CN206954510U - It is a kind of can VTOL fixed-wing unmanned plane - Google Patents
It is a kind of can VTOL fixed-wing unmanned plane Download PDFInfo
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- CN206954510U CN206954510U CN201720639301.8U CN201720639301U CN206954510U CN 206954510 U CN206954510 U CN 206954510U CN 201720639301 U CN201720639301 U CN 201720639301U CN 206954510 U CN206954510 U CN 206954510U
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- wing
- motor
- unmanned plane
- bending mechanism
- fixed
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Abstract
The utility model discloses it is a kind of can VTOL fixed-wing unmanned plane, including unmanned aerial vehicle body, fuselage both sides are provided with fixed-wing, the first screw wing that the first motor is provided with fixed-wing and is installed on the first motor, the first battery and the first driver control component for the action of the first driver are provided with the fuselage；The utility model is in takeoff phase by the first bending mechanism and the second bending mechanism perpendicular to horizontal plane, then vertical lift is realized, after take off, two bending mechanisms are playbacked, whole unmanned plane is in " one " font, realized and advanced using the screw wing on two bending mechanisms, and coordinate the screw wing collective effect on fixed-wing, realize whole power and the control of steering of unmanned plane.
Description
Technical field
The utility model is related to unmanned plane field, and in particular to it is a kind of can VTOL fixed-wing unmanned plane.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.Nothing on machine
Driving cabin, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or machine tool remote control station personnel pass through
The equipment such as radar, it is tracked, positioned, is remotely controlled, remote measurement and Digital Transmission.Can be under wireless remotecontrol as conventional airplane one
Sample takes off or launched with booster rocket, can also take aerial launch to by machine tool and fly.During recovery, it can with conventional airplane
The same mode automatic Landing of land process, it can also be reclaimed by remote control parachute or block.Can repetitiousness use it is multiple.Use extensively
In mapping, aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
General existing fixed-wing unmanned plane is taken off, and mode is mostly launched, hand is thrown, runway is slided and taken off；Landing modes are umbrella
Drop, runway slides, stall hits ground.Catapult-assisted take-off needs launching cradle, not readily portable；Hand, which is thrown, flies have certain danger to operating personnel
Nearly, can not hand throwing when while unmanned plane own wt is excessive；Runway slides landing of taking off and does not generally possess the condition in the wild；Drop
Flying weight can be increased by falling umbrella, while big by windage, and can not accurately land setting position, and these all have a variety of inconvenience and risen
Fly the factor of landing.
Utility model content
The utility model is directed to deficiency of the prior art, there is provided it is a kind of can VTOL fixed-wing unmanned plane.
The utility model is achieved through the following technical solutions：It is a kind of can VTOL fixed-wing unmanned plane, bag
Unmanned aerial vehicle body is included, fuselage both sides are provided with fixed-wing, and the first motor is provided with fixed-wing and is installed on the first drive
The first screw wing on motor is moved, the first battery and the first driver for the action of the first driver are provided with the fuselage
Control assembly；
The both ends of the fuselage offer a fitting recess, and first bender is provided with one of fitting recess
Structure, second bending mechanism is installed in another fitting recess, first bending mechanism and the second bending mechanism pass through
The department of assembly of one end is fitted into fitting recess, and the both sides of department of assembly set a rotating shaft respectively, and the both ends outboard end of rotating shaft connects respectively
An electric rotating machine is connect, electric rotating machine drives two bending mechanisms to rotate 90 degree.
As preferable technical scheme, the second motor, the second motor are provided with first bending mechanism
By the second battery powered being independently arranged, the second motor is controlled by the second driver control component, the second driving electricity
Second screw wing is installed on the output shaft of machine.
As preferable technical scheme, the 3rd motor, the 3rd motor are provided with second bending mechanism
By the 3rd battery powered being independently arranged, the 3rd motor is controlled by the 3rd driver control component, the 3rd driving electricity
3rd screw wing is installed, the second bending mechanism is arranged at the tail end of unmanned plane, and the first bending mechanism is set on the output shaft of machine
In the head end of unmanned plane.
As preferable technical scheme, a wireless communication module, its point are mounted on three driver control components
Do not controlled by the remote control wireless remote control on ground.
The beneficial effects of the utility model are：The utility model passes through the first bending mechanism and the second folding in takeoff phase
Then bender structure is realized vertical lift, after take off, two bending mechanisms playbacked, whole unmanned plane is in perpendicular to horizontal plane
" one " font, realized and advanced using the screw wing on two bending mechanisms, and coordinate the screw wing collective effect on fixed-wing, it is real
The whole power of existing unmanned plane and the control of steering.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is overall structure diagram of the present utility model；
Fig. 2 is takeoff condition schematic diagram of the present utility model.
Embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine in any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically chatting
State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature
It is an example in a series of equivalent or similar characteristics.
As depicted in figs. 1 and 2, including unmanned aerial vehicle body 6, the both sides of fuselage 6 are provided with fixed-wing 5, are provided with fixed-wing 5
First motor and the first screw wing 4 being installed on the first motor, it is provided with fuselage 6 and is moved for the first driver
The first battery and the first driver control component made；
The both ends of fuselage 6 offer a fitting recess, and first bending mechanism is provided with one of fitting recess
3, second bending mechanism 8 is installed in another fitting recess, the first bending mechanism 3 and the second bending mechanism 8 pass through one
The department of assembly 7 at end is fitted into fitting recess, and the both sides of department of assembly 7 set a rotating shaft respectively, and the both ends outboard end of rotating shaft connects respectively
An electric rotating machine 2 is connect, electric rotating machine 2 drives two bending mechanisms to rotate 90 degree.
Wherein, it is provided with the second motor 11 in the first bending mechanism 3, the second motor 11 is by being independently arranged
Second battery powered, the second motor are controlled by the second driver control component, on the output shaft of the second motor 11
Second screw wing 1 is installed.
The 3rd motor 12 is provided with second bending mechanism, the 3rd motor 12 is electric by the be independently arranged the 3rd
Pond is powered, and the 3rd motor 12 is controlled by the 3rd driver control component, is provided with the output shaft of the 3rd motor
3rd screw wing 9, the second bending mechanism are arranged at the tail end of unmanned plane, and the first bending mechanism is arranged at the head end of unmanned plane.
A wireless communication module is mounted on three driver control components, it is filled by the remote control on ground respectively
Put wireless remote control control.
We realize that single dynamic Control and power open by three driver control components of remote control remote control
Dynamic, when taking off, we are rotated up 90 degree, make its perpendicular to the ground, both ends by electric rotating machine, two bending mechanisms of driving
Balance is kept, the screw wing on two screw wings and fixed-wing is opened, is taken off vertically using three screw wings, its principle is with straight
The principle of the machine of liter is identical, is realized and risen using uprush, after taking off, returned bending mechanism using remote control control electric rotating machine
Position, in Fig. 1, now whole fuselage is in " one " font, now using the second screw wing, the 3rd auger, realizes and advances, turns
To being balanced by two the first screw wings, a series of action of adjustment etc., because unmanned aerial vehicle body both sides are equal in weight, risen
It is identical with helicopter when flying, the gliding of later-stage utilization fixed-wing, promoted, had more preferable by the second screw wing and the 3rd screw wing
Offline mode.
The beneficial effects of the utility model are：The utility model passes through the first bending mechanism and the second folding in takeoff phase
Then bender structure is realized vertical lift, after take off, two bending mechanisms playbacked, whole unmanned plane is in perpendicular to horizontal plane
" one " font, realized and advanced using the screw wing on two bending mechanisms, and coordinate the screw wing collective effect on fixed-wing, it is real
The whole power of existing unmanned plane and the control of steering.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to
In this, any change or replacement expected without creative work, should all cover within the scope of protection of the utility model.
Therefore, the scope of protection of the utility model should be determined by the scope of protection defined in the claims.
Claims (4)
1. it is a kind of can VTOL fixed-wing unmanned plane, it is characterised in that：Including unmanned aerial vehicle body, fuselage both sides are provided with solid
Determine the wing, the first screw wing that the first motor is provided with fixed-wing and is installed on the first motor, the fuselage
Inside it is provided with the first battery and the first driver control component for the action of the first driver；
The both ends of the fuselage offer a fitting recess, and first bending mechanism is provided with one of fitting recess,
One the second bending mechanism is installed in another fitting recess；
First bending mechanism and the second bending mechanism are fitted into fitting recess by the department of assembly of one end；
The both sides of department of assembly set a rotating shaft respectively, and the both ends outboard end of rotating shaft connects an electric rotating machine, electric rotating machine respectively
Two bending mechanisms of driving rotate 90 degree.
2. as claimed in claim 1 can VTOL fixed-wing unmanned plane, it is characterised in that：In first bending mechanism
It is provided with the second motor, the second motor passes through by the second battery powered for being independently arranged, the second motor
Two driver control components are controlled, and the second screw wing is provided with the output shaft of the second motor.
3. as claimed in claim 1 can VTOL fixed-wing unmanned plane, it is characterised in that：In second bending mechanism
It is provided with the 3rd motor, the 3rd motor passes through by the 3rd battery powered that is independently arranged, the 3rd motor
Three driver control components are controlled, and the 3rd screw wing is provided with the output shaft of the 3rd motor, and the second bending mechanism is set
In the tail end of unmanned plane, the first bending mechanism is arranged at the head end of unmanned plane.
4. as claimed in claim 1 can VTOL fixed-wing unmanned plane, it is characterised in that：Three driver control components
On be mounted on a wireless communication module, it is controlled by remote control wireless remote control on ground respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720639301.8U CN206954510U (en) | 2017-06-05 | 2017-06-05 | It is a kind of can VTOL fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720639301.8U CN206954510U (en) | 2017-06-05 | 2017-06-05 | It is a kind of can VTOL fixed-wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206954510U true CN206954510U (en) | 2018-02-02 |
Family
ID=61378736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720639301.8U Expired - Fee Related CN206954510U (en) | 2017-06-05 | 2017-06-05 | It is a kind of can VTOL fixed-wing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206954510U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107150806A (en) * | 2017-06-05 | 2017-09-12 | 深圳市科比特航空科技有限公司 | It is a kind of can VTOL fixed-wing unmanned plane |
| CN110466752A (en) * | 2019-08-07 | 2019-11-19 | 深圳市道通智能航空技术有限公司 | A kind of control method and tilting rotor wing unmanned aerial vehicle of tilting rotor wing unmanned aerial vehicle |
-
2017
- 2017-06-05 CN CN201720639301.8U patent/CN206954510U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107150806A (en) * | 2017-06-05 | 2017-09-12 | 深圳市科比特航空科技有限公司 | It is a kind of can VTOL fixed-wing unmanned plane |
| CN110466752A (en) * | 2019-08-07 | 2019-11-19 | 深圳市道通智能航空技术有限公司 | A kind of control method and tilting rotor wing unmanned aerial vehicle of tilting rotor wing unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180202 |