CN107031830A - It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance - Google Patents
It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance Download PDFInfo
- Publication number
- CN107031830A CN107031830A CN201710335893.9A CN201710335893A CN107031830A CN 107031830 A CN107031830 A CN 107031830A CN 201710335893 A CN201710335893 A CN 201710335893A CN 107031830 A CN107031830 A CN 107031830A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- disk
- contact chip
- rotary shaft
- contact
- 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
Links
- 238000010586 diagram Methods 0.000 description 3
- 238000007664 blowing Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000208340 Araliaceae Species 0.000 description 1
- 235000005035 Panax pseudoginseng ssp. pseudoginseng Nutrition 0.000 description 1
- 235000003140 Panax quinquefolius Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 235000008434 ginseng Nutrition 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
Abstract
The invention discloses it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, including unmanned plane, compensate fan, wind vane, rotary shaft, disk, contact pilotage, contact chip, described unmanned plane bottom sets disk, described disk inward flange sets contact chip, rotary shaft is set in the middle part of described disk, contact pilotage is set at the top of described rotary shaft, described rotary shaft bottom is installed by wind vane, described unmanned plane surrounding installs compensation fan, described contact chip is connected to compensation fan, described contact chip is set to eight, and it is evenly arranged in disk inside edge around disc centre, the distribution arrangement of the coupled contact chip of direction of described compensation fan is consistent, described compensation fan is arranged at the waist of unmanned plane, described contact pilotage and contact chip are all brush, generally, the present invention, which has, automatically adjusts flight balance, unmanned plane is avoided to occur off-line advantage.
Description
Technical field
The invention belongs to vehicle technology field, being related to a kind of unmanned plane, particularly one kind can be according to wind direction self-adjusting balance
Unmanned plane.
Background technology
Unmanned plane is the not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself.At present
Utilization to unmanned plane has been extended to multiple civil areas, wherein often being revolved with agricultural application for the unmanned plane of representative using more
The form of the wing, it is that one kind has multiple propellers, because the lift that multiple propellers are arranged in around aircraft and provided is big
Cause identical, therefore total life is equivalent on the horn crosspoint for acting on aircraft, i.e., in the geometric center of fuselage plane, thus,
Other load-supporting parts of unmanned plane are just distributed in above or below the geometric center, so that the application point of the total force of aircraft
Also as best one can close to the geometric center of fuselage plane, so as to keep balancing with total life.However, when unmanned plane meets with Cross Wind Force
When, the set-up mode of the above is easily caused unmanned plane and occurs course drift, and cause aircraft to jolt, unbalanced danger
Danger.Therefore, using ginsengs such as rotating speed, the corners of each rotor motor for correspondingly persistently changing unmanned plane more than present unmanned plane
Number, adjusts the lift and action direction of each propeller, this undoubtedly considerably increases the difficulty of UAV Flight Control.
The content of the invention
It is an object of the invention to provide it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, the unmanned plane can be according to wind
To automatically adjusting flight balance, it is to avoid the danger that unmanned plane drifts off the course, fuselage topples, with high use value.
The object of the present invention is achieved like this：It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, including unmanned plane, mend
Fan, wind vane, rotary shaft, disk, contact pilotage, contact chip are repaid, described unmanned plane bottom sets disk, described disk inner edge
Edge sets to set in the middle part of contact chip, described disk and set at the top of rotary shaft, described rotary shaft under contact pilotage, described rotary shaft
Wind vane is installed in portion, and described unmanned plane surrounding installs compensation fan, and described contact chip is connected to compensation fan.
Described contact chip is set to eight, and is evenly arranged in disk inside edge around disc centre.
The distribution arrangement of the coupled contact chip of direction of described compensation fan is consistent.
Described compensation fan is arranged at the waist of unmanned plane.
Described contact pilotage and contact chip are all brush.
The beneficial effect comprise that：The wind vane of the present invention can be carried out according to the wind-force suffered by unmanned plane side
Contact pilotage rotation at the top of rotation, the rotated by rotation axle of wind vane, contact pilotage is during rotation or touches contact chip, when
The switch with the compensation fan of contact chip same position can be triggered after contact pilotage and contact chip contact, compensation fan is rotated so as to nothing
The wind-force that man-machine side is subjected to carries out Contrary compensation, can avoid unmanned plane by course line of blowing off.
Brief description of the drawings
Fig. 1 is positive structure schematic of the invention.
Fig. 2 is overlooking the structure diagram of the invention.
Fig. 3 is the dimensional structure diagram at disk and wind vane.
Fig. 4 is the overlooking the structure diagram at disk
In figure：1st, unmanned plane 2, compensation fan 3, wind vane 4, rotary shaft 5, disk 6, contact pilotage 7, contact chip.
Embodiment
Below in conjunction with the accompanying drawings to embodiments of the invention further instruction.
Embodiment 1
As shown in accompanying drawing 1-4, it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, including unmanned plane 1, compensation fan 2, wind vane
3rd, rotary shaft 4, disk 5, contact pilotage 6, contact chip 7, the described bottom of unmanned plane 1 set disk 5, and the described inward flange of disk 5 is set
Contact chip 7 is put, the described middle part of disk 5 sets rotary shaft 4, and the described top of rotary shaft 4 sets contact pilotage 6, described rotary shaft 4
Wind vane 3 is installed in bottom, and the described surrounding of unmanned plane 1 installs compensation fan 2, and described contact chip 7 is connected to compensation fan 2.
Described contact chip 7 is set to eight, and is evenly arranged in the inside edge of disk 5 around the center of disk 5.
The distribution arrangement of the coupled contact chip 7 of direction of described compensation fan 2 is consistent.
Described compensation fan 2 is arranged at the waist of unmanned plane 1.
Described contact pilotage 6 and contact chip 7 are all brush.
The present invention is when in use：It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, including unmanned plane, compensation fan, wind
Xiang Biao, rotary shaft, disk, contact pilotage, contact chip, are consolidated disk by welding or bolted mode in the bottom of unmanned plane
Due to unmanned plane, disk inside edge is provided with is evenly arranged in eight contact chips on the inside of disk, disk around disc centre
Center be provided with the top of a rotary shaft, rotary shaft and be provided with a contact pilotage, the top edge of contact pilotage can be touched
Contact, the bottom of rotary shaft is provided with wind vane；The fuselage of unmanned plane installs eight compensation fans, and each compensation fan is right respectively
The direction of a contact chip is answered, and each compensation fan connects the contact chip of that side consistent with its direction respectively.
When unmanned plane carries out working flight, unmanned plane is inevitably acted on by the wind-force from side, wind direction
Mark can be rotated by the effect of wind-force, turn to at wind direction identical position.The rotated by rotation axle top of wind vane
The contact pilotage rotation in portion, contact pilotage is during rotation or touches contact chip, can trigger and connect when after contact pilotage and contact chip contact
The switch of the compensation fan of contact same position, compensation fan rotates reverse so as to be carried out to the wind-force that unmanned plane side is subjected to
Compensation, can avoid unmanned plane by course line of blowing off.
Generally, the present invention, which has, automatically adjusts flight balance, avoids unmanned plane from occurring off-line advantage.
Claims (5)
1. it is a kind of can according to the unmanned plane of wind direction self-adjusting balance, including unmanned plane, compensation fan, wind vane, rotary shaft, disk,
Contact pilotage, contact chip, it is characterised in that：Described unmanned plane bottom sets disk, and described disk inward flange sets contact chip, institute
Set in the middle part of the disk stated and contact pilotage is set at the top of rotary shaft, described rotary shaft, wind vane, institute are installed in described rotary shaft bottom
The unmanned plane surrounding stated installs compensation fan, and described contact chip is connected to compensation fan.
2. it is according to claim 1 it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, it is characterised in that：Described contact
Piece is set to eight, and is evenly arranged in disk inside edge around disc centre.
3. it is according to claim 1 or 2 it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, it is characterised in that：Described
The distribution arrangement for compensating the coupled contact chip of direction of fan is consistent.
4. it is according to claim 1 it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, it is characterised in that：Described compensation
Fan is arranged at the waist of unmanned plane.
5. it is according to claim 1 it is a kind of can be according to the unmanned plane of wind direction self-adjusting balance, it is characterised in that：Described contact pilotage
All it is brush with contact chip.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710335893.9A CN107031830A (en) | 2017-05-12 | 2017-05-12 | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710335893.9A CN107031830A (en) | 2017-05-12 | 2017-05-12 | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107031830A true CN107031830A (en) | 2017-08-11 |
Family
ID=59538140
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710335893.9A Pending CN107031830A (en) | 2017-05-12 | 2017-05-12 | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107031830A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382588A (en) * | 2018-02-02 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | It can be according to the unmanned plane of wind direction self-adjusting balance |
| CN108583896A (en) * | 2018-04-19 | 2018-09-28 | 深圳市安思科电子科技有限公司 | A kind of good plant protection drone that work efficiency is high of pesticide spraying effect |
| CN108639316A (en) * | 2018-03-29 | 2018-10-12 | 成都众宜合生科技有限公司 | When a kind of landing can effectively damping unmanned plane |
| CN108657421A (en) * | 2018-03-29 | 2018-10-16 | 成都众宜合生科技有限公司 | It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights |
| CN108725782A (en) * | 2018-05-30 | 2018-11-02 | 永春县乾高智能科技有限公司 | A kind of intelligence mountain forest tour unmanned plane |
| CN109557335A (en) * | 2018-11-12 | 2019-04-02 | 中国航天空气动力技术研究院 | A kind of near space anemoscope |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2003244415A1 (en) * | 2002-02-07 | 2003-09-02 | Levitation Technologies Ltd. | Stabilisation and control of aircraft and other objects |
| KR20160010711A (en) * | 2014-07-17 | 2016-01-28 | 서울과학기술대학교 산학협력단 | multicopter |
| US20160159472A1 (en) * | 2014-12-04 | 2016-06-09 | Elwha Llc | Reconfigurable unmanned aircraft system |
| CN205311901U (en) * | 2015-11-24 | 2016-06-15 | 郑州大学 | Remote control aircraft |
| KR20160116748A (en) * | 2015-03-31 | 2016-10-10 | 주식회사 샘코 | Wind direction auto directional VTOL drone and the method for controlling the same |
| CN106275410A (en) * | 2016-11-17 | 2017-01-04 | 湖南科瑞特科技股份有限公司 | A kind of wind disturbance resistant unmanned plane |
| CN106502262A (en) * | 2015-09-08 | 2017-03-15 | 中国农业机械化科学研究院 | A kind of agricultural unmanned plane during flying platform and its control system and control method |
| CN106585966A (en) * | 2016-12-13 | 2017-04-26 | 天津传承科技有限公司 | Electromechanical integration unmanned aerial vehicle device capable of smoothly taking off and landing |
-
2017
- 2017-05-12 CN CN201710335893.9A patent/CN107031830A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2003244415A1 (en) * | 2002-02-07 | 2003-09-02 | Levitation Technologies Ltd. | Stabilisation and control of aircraft and other objects |
| KR20160010711A (en) * | 2014-07-17 | 2016-01-28 | 서울과학기술대학교 산학협력단 | multicopter |
| US20160159472A1 (en) * | 2014-12-04 | 2016-06-09 | Elwha Llc | Reconfigurable unmanned aircraft system |
| KR20160116748A (en) * | 2015-03-31 | 2016-10-10 | 주식회사 샘코 | Wind direction auto directional VTOL drone and the method for controlling the same |
| CN106502262A (en) * | 2015-09-08 | 2017-03-15 | 中国农业机械化科学研究院 | A kind of agricultural unmanned plane during flying platform and its control system and control method |
| CN205311901U (en) * | 2015-11-24 | 2016-06-15 | 郑州大学 | Remote control aircraft |
| CN106275410A (en) * | 2016-11-17 | 2017-01-04 | 湖南科瑞特科技股份有限公司 | A kind of wind disturbance resistant unmanned plane |
| CN106585966A (en) * | 2016-12-13 | 2017-04-26 | 天津传承科技有限公司 | Electromechanical integration unmanned aerial vehicle device capable of smoothly taking off and landing |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382588A (en) * | 2018-02-02 | 2018-08-10 | 天津翰宇昊德科技发展有限公司 | It can be according to the unmanned plane of wind direction self-adjusting balance |
| CN108639316A (en) * | 2018-03-29 | 2018-10-12 | 成都众宜合生科技有限公司 | When a kind of landing can effectively damping unmanned plane |
| CN108657421A (en) * | 2018-03-29 | 2018-10-16 | 成都众宜合生科技有限公司 | It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights |
| CN108583896A (en) * | 2018-04-19 | 2018-09-28 | 深圳市安思科电子科技有限公司 | A kind of good plant protection drone that work efficiency is high of pesticide spraying effect |
| CN108725782A (en) * | 2018-05-30 | 2018-11-02 | 永春县乾高智能科技有限公司 | A kind of intelligence mountain forest tour unmanned plane |
| CN109557335A (en) * | 2018-11-12 | 2019-04-02 | 中国航天空气动力技术研究院 | A kind of near space anemoscope |
| CN109557335B (en) * | 2018-11-12 | 2020-09-18 | 中国航天空气动力技术研究院 | Near space anemoscope |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107031830A (en) | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance | |
| CN104787317B (en) | Aircraft and its control method | |
| CN107458599B (en) | Electric distributed propulsion reactive torque redundant power and control system | |
| CN107323653A (en) | One kind vertical lift tilting rotor wing unmanned aerial vehicle and its control method | |
| CN103072690A (en) | Single-ducted coaxial rotor/propeller saucer-shaped aircraft | |
| KR102077291B1 (en) | Flight vehicle and controlling method thereof | |
| CN203199178U (en) | Single-duct coaxial rotor/propeller saucer-shaped aircraft | |
| RU2016117529A (en) | JET PLANE WITH A SHORTED OR VERTICAL TAKE-OFF AND LANDING (OPTIONS) | |
| KR102032243B1 (en) | Tilt-prop air vehicle | |
| CN204623829U (en) | Aircraft | |
| CN205022859U (en) | Hybrid plant protection unmanned aerial vehicle tranquilizer | |
| CN104787322B (en) | Power system and multi-axis aircraft | |
| CN206945733U (en) | A kind of wind direction detection means for unmanned plane | |
| CN206939067U (en) | It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance | |
| CN206446792U (en) | Aircraft | |
| CN109367762B (en) | Auxiliary control surface control device of tilting ducted aircraft | |
| CN204660024U (en) | A kind of dish-type rotor unmanned helicopter | |
| CN109204805A (en) | A kind of DCB Specimen unmanned plane of external motor | |
| CN206719540U (en) | Tilting rotor type VUAV based on Flying-wing | |
| CN104743109B (en) | Dynamical system and aircraft | |
| WO2019080442A1 (en) | Rotorcraft | |
| CN205060003U (en) | Low novel multiaxis unmanned aerial vehicle of power consumption cruises | |
| CN204368425U (en) | The rainproof unmanned plane of a kind of rotary wind type | |
| CN204623840U (en) | Power system and aircraft | |
| CN204623836U (en) | Power system and multi-axis aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170811 |