CN215436907U

CN215436907U - Anti-collision unmanned aerial vehicle equipment

Info

Publication number: CN215436907U
Application number: CN202121083581.1U
Authority: CN
Inventors: 曹郁
Original assignee: Jiangsu Langwei Intelligent Technology Co ltd
Current assignee: Jiangsu Langwei Intelligent Technology Co ltd
Priority date: 2021-05-19
Filing date: 2021-05-19
Publication date: 2022-01-07
Anticipated expiration: 2031-05-19

Abstract

The utility model discloses anti-collision unmanned aerial vehicle equipment which comprises an unmanned aerial vehicle body, an annular base and a mounting seat, wherein the mounting seat is fixedly connected to the top of the unmanned aerial vehicle body, wings are fixedly connected to the periphery of the unmanned aerial vehicle body, and a buffer column is fixedly connected to the bottom of the unmanned aerial vehicle body. According to the utility model, the contact area of the unmanned aerial vehicle and the ground can be increased through the annular base, the buffer column can move towards the inner cavity of the limiting sleeve under the stress when the unmanned aerial vehicle is in contact with the ground, the buffer column can extrude the air cushion when moving downwards, the air cushion can deform under the stress, the gas in the inner cavity of the air cushion can be discharged through the exhaust pipe, the air cushion can buffer the impact force when deforming, the air cushion can suck air through the exhaust pipe to reset, and the problems that the unmanned aerial vehicle can generate large impact force when falling from high altitude in the use process, the unmanned aerial vehicle can be collided due to the impact force, the unmanned aerial vehicle can be damaged, and the service life of the unmanned aerial vehicle can be shortened are solved.

Description

Anti-collision unmanned aerial vehicle equipment

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to collision-prevention unmanned aerial vehicle equipment.

Background

Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and the program control device of self-contained to control, or by the vehicle-mounted computer completely or intermittently independently operate, compare with manned aircraft, unmanned aerial vehicle often more is fit for those too foolproof, dirty or dangerous tasks, unmanned aerial vehicle is according to the application, can be for military use and civilian use, for military use aspect, unmanned aerial vehicle divide into scout and target plane, at present in the field wide application such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, rescue disaster, observe wild animal, control infectious disease, survey and drawing, news report, electric power inspection, relief disaster, movie & TV are shot and are made romantic, the great use that has expanded unmanned aerial vehicle itself.

Unmanned aerial vehicle descends from the high altitude in the use and can produce great impact force, and the impact force can lead to unmanned aerial vehicle to receive and collide with, consequently can lead to unmanned aerial vehicle's damage, shortens its life.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide anti-collision unmanned aerial vehicle equipment which has the anti-collision advantage and solves the problems that when an unmanned aerial vehicle lands from high altitude in the using process, a large impact force is generated, and the impact force can cause the unmanned aerial vehicle to be collided, so that the unmanned aerial vehicle is damaged and the service life of the unmanned aerial vehicle is shortened.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides an unmanned aerial vehicle equipment of preventing colliding with, includes unmanned aerial vehicle body, annular base and mount pad, the top fixedly connected with mount pad of unmanned aerial vehicle body, equal fixedly connected with wing all around of unmanned aerial vehicle body, the bottom fixedly connected with buffering post of unmanned aerial vehicle body, the inner wall fixedly connected with support of annular base, one side fixedly connected with limit sleeve of annular base inner wall is kept away from to the support, the bottom of buffering post extends to limit sleeve's inner chamber, limit sleeve inner chamber's bottom fixedly connected with air cushion, the surface intercommunication of air cushion has the blast pipe, the blast pipe runs through to limit sleeve's outside, the buffering post is located the bottom of limit sleeve inner chamber one end and the top fixed connection of air cushion.

Preferably, the inner cavity of the mounting seat is movably connected with a mounting rod, and the top of the mounting rod is fixedly connected with a camera.

Preferably, the mounting rod is located both sides of mount pad inner chamber one end and has all seted up spacing spout, the inner chamber sliding connection of spacing spout has spacing slider, spacing slider keeps away from one side of spacing spout inner chamber and the inner wall fixed connection of mount pad.

Preferably, the surface of the mounting rod at one end of the mounting seat inner cavity is provided with a threaded hole.

Preferably, the surface of the mounting seat is in threaded connection with a fastening bolt, and the fastening bolt is in threaded connection with an inner cavity of the threaded hole.

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

1. according to the utility model, the contact area of the unmanned aerial vehicle and the ground can be increased through the annular base, the buffer column can move towards the inner cavity of the limiting sleeve under the stress when the unmanned aerial vehicle is in contact with the ground, the buffer column can extrude the air cushion when moving downwards, the air cushion can deform under the stress, the gas in the inner cavity of the air cushion can be discharged through the exhaust pipe, the air cushion can buffer the impact force when deforming, the air cushion can suck air through the exhaust pipe to reset, and the problems that the unmanned aerial vehicle can generate large impact force when falling from high altitude in the use process, the unmanned aerial vehicle can be collided due to the impact force, the unmanned aerial vehicle can be damaged, and the service life of the unmanned aerial vehicle can be shortened are solved.

2. The camera mounting device has the advantages that the camera mounting effect is achieved by the aid of the mounting seat, the mounting rod and the camera, the mounting position of the mounting rod is limited by the aid of the limiting sliding groove and the limiting sliding block, and the mounting rod is fixed by the aid of the threaded holes and the fastening bolts.

Drawings

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

FIG. 2 is a schematic cross-sectional view of the position limiting sleeve according to the present invention;

fig. 3 is a schematic cross-sectional view of the mounting base of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. an airfoil; 3. a buffer column; 4. a limiting sleeve; 5. an air cushion; 6. an exhaust pipe; 7. an annular base; 8. a support; 9. a mounting seat; 10. mounting a rod; 11. a camera; 12. a limiting chute; 13. a limiting slide block; 14. a threaded hole; 15. and fastening the bolt.

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.

The unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wings 2, buffer columns 3, limiting sleeves 4, air cushions 5, exhaust pipes 6, an annular base 7, a support 8, a mounting seat 9, a mounting rod 10, a camera 11, a limiting sliding groove 12, a limiting sliding block 13, threaded holes 14 and fastening bolts 15, wherein the parts are all universal standard parts or parts known by technical personnel in the field, and the structure and the principle of the unmanned aerial vehicle are known by technical manuals or conventional experimental methods.

Referring to fig. 1-3, an anti-collision unmanned aerial vehicle device comprises an unmanned aerial vehicle body 1, an annular base 7 and a mounting seat 9, the mounting seat 9 is fixedly connected to the top of the unmanned aerial vehicle body 1, wings 2 are fixedly connected to the periphery of the unmanned aerial vehicle body 1, a buffering column 3 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, a support 8 is fixedly connected to the inner wall of the annular base 7, a limiting sleeve 4 is fixedly connected to one side of the support 8 away from the inner wall of the annular base 7, the bottom of the buffering column 3 extends to the inner cavity of the limiting sleeve 4, an air cushion 5 is fixedly connected to the bottom of the inner cavity of the limiting sleeve 4, an exhaust pipe 6 is communicated with the surface of the air cushion 5, the exhaust pipe 6 penetrates through the outer part of the limiting sleeve 4, the bottom of the buffering column 3 at one end of the inner cavity of the limiting sleeve 4 is fixedly connected with the top of the air cushion 5, and the contact area between the unmanned aerial vehicle and the ground can be increased through the annular base 7, buffer column 3 can receive the force to limit sleeve 4's inner chamber motion when unmanned aerial vehicle contacts with ground, buffer column 3 can extrude air cushion 5 when downstream, air cushion 5 atress can produce deformation, the gas in air cushion 5 inner chamber can be discharged through blast pipe 6, both be the buffering to the impact force when air cushion 5 deforms, air cushion 5 inhales the air and then resets through blast pipe 6, unmanned aerial vehicle descending from the high altitude in the use can produce great impact force, the impact force can lead to unmanned aerial vehicle to receive and collide with, consequently, can lead to unmanned aerial vehicle's damage, shorten its life's problem.

In this embodiment, specifically, the inner cavity of the mounting base 9 is movably connected with a mounting rod 10, the top of the mounting rod 10 is fixedly connected with a camera 11, and the effect of mounting the camera 11 is achieved by arranging the mounting base 9, the mounting rod 10 and the camera 11.

In this embodiment, it is concrete, spacing spout 12 has all been seted up to the both sides that installation pole 10 is located mount pad 9 inner chamber one end, and the inner chamber sliding connection of spacing spout 12 has spacing slider 13, and spacing slider 13 keeps away from one side of spacing spout 12 inner chamber and the inner wall fixed connection of mount pad 9, through setting up spacing spout 12 and spacing slider 13, has played and has carried out spacing effect to the mounted position of installation pole 10.

In this embodiment, specifically, a threaded hole 14 is formed in the surface of the mounting rod 10 at one end of the inner cavity of the mounting seat 9.

In this embodiment, specifically, the surface of the mounting seat 9 is connected with the fastening bolt 15 through a thread, the fastening bolt 15 is connected with the inner cavity of the threaded hole 14 through a thread, and the threaded hole 14 and the fastening bolt 15 are arranged, so that the effect of fixing the mounting rod 10 is achieved.

During the use, can increase the area of contact of unmanned aerial vehicle and ground through ring base 7, cushion column 3 can receive the atress to limit sleeve 4's inner chamber motion when unmanned aerial vehicle contacts with ground, cushion column 3 can extrude air cushion 5 when the downstream, air cushion 5 atress can produce deformation, the gas in air cushion 5 inner chamber can be discharged through blast pipe 6, both be the buffering to the impact force when air cushion 5 deforms, air cushion 5 inhales the air and then resets through blast pipe 6, unmanned aerial vehicle descending from the high altitude in the use can produce great impact force, the impact force can lead to unmanned aerial vehicle to receive and collide with, consequently, can lead to unmanned aerial vehicle's damage, shorten its life's problem.

The standard parts used in the present application document can be purchased from the market, and can be customized according to the description of the specification and the accompanying drawings, the specific connection mode of each part adopts the conventional means of mature bolt, rivet, welding and the like in the prior art, the machines, parts and equipment adopt the conventional models in the prior art, the control mode is automatically controlled by a controller, the control circuit of the controller can be realized by simple programming of technicians in the field, the control circuit belongs to the common knowledge in the field, and the present application document is mainly used for protecting mechanical devices, so the control mode and the circuit connection are not explained in detail in the present application.

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. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

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. The utility model provides a prevent unmanned aerial vehicle equipment that collides with, includes unmanned aerial vehicle body (1), annular base (7) and mount pad (9), its characterized in that: the top of the unmanned aerial vehicle body (1) is fixedly connected with a mounting seat (9), the periphery of the unmanned aerial vehicle body (1) is fixedly connected with wings (2), the bottom of the unmanned aerial vehicle body (1) is fixedly connected with a buffer column (3), the inner wall of the annular base (7) is fixedly connected with a support (8), one side of the bracket (8) far away from the inner wall of the annular base (7) is fixedly connected with a limiting sleeve (4), the bottom of the buffer column (3) extends to the inner cavity of the limit sleeve (4), the bottom of the inner cavity of the limit sleeve (4) is fixedly connected with an air cushion (5), the surface of the air cushion (5) is communicated with an exhaust pipe (6), the exhaust pipe (6) penetrates to the outside of the limit sleeve (4), the bottom of the buffer column (3) at one end of the inner cavity of the limit sleeve (4) is fixedly connected with the top of the air cushion (5).

2. The anti-collision unmanned aerial vehicle device according to claim 1, wherein: the inner cavity of the mounting seat (9) is movably connected with a mounting rod (10), and the top of the mounting rod (10) is fixedly connected with a camera (11).

3. The anti-collision unmanned aerial vehicle device according to claim 2, wherein: spacing spout (12) have all been seted up to the both sides that installation pole (10) are located mount pad (9) inner chamber one end, the inner chamber sliding connection of spacing spout (12) has spacing slider (13), spacing slider (13) keep away from the inner wall fixed connection of one side of spacing spout (12) inner chamber and mount pad (9).

4. The anti-collision unmanned aerial vehicle device according to claim 2, wherein: the surface of the mounting rod (10) at one end of the inner cavity of the mounting seat (9) is provided with a threaded hole (14).

5. The anti-collision unmanned aerial vehicle device according to claim 4, wherein: the surface of the mounting seat (9) is in threaded connection with a fastening bolt (15), and the fastening bolt (15) is in threaded connection with an inner cavity of the threaded hole (14).