CN219506229U

CN219506229U - Unmanned aerial vehicle shocks resistance

Info

Publication number: CN219506229U
Application number: CN202320867030.7U
Authority: CN
Inventors: 玉康罕
Original assignee: Shanxi Yifei Innovation Technology Co ltd
Current assignee: Shanxi Yifei Innovation Technology Co ltd
Priority date: 2023-04-18
Filing date: 2023-04-18
Publication date: 2023-08-11
Anticipated expiration: 2033-04-18

Abstract

The utility model discloses an impact-resistant unmanned aerial vehicle, which comprises a machine body, wherein a camera is fixedly connected to the bottom of the machine body, wings are arranged at four corners of the machine body, a protective shell is sleeved on the surface of the wings, a protective ring is sleeved on the surface of the protective shell, storage strips are fixedly connected to the front surface and the back surface of the machine body, and damping springs are fixedly connected to the inner walls of the storage strips. According to the utility model, the blades on the wing can be protected through the protective shell and the protective ring, impact force generated during collision can be buffered, the machine body of the machine body can be buffered and protected through the common cooperation of the damping spring, the protective strip and the protective roller, and then the impact force generated during landing of the machine body can be buffered and protected through the cooperation of the supporting block, the sealing block, the supporting column and the rubber pad, so that the outer edge of the unmanned aerial vehicle can be buffered and protected, and the purpose of impact force is achieved.

Description

Unmanned aerial vehicle shocks resistance

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an impact-resistant unmanned aerial vehicle.

Background

Unmanned aerial vehicles, as their name implies, are unmanned aircraft. Is a drone operated by a radio remote control device and a self-contained programming means, or is operated autonomously, either entirely or intermittently, by an on-board computer. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In the civil aspect, the unmanned aerial vehicle and industry application is the real just-needed unmanned aerial vehicle, and is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, electric power inspection, disaster relief, video shooting, romantic manufacturing and the like, so that the application of the unmanned aerial vehicle is greatly expanded, and developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.

At present, in the unmanned aerial vehicle flight process, often because the operator is operated carelessly or because of the phenomenon of colliding with and striking of unmanned aerial vehicle is caused to the topography and air current etc. cause certain degree damage to unmanned aerial vehicle's fuselage and paddle, make unmanned aerial vehicle lose balance and crash damage very easily to lead to the damage of the shooting equipment that unmanned aerial vehicle carried, thereby bring economic loss.

Therefore, the existing unmanned aerial vehicle needs to be modified, and the problem that impact force generated when the unmanned aerial vehicle is bumped and impacted cannot be buffered is effectively prevented.

Disclosure of Invention

In order to solve the problems in the prior art, the utility model aims to provide an impact-resistant unmanned aerial vehicle, which is provided with a buffer protection function for the outer edge of the unmanned aerial vehicle, so that the impact-resistant unmanned aerial vehicle has the advantage of impact resistance, and the problem that the impact force generated when the unmanned aerial vehicle is knocked and impacted cannot be buffered is solved.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an anti-impact unmanned aerial vehicle, includes the organism, the bottom fixedly connected with camera of organism, the four corners of organism all is provided with the wing, the surface cover of wing is equipped with the protecting crust, the surface cover of protecting crust is equipped with the guard ring, the equal fixedly connected with of front and back of organism accomodates the strip, the inner wall fixedly connected with damping spring of accomodating the strip, damping spring's the other end fixedly connected with protection strip, and the surface and the accomodating strip sliding connection of protection strip, the antifriction slot has been seted up to the other end of protection strip, the inside of antifriction slot is rotated through the pivot and is connected with the guard roller, the equal fixedly connected with supporting shoe in four corners of organism bottom, the inside sliding connection of supporting shoe has the sealing block, and sealing block and supporting shoe are sealed the setting, the bottom fixedly connected with support column of sealing block, the bottom fixedly connected with rubber pad of support column.

As the preferable mode of the utility model, the top of the machine body is fixedly connected with a supporting frame, the periphery of the machine body is fixedly connected with a plurality of shock absorption pads, and the shock absorption pads are uniformly arranged.

As the preferable mode of the utility model, the interior of the protective ring is provided with a cavity, three elastic rings are arranged in the cavity, and the three elastic rings are arranged in a triangle shape.

As the preferable mode of the utility model, the number of the damping springs and the protection rollers is a plurality, and the damping springs and the protection rollers are uniformly arranged.

As the preferable mode of the utility model, the surface of the support column is sleeved with the buffer spring, and the top and the bottom of the buffer spring are respectively fixedly connected with the support block and the rubber pad.

Preferably, the bottom of the machine body is fixedly connected with a transparent shell, and the transparent shell is matched with the camera.

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

1. according to the utility model, the blades on the wing can be protected through the protective shell and the protective ring, impact force generated during collision can be buffered, the machine body of the machine body can be buffered and protected through the common cooperation of the damping spring, the protective strip and the protective roller, and then the impact force generated during landing of the machine body can be buffered and protected through the cooperation of the supporting block, the sealing block, the supporting column and the rubber pad, so that the outer edge of the unmanned aerial vehicle can be buffered and protected, and the purpose of impact force is achieved.

2. According to the utility model, the top of the machine body can be protected through the arrangement of the supporting frame, and the periphery of the machine body can be secondarily protected through the arrangement of the plurality of shock absorption pads, so that the protection effect of the machine body is improved.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic top view of the structure of the present utility model;

FIG. 3 is an enlarged schematic view of the utility model at A in FIG. 1;

fig. 4 is an enlarged schematic view of fig. 2B in accordance with the present utility model.

In the figure: 1. a body; 2. a camera; 3. a wing; 4. a protective shell; 5. a protective ring; 6. a storage strip; 7. a damping spring; 8. a guard bar; 9. a rolling groove; 10. a protective roller; 11. a support block; 12. a sealing block; 13. a support column; 14. a rubber pad; 15. a support frame; 16. a shock pad; 17. a cavity; 18. an elastic ring; 19. a buffer spring; 20. a transparent shell.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

As shown in fig. 1 to 4, the shock-resistant unmanned aerial vehicle provided by the utility model comprises a machine body 1, wherein a camera 2 is fixedly connected to the bottom of the machine body 1, wings 3 are arranged at four corners of the machine body 1, a protective shell 4 is sleeved on the surface of the wings 3, a protective ring 5 is sleeved on the surface of the protective shell 4, a storage strip 6 is fixedly connected to the front surface and the back surface of the machine body 1, a damping spring 7 is fixedly connected to the inner wall of the storage strip 6, the other end of the damping spring 7 is fixedly connected with a protective strip 8, the surface of the protective strip 8 is in sliding connection with the storage strip 6, a rolling groove 9 is formed at the other end of the protective strip 8, a protective roller 10 is rotatably connected to the inside of the rolling groove 9 through a rotating shaft, supporting blocks 11 are fixedly connected to four corners of the bottom of the machine body 1, sealing blocks 12 are fixedly connected to the inside of the supporting blocks 11, the sealing blocks 12 are in sealing arrangement with the supporting blocks 11, supporting columns 13 are fixedly connected to the bottoms of the sealing blocks 12, and rubber pads 14 are fixedly connected to the bottoms of the supporting columns 13.

Referring to fig. 1 and 2, a supporting frame 15 is fixedly connected to the top of the machine body 1, a plurality of shock pads 16 are fixedly connected to the periphery of the machine body 1, and the shock pads 16 are uniformly arranged.

As a technical optimization scheme of the utility model, the top of the machine body 1 can be protected through the arrangement of the supporting frame 15, and the periphery of the machine body 1 can be secondarily protected through the arrangement of the plurality of shock pads 16, so that the protection effect of the machine body is improved.

Referring to fig. 3, a cavity 17 is formed in the guard ring 5, three elastic rings 18 are disposed in the cavity 17, and the three elastic rings 18 are arranged in a triangle.

As a technical optimization scheme of the utility model, through the arrangement of the cavity 17 and the three elastic rings 18, impact force can be absorbed through mutual extrusion and deformation of the three elastic rings 18, so that the buffering effect on the protective ring 5 can be improved.

Referring to fig. 1 and 2, the number of damper springs 7 and the shielding roller 10 is several, and the several damper springs 7 and the shielding roller 10 are uniformly arranged.

As a technical optimization scheme of the utility model, through the arrangement of the damping springs 7 and the protection rollers 10, the protection buffering effect on the surface of the machine body 1 is improved through the number of the damping springs 7 and the protection rollers 10.

Referring to fig. 1, a buffer spring 19 is sleeved on the surface of the support column 13, and the top and bottom of the buffer spring 19 are fixedly connected with the support block 11 and the rubber pad 14 respectively.

As a technical optimization scheme of the present utility model, the impact force generated when the machine body 1 falls can be damped by the arrangement of the buffer spring 19.

Referring to fig. 1, a transparent case 20 is fixedly connected to the bottom of a body 1, and the transparent case 20 is used in cooperation with a camera 2.

As a technical optimization of the present utility model, the camera 2 can be protected by the provision of the transparent shell 20.

The working principle and the using flow of the utility model are as follows: when a user shoots by using the unmanned aerial vehicle, if the user carelessly or collides and impacts the unmanned aerial vehicle caused by topography, air flow and the like, if the protective shell 4 on the wing 3 plays a role in protecting the blade, deformation generated when the protective ring 5 and the three elastic rings 18 are extruded can absorb impact force generated when the unmanned aerial vehicle is impacted, thereby achieving the effect of buffering the protective shell 4, and the machine body 1 can be protected through the protective strip 8 and the protective roller 10, the impact force can compress the damping spring 7 when extruding the protective strip 8, thereby achieving the effect of absorbing the impact force, at the moment, the damping pad 16 can secondarily protect the machine body 1, thereby achieving the effect of protecting the machine body 1, then the top of the machine body 1 and the camera 2 can be respectively protected through the supporting frame 15 and the transparent shell 20, when the user operates the unmanned aerial vehicle to land, the supporting column 13 drives the rubber pad 14 to contact with the ground, at the moment, the sealing block 12 is used for extruding air in the supporting block 11, and the damping spring 19 is used for compressing, thereby buffering the machine body 1 when the machine body is landed.

It is noted that relational terms such as first and second, and the like are 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. Moreover, 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 utility model 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 therein 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. An impact resistant unmanned aerial vehicle, includes organism (1), its characterized in that: the camera is characterized in that the camera (2) is fixedly connected to the bottom of the machine body (1), the wings (3) are arranged at four corners of the machine body (1), the protecting shell (4) is sleeved on the surface of the wings (3), the protecting ring (5) is sleeved on the surface of the protecting shell (4), the storage strip (6) is fixedly connected to the front side and the back side of the machine body (1), the damping spring (7) is fixedly connected to the inner wall of the storage strip (6), the protecting strip (8) is fixedly connected to the other end of the damping spring (7), the surface of the protecting strip (8) is in sliding connection with the storage strip (6), the rolling groove (9) is formed in the other end of the protecting strip (8), the protecting roll (10) is rotationally connected to the inside of the rolling groove (9), the supporting block (11) is fixedly connected to the four corners of the bottom of the machine body (1), the sealing block (12) is fixedly connected to the inside of the supporting block (11), the sealing block (12) is in sealing arrangement with the bottom of the supporting block (11), and the sealing block (12) is fixedly connected to the supporting column (13), and the supporting column (13) is fixedly connected to the bottom of the supporting column (13).

2. An impact resistant unmanned aerial vehicle as claimed in claim 1, wherein: the top fixedly connected with support frame (15) of organism (1), a plurality of shock pads (16) of fixedly connected with all around of organism (1), and a plurality of shock pads (16) are evenly arranged.

3. An impact resistant unmanned aerial vehicle as claimed in claim 1, wherein: the inner part of the protective ring (5) is provided with a cavity (17), three elastic rings (18) are arranged in the cavity (17), and the three elastic rings (18) are arranged in a triangle.

4. An impact resistant unmanned aerial vehicle as claimed in claim 1, wherein: the number of the damping springs (7) and the protection rollers (10) is a plurality of the damping springs (7) and the protection rollers (10) are uniformly arranged.

5. An impact resistant unmanned aerial vehicle as claimed in claim 1, wherein: the surface of the support column (13) is sleeved with a buffer spring (19), and the top and the bottom of the buffer spring (19) are fixedly connected with the support block (11) and the rubber pad (14) respectively.

6. An impact resistant unmanned aerial vehicle as claimed in claim 1, wherein: the bottom of the machine body (1) is fixedly connected with a transparent shell (20), and the transparent shell (20) is matched with the camera (2).