CN205589526U

CN205589526U - Unmanned aerial vehicle

Info

Publication number: CN205589526U
Application number: CN201620366197.5U
Authority: CN
Inventors: 刘磊
Original assignee: Gamecyber Technology Ltd; Airmada Technology Inc
Current assignee: Gamecyber Technology Ltd; Airmada Technology Inc
Priority date: 2016-04-27
Filing date: 2016-04-27
Publication date: 2016-09-21
Anticipated expiration: 2026-04-27

Abstract

The utility model discloses an unmanned aerial vehicle, including fuselage, screw, screw support and video camera, the screw install in the screw support, the screw support with the fuselage is connected, the fuselage is equipped with and holds the chamber, the video camera is located hold the intracavity, the camera lens orientation of video camera the outside of fuselage. The utility model provides an unmanned aerial vehicle, unmanned aerial vehicle's fuselage is equipped with and holds the chamber, and during the video camera was located and is held the chamber, the chamber that holds of fuselage was arranged in towards the outside of fuselage, video camera to the camera lens of video camera, and the video camera can be protected betterly to the fuselage, has reduced the damage of video camera or has lost, and the chamber that holds of fuselage is arranged in to the video camera, and unmanned aerial vehicle simple structure just conveniently carries.

Description

Unmanned plane

Technical field

This utility model relates to vehicle technology field, particularly relates to a kind of unmanned plane.

Background technology

UAV is called for short " unmanned plane ", is to utilize radio robot and the programme-control dress provided for oneself Put the not manned vehicle of manipulation.

Unmanned plane photography of taking photo by plane is using UAV as aerial platform, with airborne sensory equipment, such as height Resolution CCD digital camera, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain Win the confidence breath, with computer, image information is processed, and be fabricated to image according to certain required precision.

Existing used unmanned plane, the fuselage of unmanned plane and used camera separate design, thus make Become camera to expose to fuselage, can not get the protection of fuselage, thus camera is easily damaged or loses；And This unmanned plane is bulky, and structure is complicated, goes out to carry inconvenience.

Utility model content

Based on this, it is necessary to for fuselage and the camera separate design of unmanned plane, thus cause camera to hold Fragile or lose and go out to carry the problem of inconvenience a kind of unmanned plane is provided.

A kind of unmanned plane, including fuselage, propeller, propeller bracket and camera, described propeller is installed In described propeller bracket, described propeller bracket is connected with described fuselage, and described fuselage is provided with receiving chamber, Described camera is located at described receiving intracavity, and the camera lens of described camera is towards the outside of described fuselage.

The unmanned plane that this utility model provides, the fuselage of unmanned plane is provided with receiving chamber, and camera is located at receiving chamber In, the camera lens of camera is towards the outside of fuselage.Camera is placed in the receiving chamber of fuselage, and fuselage can be relatively Protect camera well, decrease damage or the loss of camera；And camera is placed in the receiving chamber of fuselage In, unmanned plane simple in construction and being convenient for carrying.

Wherein in an embodiment, described receiving chamber is located at described fuselage and is positioned at the head of described unmanned plane One end.

Wherein in an embodiment, described camera is detachably located at described receiving intracavity.

Wherein in an embodiment, the shape in described receiving chamber and the mating shapes of described camera.

Wherein in an embodiment, the end in described receiving chamber is provided with for stopping that described camera departs from institute Stating the stop part of fuselage, described stop part is arranged around the camera lens of described camera.

Wherein in an embodiment, the camera lens of described camera is circular, and the internal diameter of described stop part is less than The external diameter of described camera lens.

Wherein in an embodiment, the inside in described receiving chamber is provided with lobe, the camera lens of described camera It is arranged between described stop part and described lobe.

Wherein in an embodiment, described fuselage is streamlined.

Wherein in an embodiment, described unmanned plane also includes the spike being located at the described fuselage left and right sides, Described fuselage both sides are equipped with a spike described in two.

Accompanying drawing explanation

The structure chart of the unmanned plane that Fig. 1 provides for this utility model embodiment；

Fig. 2 is the partial sectional view of Fig. 1；

Fig. 3 is the enlarged drawing in Fig. 2 at A.

Detailed description of the invention

For the ease of understanding this utility model, below with reference to relevant drawings, this utility model is carried out more comprehensively Description.Accompanying drawing gives preferred embodiment of the present utility model.But, this utility model can be to be permitted The most different forms realizes, however it is not limited to embodiment described herein.On the contrary, provide these to implement The purpose of example is to make the understanding to disclosure of the present utility model more thorough comprehensively.

It should be noted that when element is referred to as " being fixed on " another element, and it can be directly at another On individual element or element placed in the middle can also be there is.When an element is considered as " connection " another yuan Part, it can be directly to another element or may be simultaneously present centering elements.Used herein Term " vertical ", " level ", "left", "right" and similar statement simply to illustrate that mesh 's.

Unless otherwise defined, all of technology used herein and scientific terminology with belong to of the present utility model The implication that those skilled in the art are generally understood that is identical.Institute in description of the present utility model herein The term used is intended merely to describe the purpose of specific embodiment, it is not intended that in limiting this utility model. Term as used herein " and/or " include the arbitrary and all of one or more relevant Listed Items Combination.

Seeing Fig. 1-Fig. 3, this utility model embodiment provides a kind of unmanned plane, including fuselage 10, propeller 20, propeller bracket 30 and camera 40, propeller 20 is installed on propeller bracket 30, propeller bracket 30 are connected with fuselage 10, and fuselage 10 is provided with receiving chamber 12, and camera 40 is located in receiving chamber 12, photography The camera lens 42 of machine 40 is towards the outside of fuselage 10.

The unmanned plane that this utility model embodiment provides, the fuselage 10 of unmanned plane is provided with receiving chamber 12, camera 40 are located in receiving chamber 12, and the camera lens 42 of camera 40 is placed in towards the outside of fuselage 10, camera 40 In the receiving chamber 12 of fuselage, fuselage 10 can preferably protect camera 40, decreases the damage of camera 40 Go bad or lose；And camera 40 is placed in the receiving chamber 12 of fuselage 10, unmanned plane simple in construction and convenience Carry.

The camera lens 42 of above-mentioned camera 40 is towards the outside of fuselage 10, not affect the normal of camera 40 Work.Specifically, seeing Fig. 1, the quantity of above-mentioned propeller 20 is 4, is respectively arranged in propeller and props up The left and right sides of frame 30, under the drive of motor, propeller 20 rotates, thus drive propeller bracket 30 and Fuselage 10 moves, and the camera 40 accommodated in chamber 12 being located at fuselage 10 is photographed.

See Fig. 1 and Fig. 2, accommodate chamber 12 and be located at one end that fuselage 10 is positioned at the head of unmanned plane, i.e. photograph Machine 40 is installed on the front end of fuselage 10, and above-mentioned front end is the one end in the direction advanced towards unmanned plane.When So, accommodating chamber 12 and can also be located at the rear end of fuselage 10, above-mentioned rear end is corresponding with above-mentioned front end to be arranged at Above-mentioned fuselage 10.

In the present embodiment, camera 40 detachably be located at receiving chamber 12 in, i.e. camera 40 can at any time from The receiving chamber 12 of fuselage 10 is taken out, it is simple to carry out camera 40 checking work.

Specifically, the shape in chamber 12 and the mating shapes of camera 40 are accommodated.Receiving chamber 12 can be set Cavity size identical with the profile size of camera 40, so that camera 40 is just installed on above-mentioned receiving In chamber 12.

Seeing Fig. 3, in the present embodiment, the end accommodating chamber 12 is provided with for stopping that camera 40 departs from institute Stating the stop part 14 of fuselage, stop part 14 is arranged around the camera lens 42 of camera 40, not affect camera The work of the camera lens 42 of 40.Specifically, stop part 14 could be arranged to opening-closing structure, when opening stop part When 14, camera 40 can be taken out from the receiving chamber 12 of fuselage 10, when stop part 14 closes, Camera 40 can be fixed on receiving chamber 12 internal.

In the present embodiment, the camera lens 42 of camera 40 is circular, and the internal diameter of stop part 14 is less than camera lens 42 External diameter, in order to block the camera lens 42 of camera 40.The set-up mode of above-mentioned stop part 14, Bu Huiying Ring the normal work of the eyeglass of the camera lens 42 to camera.

Seeing Fig. 3, in the present embodiment, the inside accommodating chamber 12 is provided with lobe 16, camera 40 Camera lens 42 is arranged between stop part 14 and lobe 16.Common work at stop part 14 with lobe 16 It is firmly secured to accommodate in chamber 12 by camera 40 with lower.Specifically, in fuselage 10, it is additionally provided with circuit Plate 50, camera 40 is connected with circuit board 50.

In the present embodiment, it is also possible to it is streamlined for arranging fuselage 10, and unmanned plane also includes being located at fuselage 10 A spike 18 of the left and right sides, fuselage 10 both sides are equipped with two spikes 18.When unmanned plane lands, Can be easy to be supported in ground under the effect of a spike 18.

Embodiment described above only have expressed several embodiments of the present utility model, its describe more concrete and In detail, but therefore can not be interpreted as the restriction to this utility model the scope of the claims.It should be pointed out that, For the person of ordinary skill of the art, without departing from the concept of the premise utility, it is also possible to Making some deformation and improvement, these broadly fall into protection domain of the present utility model.Therefore, this utility model The protection domain of patent should be as the criterion with claims.

Claims

1. a unmanned plane, including fuselage, propeller, propeller bracket and camera, described propeller is pacified Being loaded on described propeller bracket, described propeller bracket is connected with described fuselage, it is characterised in that described machine Body is provided with receiving chamber, and described camera is located at described receiving intracavity, and the camera lens of described camera is towards described machine The outside of body.

Unmanned plane the most according to claim 1, it is characterised in that described fuselage is located in described receiving chamber It is positioned at one end of the head of described unmanned plane.

Unmanned plane the most according to claim 1, it is characterised in that described camera is detachably located at institute State receiving intracavity.

Unmanned plane the most according to claim 1, it is characterised in that the shape in described receiving chamber is with described The mating shapes of camera.

Unmanned plane the most according to claim 1, it is characterised in that the end in described receiving chamber is provided with use In stopping that described camera departs from the stop part of described fuselage, described stop part is around the camera lens of described camera Arrange.

Unmanned plane the most according to claim 5, it is characterised in that the camera lens of described camera is circular, The internal diameter of described stop part is less than the external diameter of described camera lens.

Unmanned plane the most according to claim 5, it is characterised in that the inside in described receiving chamber is provided with convex The portion of rising, the shot card of described camera is located between described stop part and described lobe.

Unmanned plane the most according to claim 1, it is characterised in that described fuselage is streamlined.

Unmanned plane the most according to claim 1, it is characterised in that described unmanned plane also includes being located at institute Stating a spike of the fuselage left and right sides, described fuselage both sides are equipped with a spike described in two.