmanned aerial vehicle body 1, adjacent 2 protection plates 6 are connected through a torsion spring 15, the protection plates 6 can be shifted to enable the protection plates 6 to be positioned in the same horizontal plane, then the protection plates 6 are moved downwards from the upper side of the unmanned aerial vehicle body 1 to ensure that the protection plates 6 are sleeved on the outer side of the unmanned aerial vehicle body 1, as shown in figure 3, when the protection plates 6 move downwards, the wing body 2 pushes a clamping block 12, the clamping block 12 drives an adjusting block 11 to move in a moving groove 9 and extrudes a compression spring 10, meanwhile, a T-shaped limiting block 13 on the upper side of the adjusting block 11 slides in a limiting groove 14 to ensure the horizontal movement of the clamping block 12, when the clamping block 12 corresponds, the compression spring 10 can push the adjusting block 11 to reset, so that the clamping block 12 is pushed to reset and clamp into the mounting groove 5, the protection plate 6 is connected with the unmanned aerial vehicle body 1, as shown in the combined drawing 2, the connection between the protection plate 6 and the 3 wing bodies 2 is completed according to the steps, when the unmanned aerial vehicle flies, if the deviation occurs in the flying process, when the wing bodies 2 collide with or are scratched by foreign objects, the buffer plate 8 made of rubber materials on the outer side of the protection plate 6 can buffer the collision force, and the buffer plate 8 is connected with the protection plate 6 through the buffer spring 7, so that the buffer force is increased, and the protection and buffering of the wing bodies 2 are facilitated;

when the whole protection device needs to be disassembled, the adjusting rod 3 shown in fig. 3 is pushed upwards, the adjusting rod 3 extrudes the connecting spring 4 connected to the outer side, the adjusting block 11 is pushed to extrude the compression spring 10 to slide in the moving groove 9, so that the clamping block 12 is driven to slide and be disconnected from the mounting groove 5, then the protection plate 6 is pushed upwards, the protection plate 6 is folded upwards through the torsion spring 15 shown in fig. 1, the connection between the protection plate 6 and the wing body 2 is removed, the disassembly of the 3 protection plates 6 is completed according to the steps, at the moment, the disassembly of the whole protection device is conveniently completed, the above is the working process of the whole protection device, and the content which is not described in detail in the specification belongs to the prior art known by technical personnel in the field.

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 may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.

Claims

1. The utility model provides a wing buffering protector for unmanned aerial vehicle, includes unmanned aerial vehicle body (1), buffer spring (7) and fixture block (12), its characterized in that: the unmanned aerial vehicle wing comprises an unmanned aerial vehicle body (1), and is characterized in that the wing body (2) is installed on the outer side of the unmanned aerial vehicle body (1), a mounting groove (5) is formed in the outer side of the wing body (2), a protection plate (6) is arranged on the outer side of the wing body (2), a buffer spring (7) is connected to the outer side of the protection plate (6), a torsion spring (15) is connected to the inner side of the protection plate (6), a moving groove (9) is formed in the protection plate (6), a compression spring (10) is connected to the inner portion of the moving groove (9), an adjusting block (11) is connected to the outer side of the compression spring (10), a clamping block (12) is installed on the outer side of the adjusting block (11), an adjusting rod (3) is arranged on the lower side of the adjusting block (11), a connecting spring (4, and the outside of stopper (13) is provided with spacing groove (14), the inboard at guard plate (6) is seted up in spacing groove (14), the outside of buffer spring (7) is connected with buffer board (8).

2. The wing cushioning device for the unmanned aerial vehicle as claimed in claim 1, wherein: adjust pole (3) and constitute elastic construction through connecting spring (4) and guard plate (6), and the last side of adjusting pole (3) is the arc structure with the downside of regulating block (11) to adjust pole (3) and laminate each other with regulating block (11).

3. The wing cushioning device for the unmanned aerial vehicle as claimed in claim 1, wherein: the depression section of the protection plate (6) is of a U-shaped structure, the width of the inner side face of the protection plate (6) is larger than that of the outer side face of the wing body (2), and the adjacent 2 protection plates (6) are connected through torsion springs (15).

4. The wing cushioning device for the unmanned aerial vehicle as claimed in claim 1, wherein: buffer board (8) are the rubber material, and even distribution has buffer spring (7) between the lateral surface of medial surface and guard plate (6) of buffer board (8).

5. The wing cushioning device for the unmanned aerial vehicle as claimed in claim 1, wherein: the main section of the adjusting block (11) is in a right trapezoid shape, the adjusting block (11) is in sliding connection with the protection plate (6), the adjusting block (11) and the clamping block (12) are in an integral structure, and meanwhile the position and the size of the clamping block (12) are matched with the mounting groove (5) mutually.