CN107878752A - From steady wind resistance unmanned plane - Google Patents
From steady wind resistance unmanned plane Download PDFInfo
- Publication number
- CN107878752A CN107878752A CN201711461569.8A CN201711461569A CN107878752A CN 107878752 A CN107878752 A CN 107878752A CN 201711461569 A CN201711461569 A CN 201711461569A CN 107878752 A CN107878752 A CN 107878752A
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- CN
- China
- Prior art keywords
- unmanned plane
- horn
- wind resistance
- drive device
- rotor driver
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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- 239000006096 absorbing agent Substances 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 claims description 4
- 238000000034 method Methods 0.000 abstract description 3
- 230000005484 gravity Effects 0.000 description 7
- 238000009434 installation Methods 0.000 description 4
- 238000013016 damping Methods 0.000 description 3
- 238000006073 displacement reaction Methods 0.000 description 3
- 108010066057 cabin-1 Proteins 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
The present invention relates to unmanned air vehicle technique field, more particularly to from steady wind resistance unmanned plane, including center cabin, battery flat, horn, vector drive device, rotor driver, landing gear and control system, the vector drive device is installed on the horn, the horn is connected with the center cabin forms organism frame, the rotor driver is arranged in vector drive device driving, the vector drive device is connected with the control system to control rotor driver to be moved relative to horn, the vector drive device includes turning part and rotating part, turning part spins upside down mode with horn use and connected, the rotating part is connected with rotor driver using rotation mode, when solving unmanned plane bad weather run into flight course, easily cause unmanned plane during flying extremely unstable or even have the problem of risk fallen.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to from steady wind resistance unmanned plane.
Background technology
With the development of society, unmanned plane is using more and more extensive, such as express transportation, take photo by plane, crops monitoring, Xin Wen Bao
The fields such as road, electric inspection process and movies-making, rotor wing unmanned aerial vehicle change variable rotor speed by regulation motor rotating speed, realize and rise
Power changes, so as to control flight, such as four rotor wing unmanned aerial vehicles, when the lift sum of four propellers of aircraft is equal to aircraft gross weight amount
When, lift and the gravity of aircraft are balanced each other, and aircraft can is hovered in the air, but when unmanned plane is by adverse weather conditions
When, unmanned plane because being acted on by different directions power, easily causes unmanned plane entirety stress extremely unstable in flight course, from
And make unmanned plane that there is the risk fallen.
In summary, need a kind of technical scheme solution unmanned plane badly at present and bad weather is frequently run onto in flight course
When, easily cause unmanned plane during flying extremely unstable or even have the problem of risk fallen.
The content of the invention
When being frequently run onto bad weather it is an object of the invention to solve unmanned plane in flight course, easily cause nobody
Machine flight is extremely unstable or even has the problem of risk fallen.
To achieve the above object, the technical solution adopted by the present invention is：
From steady wind resistance unmanned plane, including center cabin, battery flat, several horns, vector drive device, rotor driver, undercarriage
Device and control system；
The vector drive device is mounted on each horn, the horn is connected with the center cabin forms body frame
Frame, the rotor driver are arranged in vector drive device driving, the vector drive device and control system electricity
Property connection to control rotor driver to be moved relative to horn；
The vector drive device includes turning part and rotating part, and turning part one end is connected on the horn and can made
Turning part is spun upside down with respect to horn, the turning part other end rotatable connection rotating part, and the rotating part energy
Enough axial-rotations along turning part, the rotor driver rotatable connection is on the rotating part.
Horn is connected with center cabin forms organism frame, and rotor driver is installed in the driving of vector drive device, and vector drives
Dynamic device is connected with control system to control rotor driver to be moved relative to horn, and vector drive device includes turning part and rotation
Portion, when unmanned plane is running into bad weather, the turning part of vector drive device can be controlled to drive rotor to fill by control system
Put and move up and down, while drive rotor driver to turn to different angles by rotating part, active force caused by rotating device point
In unmanned plane vertically and horizontally, the active force of vertical direction offsets the gravity suffered by unmanned plane, horizontal direction to solution
Active force can offset active force of the unmanned plane by different horizontal directions, active force offsets unmanned plane by different directions
External force, make unmanned plane held stationary, when running into bad weather so as to solve unmanned plane in flight course, easily cause nobody
Machine flight is extremely unstable or even has the problem of risk fallen.
Preferably, turning part includes the mounting seat located at the end one of horn, and the mounting seat is provided with steering wheel one, institute
State steering wheel one and be provided with gear shaft one, the gear engagement of end one of the drive link of the gear shaft one and the vector drive device connects
Connect, while the end one of the drive link is connected with mounting seat using rotating shaft, the end one of horn is provided with mounting seat, and mounting seat is provided with
Steering wheel one, rotated by the gear shaft one of steering wheel one, the gear of end one of gear shaft one and the drive link of vector drive device is nibbled
Connection is closed, while the end one of drive link is connected with mounting seat rotating shaft, so as to drive drive link relative to installation by gear drive
Seat rotates upwardly and downwardly, and reaches the purpose of regulation rotor driver vertical displacement.
Preferably, the steering wheel one is symmetrically set in mounting seat both sides.
Preferably, the rotating part includes the steering wheel two located at the end two of drive link, and the steering wheel two is provided with gear shaft
Two, the gear shaft two engages connection with the rotor driver gear, while the end two of the drive link uses with rotor driver
Bearing connects, and steering wheel two is provided with gear shaft two, and gear shaft two engages connection, the end two of drive link with rotor driver using gear
It is connected with rotor driver bearing, so as to drive rotor driver to be rotated relative to drive link by gear drive, reaches regulation rotor
Device adjusts stable purpose by angle change.
Preferably, the steering wheel two is arranged with the end two of drive link.
Preferably, the center cabin is provided with neck, and the end two of the horn is provided with the deck being adapted to neck, the card
Groove is connected with deck using clamping body, is connected by the deck on horn with the neck on the cabin of center using clamping body, side
Just the installation and removal of horn.
Preferably, the landing gear includes the vertical tube component of centrally disposed cabin lower end, the vertical tube component lower end
Provided with transverse tube, vertical tube component lower end is provided with transverse tube, and the contact area on transverse tube and ground is big, so as to make unmanned plane on landing ground
When held stationary.
Preferably, the vertical tube component includes the vertical tube being hinged, and the vertical tube is provided with vibration absorber, by perpendicular
Damping device is set to reduce unmanned plane in vibrations caused by landing ground in tube assembly.
Preferably, the horn is that arc is down-set, and horn is that arc is down-set, the center of gravity of unmanned plane is sunk,
So that the stability of unmanned plane is more preferable.
Preferably, center cabin upper end is provided with center hatchcover, and there is GPS device on the center hatchcover top, passed through
GPS device is provided with center hatchcover top and receives transmission signal, realizes the purpose for monitoring nobody flight position.
Compared with prior art, the advantage of the invention is that：
It is provided by the invention from steady wind resistance unmanned plane, horn is connected with center cabin forms organism frame, and rotor driver is arranged on institute
State in the driving of vector drive device, vector drive device is connected with the control system to control rotor driver to be transported relative to horn
Dynamic, vector drive device includes turning part and rotating part, when unmanned plane is running into bad weather, can be controlled by control system
The turning part of vector drive device drives rotor driver to move up and down, while drives rotor driver to turn to difference by rotating part
Angle, Force decomposition caused by rotating device in unmanned plane vertically and horizontally, the active force of vertical direction
The gravity suffered by unmanned plane is offset, the active force of horizontal direction can offset active force of the unmanned plane by different horizontal directions,
Active force offsets unmanned plane by the external force of different directions, makes unmanned plane held stationary, was being flown so as to solve unmanned plane
When bad weather is run into journey, easily cause unmanned plane during flying extremely unstable or even have the problem of risk fallen.
The beneficial effect of the application other embodiment is：
1st, the end one of horn is provided with mounting seat, and mounting seat is provided with steering wheel one, is rotated by the gear shaft one of steering wheel one, gear
Axle one engages connection with the gear of end one of the drive link of vector drive device, while the end one of drive link connects with mounting seat rotating shaft
Connect, so as to drive drive link to be rotated upwardly and downwardly relative to mounting seat by gear drive, reach regulation rotor driver vertical displacement
Purpose.
2. steering wheel two is provided with gear shaft two, gear shaft two engages connection, the end of drive link with rotor driver using gear
Two are connected with rotor driver bearing, so as to drive rotor driver to be rotated relative to drive link by gear drive, reach regulation rotation
Swing device adjusts stable purpose by angle change in the horizontal plane.
3. connected by the deck on horn with the neck on the cabin of center using clamping body, facilitate horn installation and
Dismounting.
4. vertical tube component lower end is provided with transverse tube, the contact area on transverse tube and ground is big, so as to make unmanned plane in jump area
Held stationary during face.
5. by setting damping device to reduce unmanned plane in vibrations caused by landing ground on vertical tube component.
6. horn is that arc is down-set, the center of gravity of unmanned plane is set to sink so that the stability of unmanned plane is more preferable.
7. receiving transmission signal by being provided with GPS device on center hatchcover top, realize and monitor nobody flight position
Purpose.
Brief description of the drawings
Fig. 1 is the structural representation from steady wind resistance unmanned plane of the embodiment of the present invention 1；
Fig. 2 is the mounting structure from the horn of steady wind resistance unmanned plane, vector drive device and rotor driver of the embodiment of the present invention 1
Schematic diagram.
Reference
1- centers cabin, 2- battery flats, 3- horns, 4- vector drive devices, 41- turning part, 411- mounting seats, 412- steering wheels one,
413- gear shafts one, 414- drive links, 42- rotating parts, 421- steering wheels two, 422- gear shafts two, 5- rotor drivers, 6- undercarriages
Device, 61- vertical tube components, 62- transverse tubes, 63- vibration absorbers, 7- centers hatchcover, 8-GPS devices.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that specific embodiment described herein is only to explain the present invention, not
For limiting the present invention.
Embodiment 1
The present embodiment includes center cabin 1, battery flat 2, horn 3, vector driving from steady wind resistance unmanned plane as shown in accompanying drawing 1, accompanying drawing 2
Device 4, turning part 41, mounting seat 411, steering wheel 1, gear shaft 1, drive link 414, rotating part 42, steering wheel 2 421,
Gear shaft 2 422, rotor driver 5, landing gear 6, vertical tube component 61, transverse tube 62, vibration absorber 63, center hatchcover 7, GPS
Device 8, from steady wind resistance unmanned plane, horn 3 is connected with center cabin 1 forms organism frame, and rotor driver 5 drives installed in the vector
In the dynamic driving of device 4, vector drive device 4 is connected with the control system to control rotor driver 5 to be moved relative to horn 3,
Vector drive device 4 includes turning part 41 and rotating part 42, when unmanned plane is running into bad weather, can pass through control system control
The turning part 41 of vector drive device 4 processed drives rotor driver 5 to move up and down, while drives rotor driver 5 by rotating part 42
Turn to different angles, Force decomposition caused by rotating device 5 in unmanned plane vertically and horizontally, vertical side
To active force offset gravity suffered by unmanned plane, the active force of horizontal direction can offset unmanned plane by different horizontal directions
Active force, active force offset unmanned plane by the external force of different directions, make unmanned plane held stationary, so as to solve unmanned plane
When bad weather is run into flight course, easily cause unmanned plane during flying extremely unstable or even have the problem of risk fallen.
The end one of horn 3 is provided with mounting seat 411, and mounting seat 411 is provided with steering wheel 1, passes through the sliding tooth of steering wheel 1
Wheel shaft 1 rotates, and gear shaft 1 engages connection with the gear of end one of the drive link 414 of vector drive device 4, passed simultaneously
The end one of lever 414 is connected with the rotating shaft of mounting seat 411, so as to drive drive link 414 relative to mounting seat 411 by gear drive
Rotate upwardly and downwardly, reach the purpose of the regulation vertical displacement of rotor driver 5.
Steering wheel 2 421 is provided with gear shaft 2 422, and gear shaft 2 422 engages connection using gear with rotor driver 5, passed
The end two of lever 414 is connected with the bearing of rotor driver 5, so as to drive rotor driver 5 relative to drive link 414 by gear drive
Rotation, reach regulation rotor driver 5 and stable purpose is adjusted by angle change.
Connected by the deck on horn 3 with the neck on the cabin of center using clamping body, facilitate the peace installation and dismantling of horn 3
Unload.
The lower end of vertical tube component 61 is provided with transverse tube 62, and transverse tube 62 and the contact area on ground are big, so as to drop unmanned plane
Held stationary during landing face.
By setting damping device 63 to reduce unmanned plane in vibrations caused by landing ground on vertical tube component 61.
Horn 3 is that arc is down-set, the center of gravity of unmanned plane is sunk so that the stability of unmanned plane is more preferable.
Transmission signal is received by being provided with GPS device 8 on the top of center hatchcover 7, realizes and monitors nobody flight position
Purpose.
Above example only not limits technical scheme described in the invention to illustrate the present invention, although this explanation
Book is with reference to above-mentioned each embodiment to present invention has been detailed description, but the present invention is not limited to above-mentioned specific implementation
Mode, therefore any the present invention is modified or equivalent substitution；And the technical side of all spirit and scope for not departing from invention
Case and its improvement, it all should cover among scope of the presently claimed invention.
Claims (10)
1. from steady wind resistance unmanned plane, it is characterised in that：Including center cabin（1）, battery flat（2）, several horns（3）, vector drive
Dynamic device（4）, rotor driver（5）, landing gear（6）And control system；
Each horn（3）On be mounted on the vector drive device（4）, the horn（3）With the center cabin（1）Phase
Even form organism frame, the rotor driver（5）Installed in the vector drive device（4）In driving, the vector driving dress
Put（4）It is electrically connected with the control system to control rotor driver（5）Relative to horn（3）Motion；
The vector drive device（4）Including turning part（41）And rotating part（42）, turning part（41）One end is connected to institute
State horn（3）Go up and turning part can be made（41）With respect to horn（3）Spin upside down, turning part（41）The other end rotates
Connect the rotating part（42）, and the rotating part（42）Can be along turning part（41）Axial-rotation, rotor dress
Put（5）Rotatable connection is in the rotating part（42）On.
It is 2. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：Turning part（41）Including located at horn
（3）The mounting seat at end one（411）, the mounting seat（411）It is provided with steering wheel one（412）, the steering wheel one（412）It is provided with tooth
Wheel shaft one（413）, the gear shaft one（413）With the vector drive device（4）Drive link（414）The engagement of end one gear
Connection, while the drive link（414）End one and mounting seat（411）Connected using rotating shaft.
It is 3. according to claim 2 from steady wind resistance unmanned plane, it is characterised in that：The steering wheel one（412）It is symmetrically set in peace
Fill seat（411）Both sides.
It is 4. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：The rotating part（42）Including located at transmission
Bar（413）End two steering wheel two（421）, the steering wheel two（421）It is provided with gear shaft two（422）, the gear shaft two
（422）With the rotor driver（5）Gear engagement connection, while the drive link（413）End two and rotor driver（5）Using
Bearing connects.
It is 5. according to claim 4 from steady wind resistance unmanned plane, it is characterised in that：The steering wheel two（421）It is arranged with biography
Lever（413）End two both sides.
It is 6. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：The center cabin（1）It is provided with neck, institute
The end two for stating horn is provided with the deck being adapted to neck, and the deck is connected with neck using clamping body.
It is 7. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：The landing gear（6）Including setting
In center cabin（1）The vertical tube component of lower end（61）, the vertical tube component（61）Lower end is provided with transverse tube（62）.
It is 8. according to claim 7 from steady wind resistance unmanned plane, it is characterised in that：The vertical tube component（61）Including mutually hinge
The vertical tube connect, the vertical tube are provided with vibration absorber（63）.
It is 9. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：The horn（3）It is down-set for arc.
It is 10. according to claim 1 from steady wind resistance unmanned plane, it is characterised in that：Center cabin（1）Upper end is provided with
Center hatchcover（7）, the center hatchcover（7）GPS device is arranged at top（8）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711461569.8A CN107878752A (en) | 2017-12-28 | 2017-12-28 | From steady wind resistance unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711461569.8A CN107878752A (en) | 2017-12-28 | 2017-12-28 | From steady wind resistance unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107878752A true CN107878752A (en) | 2018-04-06 |
Family
ID=61770518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711461569.8A Pending CN107878752A (en) | 2017-12-28 | 2017-12-28 | From steady wind resistance unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107878752A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110416916A (en) * | 2019-08-01 | 2019-11-05 | 东北大学 | For posture regulation method and regulating and controlling mechanism of the crusing robot under wind load |
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|---|---|---|---|---|
| WO2012065584A2 (en) * | 2010-11-18 | 2012-05-24 | Horst Zell | Aircraft comprising an integrated working platform |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| CN105620743A (en) * | 2016-02-22 | 2016-06-01 | 南京航空航天大学 | Tilting mechanism for tilting three-rotor aircraft |
| US20170158320A1 (en) * | 2015-09-20 | 2017-06-08 | Daniel Bosch | Unmanned aerial system |
| CN107021218A (en) * | 2017-05-23 | 2017-08-08 | 福州大学 | The on-plane surface aircraft and control method of a kind of wind disturbance resistance |
| KR20170094045A (en) * | 2016-02-05 | 2017-08-17 | 경북대학교 산학협력단 | A multicopter type smart drone using tilt rotor |
| CN107161330A (en) * | 2017-05-27 | 2017-09-15 | 四川建筑职业技术学院 | A kind of variable abnormally-structured displacement multi-rotor unmanned aerial vehicle |
| CN207644642U (en) * | 2017-12-28 | 2018-07-24 | 四川建筑职业技术学院 | It is a kind of from steady wind resistance unmanned plane |
-
2017
- 2017-12-28 CN CN201711461569.8A patent/CN107878752A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2012065584A2 (en) * | 2010-11-18 | 2012-05-24 | Horst Zell | Aircraft comprising an integrated working platform |
| CN103359283A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | High-reliability unmanned aerial vehicle with tilt rotors |
| US20170158320A1 (en) * | 2015-09-20 | 2017-06-08 | Daniel Bosch | Unmanned aerial system |
| KR20170094045A (en) * | 2016-02-05 | 2017-08-17 | 경북대학교 산학협력단 | A multicopter type smart drone using tilt rotor |
| CN105620743A (en) * | 2016-02-22 | 2016-06-01 | 南京航空航天大学 | Tilting mechanism for tilting three-rotor aircraft |
| CN107021218A (en) * | 2017-05-23 | 2017-08-08 | 福州大学 | The on-plane surface aircraft and control method of a kind of wind disturbance resistance |
| CN107161330A (en) * | 2017-05-27 | 2017-09-15 | 四川建筑职业技术学院 | A kind of variable abnormally-structured displacement multi-rotor unmanned aerial vehicle |
| CN207644642U (en) * | 2017-12-28 | 2018-07-24 | 四川建筑职业技术学院 | It is a kind of from steady wind resistance unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110416916A (en) * | 2019-08-01 | 2019-11-05 | 东北大学 | For posture regulation method and regulating and controlling mechanism of the crusing robot under wind load |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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Application publication date: 20180406 |