CN205971790U - Multifunctional unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a multifunctional unmanned aerial vehicle, including fuselage platform, two first interfaces, two second interfaces, fixed wing and the screw machine wings, two first interface respectively the symmetry set up in the both ends of fuselage platform on width direction, two two are placed in the symmetry respectively to the second interface the inside of first interface, the fixed wing can with first interface fixed connection, the screw machine wing can with second interface fixed connection. The utility model discloses a first interface and second interface, wherein first interface is used for connecting the fixed wing, and the second interface is used for connecting the screw machine wing, according to the demand of using the scene, can select the installation fixed wing or the screw machine wing on the fuselage platform, has greatly richened unmanned aerial vehicle's applied scene, realizes that unmanned aerial vehicle's multi -functionalization is a tractor serves several purposes.

Description

A kind of multi-functional unmanned plane

Technical field

This utility model is related to unmanned plane field, particularly to a kind of unmanned plane.

Background technology

UAV referred to as " unmanned plane ", english abbreviation is " UAV ", using radio robot with provide for oneself The not manned aircraft that presetting apparatus manipulates.Unmanned plane presses application, can be divided into military and civilian.Military aspect, unmanned Machine is divided into reconnaissance plane and target drone.Civilian aspect, is the real firm need of unmanned plane；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express delivery Transport, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, system Make in the various environment such as romance and use.The function of the airborne equipment due to carrying on unmanned plane is different, steady to unmanned plane Qualitative, speed, mobility, wind resistance requirement is different, and the working environment being typically different will use different unmanned planes, and The wing of existing unmanned plane and fuselage are all unitary design, single function, people be accomplished by great amount of investment go to purchase multiple Unmanned plane.

Utility model content

This utility model is to overcome above-mentioned situation not enough, it is desirable to provide a kind of multi-functional nothing being suitable for multiple operative scenario Man-machine.

A kind of multi-functional unmanned plane, including：Fuselage platform, two first interfaces, two second interfaces, fixing wing and spiral shell Rotation wing；Two described first interfaces are respectively symmetrically the two ends being arranged at described fuselage platform in the direction of the width；Described in two Second interface is respectively symmetrically the inside being built in two described first interfaces；Described fixing wing can be solid with described first interface Fixed connection；Described spiral wing can be fixedly connected with described second interface.

Further, also include：Two the 3rd interfaces；Two described 3rd interfaces are respectively symmetrically and are arranged at described fuselage and put down Platform two ends in the longitudinal direction；Two described 3rd interfaces are connected to described spiral wing.

Further, the 4th interface that also includes being uniformly arranged along described fuselage platform periphery, the 5th interface, the 6th interface With the 7th interface；

Median plane in the direction of the width is symmetrical with respect to described fuselage platform for described 4th interface and described 5th interface Median plane in the direction of the width symmetrically sets with respect to described fuselage platform for setting, described 6th interface and described 7th interface Put, median plane in the longitudinal direction is symmetrical arranged with respect to described fuselage platform for described 4th interface and described 6th interface, Median plane in the longitudinal direction is symmetrical arranged with respect to described fuselage platform for described 5th interface and described 7th interface, and the 4th Interface, the 5th interface, the 6th interface and the 7th interface are connected to described spiral wing.

Further, the axis angle of the axis of described 4th interface and described 6th interface is 80 degree, and the described 5th connects The axis angle of the axis of mouth and described 7th interface is 80 degree.

Further, described spiral wing includes：Support arm and propeller；One end of described support arm can connect with second Mouth is fixedly connected, and the other end is connected with described propeller.

Further, each described support arm correspondence is connected with two propellers, and two spiral shells being connected with same support arm Rotation oar is coaxially disposed the both sides up and down in described support arm respectively.

Further, described second interface be shaped as polygon and the end with described spiral wing is mutually adapted.

This utility model includes first interface and second interface, and wherein first interface is used for the wing that is connected, and second connects Mouth is used for connecting spiral wing, according to the demand of application scenarios, can select to install fixing wing or spiral shell on fuselage platform Rotation wing, it can thus be appreciated that unmanned plane provided herein is vdiverse in function, is greatly enriched the application scenarios of unmanned plane.Separately Outward, two effects are at least brought in the inside that second interface is arranged at first interface by this utility model：First, avoiding in fuselage Platform surface many places arrange interface, are conducive to save space；Second, avoiding the defect having interface to expose when using, keep The integrity of fuselage platform is so that unmanned plane more meets aerodynamic requirement, the more conducively control to unmanned plane.

Additional aspect of the present utility model and advantage will be set forth in part in the description, partly will be from explained below In become obvious, or recognized by practice of the present utility model.

Brief description

Fig. 1 is the overlooking the structure diagram of this utility model middle fuselage platform；

Fig. 2 is top view when this utility model middle fuselage platform is connected with fixing wing；

Fig. 3 is the main structure diagram of this utility model middle fuselage platform；

Fig. 4 is top view when this utility model fuselage platform is connected with spiral wing.

Accompanying drawing marks：

1. fuselage platform；

11. first interfaces；

12. second interfaces；

13. the 3rd interfaces；

14. the 4th interfaces；

15. the 5th interfaces；

16. the 6th interfaces；

17. the 7th interfaces；

3. fixing wing；

5. spiral wing；

51. support arms；

53. propellers.

Specific embodiment

Embodiment of the present utility model is described below in detail, the example of described embodiment is shown in the drawings, wherein ad initio To the element that same or similar label represents same or similar element or has same or like function eventually.Below by ginseng The embodiment examining Description of Drawings is exemplary it is intended to be used for explaining this utility model, and it is not intended that to this utility model Restriction.

Please with reference to Fig. 1 to Fig. 4, a kind of multi-functional unmanned plane, including 1, two first interfaces of fuselage platform 11, two Second interface 12, fixing wing 3 and spiral wing 5.Two first interfaces 11 are respectively symmetrically and are arranged at fuselage platform 1 in width side Two ends upwards.Two second interfaces 12 are respectively symmetrically the inside being built in two first interfaces 11.Fixing wing 3 can be with the One interface 11 is fixedly connected.Spiral wing 5 can be fixedly connected with second interface 12.When needing to be assembled into fixing wing unmanned plane When, it is inserted into two fixing wings 3 in two first interfaces 11.When needing to be assembled into many rotor wing unmanned aerial vehicles, at two second Interface 12 is inserted into two spiral wings 5.By above-mentioned design, according to the demand of application scenarios, can select in fuselage platform Upper installation fixes wing or spiral wing, is greatly enriched the application scenarios of unmanned plane, realizes the multifunction of unmanned plane I.e. a tractor serves several purposes.In addition, two effects are at least brought in the inside that second interface is arranged at first interface by this utility model：Its One, it is to avoid interface is set in fuselage platform surface many places, is conducive to save space；Second, avoid thering is interface when using The defect exposing, maintains the integrity of fuselage platform so that unmanned plane more meets aerodynamic requirement, more conducively to no Man-machine control.Fixing wing 3 is connected fuselage platform as needed with spiral wing 5 and brings outstanding portability simultaneously, can Easily putting in packsack it is only necessary to install in working site, it is to avoid in prior art, wing is fixedly connected on The design of fuselage platform 1 leads to the problem that wing leads to fracture in road because jolting.

Further, fuselage platform 1 also includes two the 3rd interfaces 13.Two the 3rd interfaces 13 are respectively symmetrically and are arranged at Fuselage platform 1 two ends in the longitudinal direction.Two the 3rd interfaces 13 are connected to spiral wing 5.When two second interfaces 12 and two the 3rd interfaces 13 when being inserted into two spiral wings 5, define four rotor wing unmanned aerial vehicles, possess good mobility.

Further, also include that the 4th interface 14 being uniformly arranged, the 5th interface the 15, the 6th connect along fuselage platform 1 periphery Mouth 16 and the 7th interface 17.4th interface 14 and the 5th interface 15 median plane pair in the direction of the width with respect to fuselage platform 1 Median plane in the direction of the width is symmetrical arranged with respect to fuselage platform 1 to claim setting, the 6th interface 16 and the 7th interface 17, and the 4th Median plane in the longitudinal direction is symmetrical arranged with respect to fuselage platform 1 for interface 14 and the 6th interface 16, the 5th interface 15 and With respect to fuselage platform 1, median plane in the longitudinal direction is symmetrical arranged seven interfaces 17, the 4th interface 14, the 5th interface 15, Six interfaces 16 and the 7th interface 17 are connected to spiral wing 5.By designing connecing of more multi-link wing in fuselage platform 1 Mouthful, improve the load-carrying ability of unmanned plane, enrich the applied environment of unmanned plane further, meet working environment to stability, speed Degree, mobility, the requirement of wind resistance.

Further, the angle of the 4th interface 14 and the 6th interface 16 is 80 degree, the 5th interface 15 and the 7th interface 17 Angle is 80 degree, stability highest, and wind resistance is best.

Further, spiral wing 5 includes support arm 51 and propeller 53.One end of support arm 51 can be with second interface 12 are fixedly connected, and the other end is connected with propeller 53.During flight, the rotary motion of propeller 53 drives support arm and support arm The fuselage platform being fixedly connected circles in the air, and handling and stability is strong.

Further, each described support arm 51 correspondence is connected with two propellers 53, and be connected with same support arm 51 Two propellers 53 are coaxially disposed respectively in the both sides up and down of described support arm 51.With respect to single screw, load-carrying ability can arrive Further raising.

Further, second interface 12 be shaped as polygon and the end with spiral wing 5 is mutually adapted.Polygon connects Mouth design makes second interface 12 be connected more firm with spiral wing 5, and in wind resistance, spiral wing 5 is difficult to rotate.

In description of the present utility model it is to be understood that term " " center ", " longitudinal ", " horizontal ", " length ", " width Degree ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward ", " suitable The orientation of instruction such as hour hands ", " counterclockwise ", " axial ", " radially ", " circumferential " or position relationship are based on orientation shown in the drawings Or position relationship, be for only for ease of description this utility model and simplify description, rather than instruction or hint indication device or Element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to limit of the present utility model System.

In this utility model, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection ", " Gu Fixed " etc. term should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or integral；Can be It is mechanically connected or electrically connect；Can be to be joined directly together it is also possible to be indirectly connected to by intermediary, can be two The connection of element internal or the interaction relationship of two elements.For the ordinary skill in the art, can basis Concrete condition understands concrete meaning in this utility model for the above-mentioned term.

In this utility model, unless otherwise clearly defined and limited, fisrt feature second feature " on " or D score Can be the first and second feature directly contacts, or the first and second features pass through intermediary mediate contact.And, first is special Levy second feature " on ", " top " and " above " but fisrt feature directly over second feature or oblique upper, or only Represent that fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " permissible Be fisrt feature immediately below second feature or obliquely downward, or be merely representative of fisrt feature level height and be less than second feature.

In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show The description of example " or " some examples " etc. means specific features, structure, material or the spy describing with reference to this embodiment or example Point is contained at least one embodiment of the present utility model or example.In this manual, the schematic table to above-mentioned term State and be necessarily directed to identical embodiment or example.And, the specific features of description, structure, material or feature are permissible Any one or more embodiments or example combine in an appropriate manner.Additionally, in the case of not conflicting, this area Technical staff the feature of the different embodiments described in this specification or example and different embodiment or example can be entered Row combines and combines.

Although of the present utility model embodiment has been shown and described above it is to be understood that above-described embodiment is Exemplary it is impossible to be interpreted as that those of ordinary skill in the art is in scope of the present utility model to restriction of the present utility model Interior above-described embodiment can be changed, change, replacing and modification.

Claims (7)

1. a kind of multi-functional unmanned plane is it is characterised in that include：Fuselage platform, two first interfaces, two second interfaces, solid Determine wing and spiral wing；

Two described first interfaces are respectively symmetrically the two ends being arranged at described fuselage platform in the direction of the width；

Two described second interfaces are respectively symmetrically the inside being arranged at two described first interfaces；

Described fixing wing can be fixedly connected with described first interface；Described spiral wing can be fixed with described second interface Connect.

2. a kind of multi-functional unmanned plane according to claim 1 is it is characterised in that also include：Two the 3rd interfaces；Two Described 3rd interface is respectively symmetrically the two ends being arranged at described fuselage platform in the longitudinal direction；Two described 3rd interfaces are respectively It is connected with described spiral wing.

3. a kind of multi-functional unmanned plane according to claim 2 is it is characterised in that also include along described fuselage platform periphery The 4th interface, the 5th interface, the 6th interface and the 7th interface being uniformly arranged；

Median plane in the direction of the width is symmetrical arranged with respect to described fuselage platform for described 4th interface and described 5th interface, Median plane in the direction of the width is symmetrical arranged with respect to described fuselage platform for described 6th interface and described 7th interface, described Median plane in the longitudinal direction is symmetrical arranged with respect to described fuselage platform for 4th interface and described 6th interface, and the described 5th Median plane in the longitudinal direction is symmetrical arranged with respect to described fuselage platform for interface and described 7th interface, the 4th interface, Five interfaces, the 6th interface and the 7th interface are connected to described spiral wing.

4. a kind of multi-functional unmanned plane according to claim 3 is it is characterised in that the axis of described 4th interface and described The axis angle of the 6th interface is 80 degree, and the axis of described 5th interface and the axis angle of described 7th interface are 80 degree.

5. a kind of multi-functional unmanned plane according to claim 1 is it is characterised in that described spiral wing includes：Support arm And propeller；One end of described support arm can be fixedly connected with second interface, and the other end is connected with described propeller.

6. a kind of multi-functional unmanned plane according to claim 5 is it is characterised in that each described support arm corresponds to and two spiral shells Rotation oar is connected, and two propellers being connected with same support arm are coaxially disposed the both sides up and down in described support arm respectively.

7. a kind of multi-functional unmanned plane according to claim 1 is it is characterised in that being shaped as of described second interface is polygon The shape and end with described spiral wing is mutually adapted.