CN216128432U

CN216128432U - A buffer stop for unmanned aerial vehicle wing

Info

Publication number: CN216128432U
Application number: CN202122923248.3U
Authority: CN
Inventors: 韩青松; 刘少华; 席爱红
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-11-24
Filing date: 2021-11-24
Publication date: 2022-03-25
Anticipated expiration: 2031-11-24

Abstract

The utility model discloses an anti-collision device for wings of an unmanned aerial vehicle, which comprises an anti-collision frame, wherein the anti-collision frame is spherical and is hollow; a circular ring is horizontally arranged in the middle of the anti-collision frame, and a base is arranged in the middle of the circular ring; the upper end of base is provided with the bracing piece, the top of bracing piece is provided with places the platform, and places the middle part of platform and be provided with the camera, the bottom four corners of base evenly is provided with the screw. According to the utility model, the anti-collision frame is arranged outside the unmanned aerial vehicle, is spherical and hollow inside and is made of light transparent materials, the unmanned aerial vehicle is hinged to the anti-collision frame, the anti-collision frame always protects the unmanned aerial vehicle inside in the flying process of the unmanned aerial vehicle, the propeller on the unmanned aerial vehicle is prevented from being damaged to influence the flying, the anti-collision frame is provided with the round hole, the round hole is convenient for air flowing in the flying process, and the camera is convenient for shooting materials.

Description

A buffer stop for unmanned aerial vehicle wing

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an anti-collision device for wings of an unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is called UAV in English, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and the wings of the unmanned plane are mostly propellers, so that the unmanned plane can fly conveniently.

Unmanned aerial vehicle takes place the striking with the obstacle easily when flight, in order to prevent that unmanned aerial vehicle from taking place to damage, can set up crashproof buffer board on unmanned aerial vehicle's wing usually, however this also alleviates the damage degree to a certain extent, if directly drop after the unmanned aerial vehicle striking, unmanned aerial vehicle's wing or screw take place to damage, then unmanned aerial vehicle just can't fly. Therefore, the unmanned aerial vehicle wing collision avoidance device is improved, and the unmanned aerial vehicle wing collision avoidance device is provided.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problems, the utility model provides the following technical scheme:

the utility model relates to an anti-collision device for wings of an unmanned aerial vehicle, which comprises an anti-collision frame, wherein the anti-collision frame is spherical and is hollow inside; a circular ring is horizontally arranged in the middle of the anti-collision frame, and a base is arranged in the middle of the circular ring; the upper end of the base is provided with a supporting rod, the top of the supporting rod is provided with a placing table, the middle of the placing table is provided with a camera, four corners of the bottom end of the base are uniformly provided with propellers, and the propellers can drive the whole unmanned aerial vehicle and the anti-collision frame to fly; the placing table is used for placing the camera, and the supporting rod can support the placing table; the base is used for placing the screw, and the base supports the camera.

As a preferred technical scheme of the utility model, the middle part of the supporting rod is penetrated with the connecting rod, the two ends of the connecting rod are fixedly arranged on the inner wall of the ring, and the connecting rod plays a role in connecting the unmanned aerial vehicle and the ring.

As a preferred technical scheme, the side face, close to the anti-collision frame, of the circular ring is evenly provided with the spherical connecting pieces, the circular ring is hinged with the anti-collision frame through the spherical connecting pieces, the circular ring is hinged with the anti-collision frame, the unmanned aerial vehicle can be kept stable during flying, and the anti-collision frame can protect the unmanned aerial vehicle from being damaged if the unmanned aerial vehicle collides.

According to the preferable technical scheme, the two sides of the camera are respectively provided with the fixed block, the searchlight is arranged inside the fixed block, the camera is used for shooting materials, the fixed block plays a role in fixing the camera, and the searchlight can supplement light in the area with weak illumination, so that the shot materials are prevented from being not clear enough.

As a preferred technical scheme of the utility model, a square groove is formed in the middle of the top end of the placing table, a cushion pad is arranged at the bottom end of the square groove, the camera is positioned in the square groove, and the cushion pad can play a certain buffering role when the camera flies; the bottom of camera and the interior bottom surface of square groove all are provided with the magnet piece of mutual absorption, and the stability of camera can be strengthened to the magnet piece when unmanned aerial vehicle flies.

As a preferred technical scheme of the present invention, a fixture block is disposed on the fixed block located on one side of the camera, a clamping interface is disposed on the fixed block located on the other side of the camera, the fixture block is clamped with the clamping interface, elastic blocks are disposed on two sides of the fixture block, clamping grooves matched with the elastic blocks are disposed on two sides inside the clamping interface, and the fixed block can enhance the stability of the camera.

As a preferred technical scheme, round holes are formed in the upper side and the lower side, the left side and the right side, and the front side and the rear side of the anti-collision frame, so that the round holes are convenient for air flow of the unmanned aerial vehicle during flying, and meanwhile, the round holes are also convenient for a camera to shoot materials.

As a preferred technical scheme of the utility model, the anti-collision frame is made of transparent materials, and the transparent materials are convenient for a camera to shoot materials.

The utility model has the beneficial effects that: according to the unmanned aerial vehicle anti-collision frame, the anti-collision frame is arranged outside the unmanned aerial vehicle, is spherical and hollow inside and is made of light transparent materials, the unmanned aerial vehicle is hinged to the anti-collision frame, the anti-collision frame always protects the unmanned aerial vehicle inside in the flying process of the unmanned aerial vehicle, and the propeller on the unmanned aerial vehicle is prevented from being damaged to influence flying.

According to the utility model, the round hole is formed in the anti-collision frame, so that the round hole is convenient for air flow during flying and is also convenient for a camera to shoot materials.

Drawings

The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model and not to limit the utility model. In the drawings:

fig. 1 is a schematic perspective view of a collision avoidance device for wings of an unmanned aerial vehicle according to the first embodiment of the utility model;

FIG. 2 is a schematic perspective view of a second anti-collision device for wings of an unmanned aerial vehicle according to the present invention;

fig. 3 is a partial structural schematic diagram of a collision avoidance device for wings of an unmanned aerial vehicle according to the utility model.

In the figure: 1. an anti-collision frame; 2. a circular ring; 3. a base; 4. a support bar; 5. a placing table; 6. A camera; 7. a propeller; 8. a connecting rod; 9. a spherical connecting member; 10. a fixed block; 11. a searchlight; 12. a square groove; 13. a clamping block; 14. a card interface; 15. a circular hole.

Detailed Description

The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are described herein for the purpose of illustration and explanation and not limitation.

Example (b): as shown in fig. 1 to 3, the anti-collision device for the wings of the unmanned aerial vehicle comprises an anti-collision frame 1, wherein the anti-collision frame 1 is spherical, and the interior of the anti-collision frame 1 is hollow; a circular ring 2 is horizontally arranged in the middle of the anti-collision frame 1, and a base 3 is arranged in the middle of the circular ring 2; the upper end of the base 3 is provided with a support rod 4, the top of the support rod 4 is provided with a placing table 5, the middle of the placing table 5 is provided with a camera 6, four corners of the bottom end of the base 3 are uniformly provided with propellers 7, and the propellers 7 can drive the whole unmanned aerial vehicle and the anti-collision frame 1 to fly; the placing table 5 is used for placing the camera 6, and the supporting rod 4 can support the placing table 5; the base 3 is used for placing the propeller 7, and the base 3 supports the camera 6.

Connecting rod 8 is worn to be equipped with in the middle part of bracing piece 4, and the both ends of connecting rod 8 are fixed to be set up on the inner wall of ring 2, and connecting rod 8 plays the effect of connecting unmanned aerial vehicle and ring 2.

The side that ring 2 is close to anticollision frame 1 evenly is provided with spherical connecting piece 9, and ring 2 is articulated through spherical connecting piece 9 and anticollision frame 1, and is articulated between ring 2 and the anticollision frame 1, and the unmanned aerial vehicle of being convenient for remains stable when flying, if unmanned aerial vehicle bumps, anticollision frame 1 can protect unmanned aerial vehicle to avoid damaging.

Camera 6's both sides all are provided with fixed block 10, and the inside of fixed block 10 is provided with searchlight 11, and camera 6 is used for shooing the material, and fixed block 10 plays the fixed action to camera 6, and searchlight 11 can carry out the light filling in the not strong region of illumination, prevents that the material of shooing is not clear enough.

A square groove 12 is formed in the middle of the top end of the placing table 5, a cushion pad is arranged at the bottom end of the square groove 12, the camera 6 is located in the square groove 12, and the cushion pad can play a certain buffering role when the camera 6 flies; the bottom of camera 6 and the interior bottom surface of square groove 12 all are provided with the magnet piece of mutual absorption, and the magnet piece can strengthen camera 6's stability when unmanned aerial vehicle flies.

Be provided with fixture block 13 on the fixed block 10 that is located camera 6 one side, seted up joint interface 14 on the fixed block 10 that is located camera 6 opposite side, and fixture block 13 and joint interface 14 joint, the both sides of fixture block 13 are provided with the elastic block, the inside both sides of joint interface 14 seted up with elastic block assorted draw-in groove, fixed block 10 can strengthen camera 6's stability.

Round hole 15 has all been seted up to upside and downside, left side and right side, front side and the rear side of anticollision frame 1, and round hole 15 unmanned aerial vehicle air flow when flying of being convenient for, and round hole 15 camera 6 of also being convenient for simultaneously shoots the material.

Anticollision frame 1 is made by transparent material, and transparent material is convenient for camera 6 and shoots the material.

When the unmanned aerial vehicle flies, the circular ring 2 is hinged with the anti-collision frame 1 through the spherical connecting piece 9, so that the unmanned aerial vehicle can keep relatively stable; the unmanned aerial vehicle can shoot materials through the camera 6 in the flying process, and when the unmanned aerial vehicle flies to an area with insufficient light, light can be supplemented through the searchlight 11; the fixed block 10 can enhance the stability of the camera 6, and meanwhile, the camera 6 and the magnet blocks in the square groove 12 can also enhance the stability, so that the camera 6 is prevented from falling off when the unmanned aerial vehicle flies; the round holes 15 formed in the anti-collision frame 1 and the transparent material of the anti-collision frame 1 are convenient for the camera 6 to shoot materials; if the unmanned aerial vehicle is collided and falls to the ground, the spherical anti-collision frame 1 can protect the unmanned aerial vehicle in the interior from being damaged; the clamping relation between the fixing blocks 10 is convenient for taking down the camera 6 from the square groove 12 after shooting is finished; this kind of anti-collision device of unmanned aerial vehicle wing through the articulated relation between unmanned aerial vehicle and spherical anticollision frame 1, effectively ensures the security of unmanned aerial vehicle when flying.

In the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention.

In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

Finally, it should be noted that: 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 changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the utility model. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The anti-collision device for the wings of the unmanned aerial vehicle comprises an anti-collision frame (1), and is characterized in that the anti-collision frame (1) is spherical, and the interior of the anti-collision frame (1) is hollow; a circular ring (2) is horizontally arranged in the middle of the anti-collision frame (1), and a base (3) is arranged in the middle of the circular ring (2); the upper end of base (3) is provided with bracing piece (4), the top of bracing piece (4) is provided with places platform (5), and the middle part of placing platform (5) is provided with camera (6), the bottom four corners of base (3) evenly is provided with screw (7).

2. The anti-collision device for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein the support rod (4) is provided with a connecting rod (8) in the middle, and two ends of the connecting rod (8) are fixedly arranged on the inner wall of the ring (2).

3. The anti-collision device for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein the side of the circular ring (2) close to the anti-collision frame (1) is uniformly provided with spherical connecting pieces (9), and the circular ring (2) is hinged with the anti-collision frame (1) through the spherical connecting pieces (9).

4. A collision avoidance device for a wing of a drone according to claim 1, characterized in that the camera (6) is provided with a fixed block (10) on both sides and inside the fixed block (10) is provided with a searchlight (11).

5. The anti-collision device for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein a square groove (12) is formed in the middle of the top end of the placing table (5), a cushion pad is arranged at the bottom end of the square groove (12), and the camera (6) is located in the square groove (12).

6. The anti-collision device for the wings of the unmanned aerial vehicle as claimed in claim 4, wherein a clamping block (13) is arranged on the fixing block (10) on one side of the camera (6), a clamping interface (14) is arranged on the fixing block (10) on the other side of the camera (6), and the clamping block (13) is clamped with the clamping interface (14).

7. The anti-collision device for the wings of the unmanned aerial vehicle as claimed in claim 1, wherein the anti-collision frame (1) is provided with round holes (15) on the upper side and the lower side, the left side and the right side, and the front side and the rear side.

8. The device according to claim 1, characterized in that the frame (1) is made of transparent material.