CN216233011U

CN216233011U - Protection architecture is used to unmanned aerial vehicle wing

Info

Publication number: CN216233011U
Application number: CN202121925911.7U
Authority: CN
Inventors: 王涛
Original assignee: Individual
Current assignee: Yulin Tianduyun Laser Technology Co.,Ltd.
Priority date: 2021-08-17
Filing date: 2021-08-17
Publication date: 2022-04-08
Anticipated expiration: 2031-08-17

Abstract

The utility model discloses a protection structure for wings of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, wherein a connecting arm is fixedly connected to the surface of the unmanned aerial vehicle body, a wing is arranged on one side, away from the unmanned aerial vehicle body, of the connecting arm, a structure for protecting the wing is arranged on the surface of the wing, the structure for protecting the wing comprises a protection frame arranged on the surface of the wing, a reinforcing plate is fixedly connected to the top of the protection frame, a fixing block is fixedly connected to the surface of the protection frame, and the fixing block is sleeved on the surface of the connecting arm. According to the utility model, the fixing block is sleeved on the surface of the connecting arm, the spring fixes the fixing block through the baffle and the limiting rod, and the protective frame protects the wing fan, so that the problem that the existing unmanned aerial vehicle cannot protect the wing, and when the wing touches an unknown object, the wing can be damaged when the unmanned aerial vehicle flies, and the unmanned aerial vehicle crashes is solved.

Description

Protection architecture is used to unmanned aerial vehicle wing

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a protection structure for wings of an unmanned aerial vehicle.

Background

Unmanned aerial vehicle indicates unmanned aircraft, and current unmanned aerial vehicle can't protect the wing, and unmanned aerial vehicle when flying, when the wing runs into unidentified object, can lead to the damage of wing to lead to unmanned aerial vehicle crash.

SUMMERY OF THE UTILITY MODEL

In order to solve the problems in the background art, the utility model aims to provide a protection structure for wings of an unmanned aerial vehicle, which has the advantage of protecting the wings, and solves the problem that the existing unmanned aerial vehicle cannot protect the wings, and when the wings of the unmanned aerial vehicle collide with an unknown object during flying, the wings can be damaged, so that the unmanned aerial vehicle is crashed.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle is protection architecture for wing, includes the unmanned aerial vehicle body, the fixed surface of unmanned aerial vehicle body is connected with the linking arm, one side that the unmanned aerial vehicle body was kept away from to the linking arm sets up there is the wing, the surface of wing is provided with and is used for carrying out the structure protected to the wing.

Preferably, the structure for protecting the wing fan comprises a protection frame arranged on the surface of the wing fan, a reinforcing plate is fixedly connected to the top of the protection frame, a fixed block is fixedly connected to the surface of the protection frame, the fixed block is sleeved on the surface of a connecting arm, a fixed plate is fixedly connected to the top of the connecting arm, a moving groove is formed in the top of the fixed plate, a limiting rod is arranged inside the moving groove, the outer side of the limiting rod penetrates into the fixed block, a baffle is fixedly connected to the surface of the limiting rod, a spring is fixedly connected to the inner side of the baffle, and the inner side of the spring is fixedly connected to the inner side of the inner wall of the moving groove.

Preferably, the fixing block is internally provided with a positioning hole, and the top of the connecting arm is fixedly connected with a positioning rod matched with the positioning hole.

Preferably, the inner side of the limiting rod penetrates through the inner side of the fixing plate and is fixedly connected with a pulling block, and the surface of the pulling block is provided with anti-skid grains.

Preferably, the bottom of the connecting arm is fixedly connected with a supporting leg, and the bottom of the supporting leg is fixedly connected with an anti-skid pad.

Preferably, the surfaces of the protective frame and the fixed block are provided with corrosion-resistant layers, and the thickness of each corrosion-resistant layer is 150 microns.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the utility model, the fixing block is sleeved on the surface of the connecting arm, the spring fixes the fixing block through the baffle and the limiting rod, and the protective frame protects the wing fan, so that the problem that the existing unmanned aerial vehicle cannot protect the wing, and when the wing touches an unknown object, the wing can be damaged when the unmanned aerial vehicle flies, and the unmanned aerial vehicle crashes is solved.

2. According to the utility model, the protective frame, the fixed block and the fixed plate are arranged, so that the wing fan can be protected, and the safety of the wing fan is improved.

3. The positioning hole and the positioning rod are arranged, so that the fixing block can be positioned and fixed, and the practicability of the fixing block is improved.

4. According to the utility model, the pulling block is arranged, so that a user can conveniently pull the limiting rod, and the practicability of the limiting rod is improved.

5. According to the unmanned aerial vehicle body, the support legs and the non-slip pads are arranged, so that the unmanned aerial vehicle body can be supported and prevented from slipping, and the stability of the unmanned aerial vehicle body is improved.

6. According to the utility model, the corrosion-resistant layer is arranged, so that the protective frame and the fixed block can be prevented from being corroded, and the service lives of the protective frame and the fixed block are prolonged.

Drawings

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

FIG. 2 is a schematic top cross-sectional view of a stop lever according to the present invention;

fig. 3 is a schematic perspective view of a protection frame according to the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a connecting arm; 3. a wing fan; 4. a protective frame; 5. a reinforcing plate; 6. a fixed block; 7. a fixing plate; 8. a moving groove; 9. a limiting rod; 10. a baffle plate; 11. a spring; 12. positioning a groove; 13. positioning a rod; 14. pulling the block; 15. supporting legs; 16. a non-slip mat.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

As shown in fig. 1 to 3, the protection structure for the wings of the unmanned aerial vehicle provided by the utility model comprises an unmanned aerial vehicle body 1, wherein a connecting arm 2 is fixedly connected to the surface of the unmanned aerial vehicle body 1, a wing 3 is arranged on one side of the connecting arm 2 away from the unmanned aerial vehicle body 1, and a structure for protecting the wing 3 is arranged on the surface of the wing 3.

Referring to fig. 1, a structure for protecting wing 3 is including setting up at the protective frame 4 on wing 3 surface, top fixedly connected with reinforcing plate 5 of protective frame 4, the fixed surface of protective frame 4 is connected with fixed block 6, the fixed block 6 cover is established on the surface of linking arm 2, the top fixedly connected with fixed plate 7 of linking arm 2, shifting chute 8 has been seted up at the top of fixed plate 7, the inside of shifting chute 8 is provided with gag lever post 9, the outside of gag lever post 9 runs through to the inside of fixed block 6, the fixed surface of gag lever post 9 is connected with baffle 10, the inboard fixedly connected with spring 11 of baffle 10, the inboard fixed connection of spring 11 is in the inboard of 8 inner walls of shifting chute.

As a technical optimization scheme of the utility model, the protective frame 4, the fixed block 6 and the fixed plate 7 are arranged, so that the wing fan 3 can be protected, and the safety of the wing fan 3 is improved.

Referring to fig. 3, a positioning hole 12 is formed inside the fixing block 6, and a positioning rod 13 used in cooperation with the positioning hole 12 is fixedly connected to the top of the connecting arm 2.

As a technical optimization scheme of the utility model, the positioning holes 12 and the positioning rods 13 are arranged, so that the fixing block 6 can be positioned and fixed, and the practicability of the fixing block 6 is improved.

Referring to fig. 2, a pulling block 14 is fixedly connected to the inner side of the limiting rod 9 penetrating to the inner side of the fixing plate 7, and anti-skid threads are formed on the surface of the pulling block 14.

As a technical optimization scheme of the utility model, the pulling block 14 is arranged, so that a user can conveniently pull the limiting rod 9, and the practicability of the limiting rod 9 is improved.

Referring to fig. 1, a support leg 15 is fixedly connected to the bottom of the connecting arm 2, and a non-slip mat 16 is fixedly connected to the bottom of the support leg 15.

As a technical optimization scheme of the utility model, the support legs 15 and the non-slip mat 16 are arranged, so that the unmanned aerial vehicle body 1 can be supported and non-slip, and the stability of the unmanned aerial vehicle body 1 is improved.

Referring to fig. 1, the surfaces of the protective frame 4 and the fixing block 6 are provided with a corrosion-resistant layer having a thickness of 150 μm.

As a technical optimization scheme of the utility model, the corrosion-resistant layer is arranged, so that the protective frame 4 and the fixed block 6 can be prevented from being corroded, and the service life of the protective frame 4 and the fixed block 6 is prolonged.

The working principle and the using process of the utility model are as follows: during the use, the user inwards stimulates and draws piece 14, draws piece 14 to drive gag lever post 9 inward movement, overlaps fixed block 6 on the surface of linking arm 2, makes locating lever 13 insert in locating hole 12, loosens and draws piece 14, spring 11 outwards promotes gag lever post 9 through baffle 10, makes gag lever post 9 insert inside fixed block 6, is fixed block 6 and protective frame 4, protective frame 4 protects wing fan 3, prevents that wing fan 3 from colliding with unidentified object, can possess the effect of protection wing.

In summary, the following steps: this protection architecture for unmanned aerial vehicle wing, through covering fixed block 6 on 2 surfaces of linking arm, spring 11 passes through

baffle

10 and 9 fixed with fixed block 6 with gag lever post, and protective frame 4 protects wing fan 3, has solved current unmanned aerial vehicle and can't protect the wing, and unmanned aerial vehicle is when flying, when the wing runs into unclear object can lead to the damage of wing to lead to the problem of unmanned aerial vehicle crash.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

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 utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A protection structure for wings of an unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a connecting arm (2) is fixedly connected to the surface of the unmanned aerial vehicle body (1), and an organic wing (3) is arranged on one side, away from the unmanned aerial vehicle body (1), of the connecting arm (2);

the method is characterized in that: the surface of the wing (3) is provided with a structure for protecting the wing (3).

2. The protective structure for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein: the structure for protecting the wing (3) comprises a protective frame (4) arranged on the surface of the wing (3), the top of the protective frame (4) is fixedly connected with a reinforcing plate (5), the surface of the protective frame (4) is fixedly connected with a fixed block (6), the fixed block (6) is sleeved on the surface of the connecting arm (2), the top of the connecting arm (2) is fixedly connected with a fixed plate (7), a moving groove (8) is formed at the top of the fixed plate (7), a limiting rod (9) is arranged inside the moving groove (8), the outer side of the limiting rod (9) penetrates into the fixing block (6), the surface of the limiting rod (9) is fixedly connected with a baffle plate (10), the inner side of the baffle (10) is fixedly connected with a spring (11), and the inner side of the spring (11) is fixedly connected with the inner side of the inner wall of the movable groove (8).

3. The protective structure for the wings of the unmanned aerial vehicle as claimed in claim 2, wherein: locating holes (12) are formed in the fixing blocks (6), and locating rods (13) matched with the locating holes (12) for use are fixedly connected to the tops of the connecting arms (2).

4. The protective structure for the wings of the unmanned aerial vehicle as claimed in claim 2, wherein: the inner side of the limiting rod (9) penetrates through the inner side of the fixing plate (7) and is fixedly connected with a pulling block (14), and anti-skid grains are formed in the surface of the pulling block (14).

5. The protective structure for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein: the bottom fixedly connected with supporting leg (15) of linking arm (2), the bottom fixedly connected with slipmat (16) of supporting leg (15).

6. The protective structure for the wings of the unmanned aerial vehicle as claimed in claim 2, wherein: the surfaces of the protective frame (4) and the fixed block (6) are provided with corrosion-resistant layers, and the thickness of each corrosion-resistant layer is 150 microns.