CN207826549U - It is a kind of can VTOL unmanned aerial vehicle platform - Google Patents
It is a kind of can VTOL unmanned aerial vehicle platform Download PDFInfo
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- CN207826549U CN207826549U CN201820133711.XU CN201820133711U CN207826549U CN 207826549 U CN207826549 U CN 207826549U CN 201820133711 U CN201820133711 U CN 201820133711U CN 207826549 U CN207826549 U CN 207826549U
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Abstract
The utility model discloses it is a kind of can VTOL unmanned aerial vehicle platform, including fuselage and wing, 4 propellers are provided on the wing, it is provided with the steering engine that verts on 2 propellers of the wing nose, when taking off, 4 propellers are vertically upward, fuselage is kept to stablize by 4 motors, and it takes off vertically by the realization of the pulling force of 4 propellers, after completion is taken off vertically, 2 propellers of front end vert being driven by the steering engine that verts, and a part of pulling force is for providing lift, and a part of pulling force is for drawing unmanned aerial vehicle platform flight forward；By above-mentioned setting, the operation difficulty of requirement and personnel of the unmanned aerial vehicle platform to landing runway is reduced, to only need smaller level land that lifting program can be completed, reduces overall cost；Simultaneously by the way that wing quick fixation structure and empennage quick fixation structure is arranged, the assembling of unmanned aerial vehicle platform and dismounting is made to greatly simplify.
Description
Technical field
The utility model is related to air vehicle technique field, more particularly to it is a kind of can VTOL unmanned aerial vehicle platform.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels
Or machine tool remote control station personnel are by equipment such as radars, to it into line trace, positioning, remote control, telemetering and Digital Transmission.Currently,
Aerial survey of unmanned aerial vehicle is widely used in the industries such as agricultural, traffic, geological prospecting, fire-fighting, electric inspection process.Unmanned aerial vehicle platform is for nobody
The movable basis of machine aerial survey, generally carries sensor by unmanned aerial vehicle platform, with certain height, speed according to Route reform, according to
Sensor mounted is observed ground on machine, obtains data, completes the collecting work of aerophotogrammetry data.
As the chief component of aerial survey of unmanned aerial vehicle technology, there are many kinds of the unmanned aerial vehicle platforms of class on the market, but these
Unmanned aerial vehicle platform usually has the following problems：1, stronger to the dependence of ground landing runway；2, takeoff and landing is to personnel's
It operates more demanding.Traditional aerial survey of unmanned aerial vehicle activity can take the mode of hand throwing or parachuting to solve these problems, but still
Face higher risk.
Utility model content
In view of the above technical problems, the purpose of this utility model be to provide it is a kind of can VTOL unmanned aerial vehicle platform, lead to
It crosses and the steering engine that verts is set in front of wing, make unmanned aerial vehicle platform that can realize VTOL.
In order to achieve the above objectives, a technical solution of the utility model use is：There is provided it is a kind of can VTOL nothing
Man-machine platform, including：Fuselage, is symmetrically arranged with wing at left and right sides of the fuselage, and the wing includes stage casing wing and outer
Section wing, the stage casing wing are fixedly arranged on the left and right sides of fuselage, and the stage casing wing is provided with close to one end of outer segment empennage
The rear and front end of a piece cantilever along fuselage length direction, the cantilever is respectively arranged with propeller, is arranged on the propeller
There is motor, the steering engine that verts is additionally provided on the motor of the cantilever front end, the cantilever is internally provided with a wing fast-assembling
Structure, the outer segment wing are connect by wing quick fixation structure with cantilever, and the two sides of tail of the fuselage is symmetrically arranged with empennage
Mounting groove, the empennage mounting groove is interior to be arranged with empennage by empennage quick fixation structure, and the inside of the fuselage is also equipped with battery
And flying control, the battery and the top for flying control are provided with hatchcover.
Preferably, the wing quick fixation structure includes two blocks of side plates being symmetrically installed, and is formed among two blocks of side plates empty
Chamber, there are one wing fast-assembling buttons for the interior setting of the cavity, and the lower end of the wing fast-assembling button is provided with the first spring, passes through
The flexible of first spring can be such that wing fast-assembling button moves up and down, and the upper end of the wing fast-assembling button ejects the upper of cantilever
Surface, on the outer segment wing connection there are one cover board, the cover board setting positioned at cantilever upper side and to be arranged in wing fast
Fill the periphery of button.
Preferably, the empennage quick fixation structure includes installation side plate, and empennage fast-assembling button is provided in the installation side plate,
The lower end of the empennage fast-assembling button is provided with second spring, by the second spring it is flexible can make the empennage fast-assembling by
Button moves up and down, the upper side of the upper end ejection empennage of the empennage fast-assembling button.
Preferably, the steering engine that verts includes vert steering engine fuselage and rocking arm, and the steering engine fuselage that verts is pacified by bolt
Loaded on cantilever, the rocking arm is connect by bolt with motor, and the rocking arm can rotate around the steering engine fuselage that verts.
Preferably, the fuselage interior is additionally provided with camera, and camera aperture is arranged on the hatchcover, and the camera lens of the camera is logical
It crosses camera aperture and exposes hatchcover.
The utility model has the beneficial effects that：1, it is verted steering engine by setting, realizes the VTOL of unmanned aerial vehicle platform,
When taking off, 4 propellers on cantilever vertically upward, the stabilization of fuselage are kept by 4 motors, and rely on 4 spirals
The pulling force realization of paddle is taken off vertically, after completion is taken off vertically, 2 propellers of cantilever front end driven by the steering engine that verts forward
It verts, a part of pulling force is for providing lift, and a part of pulling force is for drawing unmanned aerial vehicle platform flight forward, to reduce nothing
Requirement and personnel operation difficulty of the man-machine platform to landing runway, to reduce overall cost；2, by the way that wing fast-assembling is arranged
Structure and empennage quick fixation structure, make the assembling of unmanned aerial vehicle platform and dismounting greatly simplify.
Description of the drawings
Fig. 1 is the structural schematic diagram of one preferred embodiment of the utility model；
Fig. 2 is the fuselage interior structural schematic diagram of the utility model embodiment；
Fig. 3 is the scheme of installation of steering engine of verting in the utility model embodiment；
Fig. 4 is the scheme of installation of wing quick fixation structure in the utility model embodiment；
Fig. 5 is the internal structure chart of Fig. 4；
Fig. 6 is the scheme of installation of empennage quick fixation structure in the utility model embodiment；
The label of each component is as follows in attached drawing：1, fuselage, 2, stage casing wing, 3, outer segment wing, 4, cantilever, 5, propeller,
6, motor, 7, vert steering engine, 8, wing quick fixation structure, 9, empennage mounting groove, 10, empennage quick fixation structure, 11, empennage, 12, electricity
Pond, 13, fly control, 14, hatchcover, 15, camera, 701, vert steering engine fuselage, 702, rocking arm, 801, side plate, 802, wing fast-assembling presses
Button, the 803, first spring, 804, cover board, 1001, installation side plate, 1002, empennage fast-assembling button, 1003, second spring.
Specific implementation mode
The preferred embodiment of the utility model is described in detail below in conjunction with the accompanying drawings, so that the advantages of the utility model
It can be easier to be readily appreciated by one skilled in the art with feature, it is apparent clear to be made to the scope of protection of the utility model
Define.
It please refers to Fig.1 to Fig. 2, the utility model embodiment includes：
It is a kind of can VTOL unmanned aerial vehicle platform, including：Fuselage 1, the left and right sides of the fuselage 1 are symmetrical arranged organic
The wing, the wing include stage casing wing 2 and outer segment wing 3, and the stage casing wing 2 is fixedly arranged on the left and right sides of fuselage 1, in described
Section wing 2 is provided with a cantilever 4 along 1 length direction of fuselage close to one end of outer segment empennage 3, and front and back the two of the cantilever 4
End is respectively arranged with propeller 5, and motor 6 is provided on the propeller 5, is additionally provided with and inclines on the motor 6 of 4 front end of the cantilever
It comes about machine 7, the cantilever 4 is internally provided with a wing quick fixation structure 8, and the outer segment wing 3 passes through wing quick fixation structure 8
It is connect with cantilever 4, the two sides of tail of the fuselage 1 is symmetrically arranged with empennage mounting groove 9, passes through tail in the empennage mounting groove 9
Wing quick fixation structure 10 is arranged with empennage 11, and the inside of the fuselage is also equipped with battery 12, flies control 13 and camera 15, the battery
12, fly control 13 and the top of camera 15 be provided with hatchcover 14,
Referring to Fig. 3, the steering engine 7 that verts includes vert steering engine fuselage 701 and rocking arm 702, the steering engine fuselage that verts
701 are installed on by bolt on cantilever 4, and the rocking arm 702 is connect by bolt with motor 6, and the rocking arm 702 can be around the rudder that verts
Machine fuselage 701 rotates.
Fig. 4 to Fig. 5 is please referred to, the wing quick fixation structure 8 includes two blocks of side plates 801 being symmetrically installed, two pieces of sides
Form cavity among plate 801, setting is there are one wing fast-assembling button 802 in the cavity, under the wing fast-assembling button 802
End is provided with the first spring 803, and flexible by first spring 803 can be such that wing fast-assembling button 802 moves up and down, described
The upper surface of the upper end ejection cantilever 4 of wing fast-assembling button 802, there are one cover boards 804 for connection on the outer segment wing 3, described
The setting of cover board 804 is located at the upper side of cantilever 4 and is arranged in the periphery of wing fast-assembling button 802.
Referring to Fig. 6, the empennage quick fixation structure 10 includes installation side plate 1001, it is provided in the installation side plate 1001
The lower end of empennage fast-assembling button 1002, the empennage fast-assembling button 1002 is provided with second spring 1003, passes through second bullet
The flexible of spring 1003 can be such that the empennage fast-assembling button 1002 moves up and down, and the upper end of the empennage fast-assembling button 1002 ejects tail
The upper side of the wing 11.
The operational process of the present embodiment includes the following steps：
One, course line is arranged according to survey zone position；
Two, course line is uploaded to and flies control 13, flown control 13 and control the steering engine 7 that verts, drive two propellers 8 of 4 front end of cantilever
Turn to vertical position；
Three, fly 13 four motors 6 of control of control to rotate, four rotations of propeller 5 of drive generate pulling force straight up, by nothing
Man-machine platform is pulled up to certain altitude；
Four, it completes after taking off vertically, two motors 6 of 4 front end of cantilever start to turn forward under the drive for the steering engine 7 that verts
Turn, generates forward pulling force, unmanned aerial vehicle platform is made to move forwards；
Five, after reaching cruising speed, the pulling force of the lift substitution propeller 5 of wing, and unmanned aerial vehicle platform is maintained to carry out
Horizontal flight；
Six, after completing aerophotogrammetric field work, unmanned aerial vehicle platform makes a return voyage, and near landing position, starts to continuously decrease height and speed
Degree, after reaching corresponding position, two motors of 4 front end of cantilever vert upwards in the case where the steering engine 7 that verts drives, and are gradually reduced forward
Pulling force, improve upward pulling force, making up airfoil lift reduces the height loss that brings and continuously decrease height.
The above description is only the embodiments of the present invention, and it does not limit the scope of the patent of the present invention, every
Equivalent structure or equivalent flow shift made based on the specification and figures of the utility model, is applied directly or indirectly in
Other related technical areas are equally included in the patent within the scope of the utility model.
Claims (5)
1. it is a kind of can VTOL unmanned aerial vehicle platform, which is characterized in that including：The left and right sides of fuselage, the fuselage is symmetrical
It is provided with wing, the wing includes stage casing wing and outer segment wing, and the stage casing wing is fixedly arranged on the left and right sides of fuselage, institute
It states stage casing wing and one end of outer segment empennage is provided with a cantilever along fuselage length direction, the rear and front end of the cantilever
It is respectively arranged with propeller, motor is provided on the propeller, the steering engine that verts is additionally provided on the motor of the cantilever front end,
The cantilever is internally provided with a wing quick fixation structure, and the outer segment wing is connect by wing quick fixation structure with cantilever,
The two sides of tail of the fuselage is symmetrically arranged with empennage mounting groove, is arranged with by empennage quick fixation structure in the empennage mounting groove
The inside of empennage, the fuselage is also equipped with battery and flies control, and the battery and the top for flying control are provided with hatchcover.
2. it is according to claim 1 it is a kind of can VTOL unmanned aerial vehicle platform, which is characterized in that the wing fast-assembling knot
Structure includes two blocks of side plates being symmetrically installed, and cavity is formed among two blocks of side plates, there are one wing is fast for the interior setting of the cavity
Button is filled, the lower end of the wing fast-assembling button is provided with the first spring, and flexible by first spring can make wing fast
Dress button moves up and down, the upper surface of the upper end ejection cantilever of the wing fast-assembling button, and one is connected on the outer segment wing
A cover board, the cover board setting are located at the upper side of cantilever and are arranged in the periphery of wing fast-assembling button.
3. it is according to claim 1 it is a kind of can VTOL unmanned aerial vehicle platform, which is characterized in that the empennage fast-assembling knot
Structure includes installation side plate, and empennage fast-assembling button is provided in the installation side plate, and the lower end of the empennage fast-assembling button is provided with
Second spring, flexible by the second spring can be such that the empennage fast-assembling button moves up and down, the empennage fast-assembling button
Upper end ejection empennage upper side.
4. it is according to claim 1 it is a kind of can VTOL unmanned aerial vehicle platform, which is characterized in that the steering engine packet that verts
Include vert steering engine fuselage and rocking arm, the steering engine fuselage that verts is installed on by bolt on cantilever, the rocking arm by bolt with
Motor connects, and the rocking arm can rotate around the steering engine fuselage that verts.
5. it is according to claim 1 it is a kind of can VTOL unmanned aerial vehicle platform, which is characterized in that the fuselage interior is also
It is provided with camera, camera aperture is set on the hatchcover, the camera lens of the camera exposes hatchcover by camera aperture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820133711.XU CN207826549U (en) | 2018-01-26 | 2018-01-26 | It is a kind of can VTOL unmanned aerial vehicle platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820133711.XU CN207826549U (en) | 2018-01-26 | 2018-01-26 | It is a kind of can VTOL unmanned aerial vehicle platform |
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| Publication Number | Publication Date |
|---|---|
| CN207826549U true CN207826549U (en) | 2018-09-07 |
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ID=63394778
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820133711.XU Active CN207826549U (en) | 2018-01-26 | 2018-01-26 | It is a kind of can VTOL unmanned aerial vehicle platform |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109515705A (en) * | 2018-11-20 | 2019-03-26 | 西安爱生无人机技术有限公司 | A kind of unmanned plane of VTOL |
| CN109720564A (en) * | 2019-02-13 | 2019-05-07 | 深圳创壹通航科技有限公司 | Fixed-wing unmanned plane and its control method with VTOL function |
| WO2020151608A1 (en) * | 2019-01-25 | 2020-07-30 | 深圳市旗客智能技术有限公司 | Rotary-wing unmanned aerial vehicle |
| CN113173246A (en) * | 2021-05-07 | 2021-07-27 | 新疆大学 | Long-endurance composite wing AI automatic detection electric cruise unmanned aerial vehicle and method |
-
2018
- 2018-01-26 CN CN201820133711.XU patent/CN207826549U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109515705A (en) * | 2018-11-20 | 2019-03-26 | 西安爱生无人机技术有限公司 | A kind of unmanned plane of VTOL |
| WO2020151608A1 (en) * | 2019-01-25 | 2020-07-30 | 深圳市旗客智能技术有限公司 | Rotary-wing unmanned aerial vehicle |
| CN109720564A (en) * | 2019-02-13 | 2019-05-07 | 深圳创壹通航科技有限公司 | Fixed-wing unmanned plane and its control method with VTOL function |
| CN113173246A (en) * | 2021-05-07 | 2021-07-27 | 新疆大学 | Long-endurance composite wing AI automatic detection electric cruise unmanned aerial vehicle and method |
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