CN107054638A - A kind of underneath type coaxial double-rotary wing unmanned plane - Google Patents
A kind of underneath type coaxial double-rotary wing unmanned plane Download PDFInfo
- Publication number
- CN107054638A CN107054638A CN201710153858.5A CN201710153858A CN107054638A CN 107054638 A CN107054638 A CN 107054638A CN 201710153858 A CN201710153858 A CN 201710153858A CN 107054638 A CN107054638 A CN 107054638A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- rotor
- aircraft body
- rotary wing
- coaxial double
- 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
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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- 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
- 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
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a kind of underneath type coaxial double-rotary wing unmanned plane, the unmanned plane includes two groups of rotors, aircraft body, cross eccentric, LED and shows light pearl, wide angle cameras and motor；Wide angle cameras is arranged on aircraft body upper end, rotor is arranged on aircraft body bottom, two groups of upper and lower co-axial alignments of rotor, turn to opposite and overlapped with aircraft body main shaft, motor is provided with above rotor, cross eccentric is arranged on the deflection that center of gravity is realized inside aircraft body, and LED shows that light pearl is arranged on rotor bottom side.The present invention, without transmission mechanism, realizes the change of posture, compact conformation is lightweight using identical but two opposite underneath type rotor counter balance torques of steering using the skew of center of gravity, and action is rapid and can be with stealthy.
Description
Technical field
The present invention relates to unmanned plane field, and in particular to a kind of underneath type coaxial double-rotary wing unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.
Unmanned plane as it is a kind of can multi-field reuse aviation aircraft, by its is cheap, intelligent high
Unique advantage, is widely used, particularly in military field, with the advanced unmanned plane system that " global hawk " is representative
The birth of system and a series of outstanding performance in tasks so that unmanned plane turns into a dazzling star.
The history for being developed so far existing more than 80 years of unmanned plane, earliest unmanned plane is just commonly used by people for military surveillance.So far
Untill the present, the actual combat that military unmanned air vehicle has been subjected to five local wars uses test.AUS FCS in the works, be
Improve the investigation ability of individual soldier or class other unit, it is proposed that the moderate unmanned vehicle of a kind of small volume, flying speed
It is used as the airborne platform of investigation equipment.Such unmanned vehicle can VTOL and hovering, and can by fan provide before
Fly before being realized to lift, with compact conformation, mobility it is good, unique perch surveillance coverage, the features such as disguised strong.
The rotor of traditional rotor aircraft hangs over the top of aircraft, is typically all single rotor longitudinal axis formula, by rear portion
Tail-rotor counter balance torque.The maximum feature of rotor tandem helicopter is technology maturation, is easily realized, and control is simple, but
It is that single rotor lap siding also has shortcomings, such as, for counter balance torque, the drive mechanism for rotating tail-rotor is heavy, adds winged
Row device empty mass etc..
The content of the invention
In view of this, the invention provides a kind of underneath type coaxial double-rotary wing unmanned plane, the unmanned plane is using identical
But two opposite underneath type rotor counter balance torques are turned to, without transmission mechanism, the change of posture is realized using the skew of center of gravity,
Compact conformation, lightweight, action is rapid and can be with stealthy.
A kind of underneath type coaxial double-rotary wing unmanned plane, the unmanned plane includes two groups of rotors, aircraft body, cross bias dress
Put, LED shows light pearl, wide angle cameras and motor；
Rotor is arranged on aircraft body bottom, two groups of upper and lower co-axial alignments of rotor, turn to it is opposite and with aircraft master
Body main shaft is overlapped, and motor is provided with above rotor, and cross eccentric is arranged on the deflection that center of gravity is realized inside aircraft body,
LED shows that light pearl is arranged on rotor bottom side, and the wide angle cameras is arranged on aircraft body upper end.
Further, the cross eccentric includes battery and cross guide rail, and battery is fixed on the sliding block of cross guide rail
On, do independent without coupled motions on transverse direction, longitudinal direction along guide rail, realize the deflection of center of gravity, adjust unmanned plane body posture.
Further, the aircraft body is cylindrical structure.
Further, the wide angle cameras top is provided with spherical mirror.
Further, the motor uses close coupled type DC brushless motor.
Further, the unmanned plane is provided with VTOL frame.
Further, the rotor is foldable.
Beneficial effect：
1st, the present invention is using identical but two opposite underneath type rotor counter balance torques of steering, without transmission mechanism,
Compact conformation, lightweight, action is rapid, by changing laterally opposed position of the barycenter relative to whole system, using gravity with
The change of posture is realized in the cooperation of bottom rotor, and controlling organization is simple；Light is shown by the LED for being arranged on lowermost end rotor bottom side
Pearl can be realized stealthy.
2nd, the present invention using rotor and the battery that is fixed on cross guide rail can posture change, mechanism is simple；And phase
For other utilize aerodynamic force control posture aircraft (such as fixed-wing, four rotors), the response speed of Moving mass control faster,
Avoid the time delay in control loop.
3rd, aircraft body of the present invention is cylindrical structure, is more suitable for carrying, convenient in carrying.
4th, the spherical mirror that wide angle cameras top of the present invention is set can reach 360 degree of visual angle, directly by it is lower extremely
It is upper to be shot, realize that earth observation is monitored, monitoring range is wide.
5th, the present invention use close coupled type DC brushless motor, can realize the supply of three phase electric machine electric power in rotation process with
And ensure the uniformity of the sense of current.
6th, the propeller blade of rotor of the present invention is foldable, and engaged position is small, is readily transported, launches.
Brief description of the drawings
Fig. 1 is overall structure diagram of the invention；
Fig. 2 is the partial view of cross guide rail of the present invention.
Wherein, 1- wide angle cameras, 2- batteries, 3- cross guide rails, 4- close coupled type DC brushless motors, 5- rotors, 6- hangs down
Straight undercarriage, 7- propeller blades.
Embodiment
The present invention will now be described in detail with reference to the accompanying drawings and examples.
For underneath type coaxial double-rotary wing unmanned plane, due to the limitation of volume, control the feature area of rudder face smaller
And relative velocity is smaller so that control moment does not reach the index of design, so the present invention is by the way of " Moving ",
" Moving " is, by changing laterally opposed position of the barycenter relative to whole system, to utilize the cooperation reality of gravity and bottom rotor
The change of existing posture.
The invention provides a kind of underneath type coaxial double-rotary wing unmanned plane, realized using cross eccentric " rotten
The heart ", the unmanned plane includes two groups of rotors 5, aircraft body, cross eccentric, LED and shows light pearl, wide angle cameras 1 and be total to
Shaft type DC brushless motor 4.
As shown in figure 1, aircraft body is cylindrical structure, wide angle cameras 1 is arranged on aircraft body upper end, rotor 5
Installed in aircraft body bottom, two groups of upper and lower co-axial alignments of rotor 5 are turned to opposite and overlapped with aircraft body main shaft,
The top of rotor 5 is provided with close coupled type DC brushless motor 4, and cross eccentric is arranged on inside aircraft body and realizes center of gravity
Deflection, LED shows that light pearl is arranged on the bottom side of rotor 5, and it can send corresponding light according to residing flight environment of vehicle color, by
The high speed rotation of rotor 5, reaches merging for aircraft color and surrounding environment, so as to realize that the vision to human eye of aircraft is hidden
Body.Unmanned plane is provided with VTOL frame 6, can be without this device when radiation pattern is projectile or big gun is penetrated.
As shown in Fig. 2 cross eccentric includes battery 2 and cross guide rail 3, battery 2 is fixed on the sliding block of cross guide rail 3
On, do independent without coupled motions on transverse direction, longitudinal direction along cross guide rail 3, realize the deflection of center of gravity, adjust unmanned plane body
Posture.Concrete methods of realizing is, when needing to change posture, and the adjustment main counterweight of aircraft is the position of battery, makes aircraft
Center of gravity occur lateral deflection, deviate one thin tail sheep of main shaft, because the direction of lift is overlapped with the main shaft of aircraft all the time, because
This is after deviation of gravity center main shaft, and lift just produces a smaller moment of torsion to system, so that the posture of system changes,
The response speed of Moving mass control is faster, it is to avoid the time delay in control loop.
The top of wide angle cameras 1 is provided with spherical mirror, when photographic subjects are located at aircraft upper end, is most pushed up positioned at aircraft
The wide angle cameras 1 at end can not directly keep a splendid viewing angles by any device.When reference object is to ground
During target, the spherical mirror combination wide angle cameras 1 at top can realize that 360 omnidirectional shoots, but when being due to shooting, wide-angle is taken the photograph
Camera 1 is located at the top of aircraft body, and the subregion of the bottom of rotor 5 is difficult to photograph, i.e., detector has dead angle, can pass through
Aircraft changes its position, or constantly motion makes up the shortcoming of dead angle presence.
Every group of rotor 5 is made up of four propeller blades 7, and the propeller blade 7 of rotor 5 can be folded up, and takes position
Put small, be readily transported, launch.When DCB Specimen hovers, because the contraction of upper rotor wake is expanded by the drainage of lower rotor,
So as to add the effective district of wake flow, it is possible to eliminate the eddy flow loss of wake flow, therefore with more preferably hovering efficiency.Close coupled type
DCB Specimen does not need extra constitutional balance moment of torsion, eliminates many drive mechanisms, therefore the gross weight of aircraft can also drop significantly
Low, structure is compacter, and shared physical dimension is smaller, and close coupled type rotor craft air force keeps symmetrical, because
This have higher driving efficiency, be adapted to minimize, can take off vertically, the unmanned surveillance plane of hovering.
In summary, presently preferred embodiments of the present invention is these are only, is not intended to limit the scope of the present invention.
Within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., should be included in the present invention's
Within protection domain.
Claims (7)
1. a kind of underneath type coaxial double-rotary wing unmanned plane, it is characterised in that the unmanned plane include two groups of rotors, aircraft body,
Cross eccentric, LED show light pearl, wide angle cameras and motor；
Rotor is arranged on aircraft body bottom, two groups of upper and lower co-axial alignments of rotor, turn to it is opposite and with aircraft body master
Motor is provided with above overlapping of axles, rotor, cross eccentric is arranged on the deflection that center of gravity is realized inside aircraft body, LED
Display light pearl is arranged on rotor bottom side, and the wide angle cameras is arranged on aircraft body upper end.
2. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the cross eccentric includes
Battery and cross guide rail, battery are fixed on the sliding block of cross guide rail, do independent without coupling on transverse direction, longitudinal direction along guide rail
Motion, realizes the deflection of center of gravity, adjusts unmanned plane body posture.
3. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the aircraft body is cylinder
Structure.
4. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the wide angle cameras top peace
Equipped with spherical mirror.
5. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the motor is straight using close coupled type
Flow brushless electric machine.
6. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the unmanned plane is provided with vertically
Undercarriage.
7. underneath type coaxial double-rotary wing unmanned plane as claimed in claim 1, it is characterised in that the rotor is foldable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710153858.5A CN107054638A (en) | 2017-03-15 | 2017-03-15 | A kind of underneath type coaxial double-rotary wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710153858.5A CN107054638A (en) | 2017-03-15 | 2017-03-15 | A kind of underneath type coaxial double-rotary wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107054638A true CN107054638A (en) | 2017-08-18 |
Family
ID=59619982
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710153858.5A Pending CN107054638A (en) | 2017-03-15 | 2017-03-15 | A kind of underneath type coaxial double-rotary wing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107054638A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110619832A (en) * | 2019-11-13 | 2019-12-27 | 徐州乐泰机电科技有限公司 | Novel propeller structure |
| CN112634609A (en) * | 2020-12-14 | 2021-04-09 | 成都飞航智云科技有限公司 | Situation early warning system based on knowledge base |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2928183Y (en) * | 2006-07-28 | 2007-08-01 | 杜大森 | Gravity regulating structure of remote control helicoptor |
| CN201168442Y (en) * | 2008-01-08 | 2008-12-24 | 沈金钟 | Portable unmanned special helicopter for aerial photography |
| US20100012774A1 (en) * | 2006-05-15 | 2010-01-21 | Kazak Composites, Incorporated | Powered unmanned aerial vehicle |
| CN101652286A (en) * | 2007-01-18 | 2010-02-17 | 保罗·E·阿尔托恩 | Rotarycraft power and propulsion system |
| CN102910287A (en) * | 2011-08-02 | 2013-02-06 | 深圳市联讯创新工场科技开发有限公司 | Rotor aircraft |
| CN103979106A (en) * | 2014-04-29 | 2014-08-13 | 浙江大学 | Rotor-type unmanned aerial vehicle automatically adjusting gravity center and adjustment method |
| CN205311892U (en) * | 2015-12-30 | 2016-06-15 | 苏州妙旋无人机应用有限公司 | Controllable formula unmanned aerial vehicle of focus |
-
2017
- 2017-03-15 CN CN201710153858.5A patent/CN107054638A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100012774A1 (en) * | 2006-05-15 | 2010-01-21 | Kazak Composites, Incorporated | Powered unmanned aerial vehicle |
| CN2928183Y (en) * | 2006-07-28 | 2007-08-01 | 杜大森 | Gravity regulating structure of remote control helicoptor |
| CN101652286A (en) * | 2007-01-18 | 2010-02-17 | 保罗·E·阿尔托恩 | Rotarycraft power and propulsion system |
| CN201168442Y (en) * | 2008-01-08 | 2008-12-24 | 沈金钟 | Portable unmanned special helicopter for aerial photography |
| CN102910287A (en) * | 2011-08-02 | 2013-02-06 | 深圳市联讯创新工场科技开发有限公司 | Rotor aircraft |
| CN103979106A (en) * | 2014-04-29 | 2014-08-13 | 浙江大学 | Rotor-type unmanned aerial vehicle automatically adjusting gravity center and adjustment method |
| CN205311892U (en) * | 2015-12-30 | 2016-06-15 | 苏州妙旋无人机应用有限公司 | Controllable formula unmanned aerial vehicle of focus |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110619832A (en) * | 2019-11-13 | 2019-12-27 | 徐州乐泰机电科技有限公司 | Novel propeller structure |
| CN112634609A (en) * | 2020-12-14 | 2021-04-09 | 成都飞航智云科技有限公司 | Situation early warning system based on knowledge base |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7665688B2 (en) | Convertible aerial vehicle with contra-rotating wing/rotors and twin tilting wing and propeller units | |
| US20150136897A1 (en) | Aircraft, preferably unmanned | |
| US8167234B1 (en) | Insect-like micro air vehicle having perching, energy scavenging, crawling, and offensive payload capabilities | |
| US20200010182A1 (en) | Pivoting wing system for vtol aircraft | |
| US11866166B2 (en) | System forming a two degrees of freedom actuator, for example for varying the pitch angle of the blades of a propeller during rotation | |
| JP2015501751A (en) | Method and apparatus for vertical / short-range take-off and landing | |
| CN204473140U (en) | New vertical landing tilting rotor two axle aircraft | |
| NL2016130B1 (en) | Multiple pairs of flapping wings for attitude control. | |
| JP2010208501A (en) | Unmanned aircraft and unmanned aircraft system | |
| CN102167155B (en) | Aircraft with turnable wings | |
| CN109606674A (en) | Tail sitting posture vertical take-off and landing drone and its control system and control method | |
| US10814972B2 (en) | Air vehicle and method and apparatus for control thereof | |
| CN109178315A (en) | A kind of scouting operation miniature drone of absorption type | |
| US11866205B2 (en) | Flying wing aircraft having a two-dimensional thrust array | |
| KR20200080825A (en) | Veryical takeoff and landing fixed wing unmanned aerial vehicle | |
| US11130569B2 (en) | Flying wing aircraft having a two-dimensional thrust array | |
| CN106005371B (en) | Difference directly drives dynamic three rudder face unmanned planes entirely | |
| WO2019119409A1 (en) | Unmanned aerial vehicle and control method for unmanned aerial vehicle | |
| CN107054638A (en) | A kind of underneath type coaxial double-rotary wing unmanned plane | |
| US11124296B2 (en) | Flying wing aircraft having flight and storage configurations | |
| CN107444606B (en) | Novel aircraft and aircraft system | |
| RU165676U1 (en) | UAV VERTICAL TAKEOFF AND LANDING | |
| KR20160023285A (en) | Tilt-Cube-In-Wing Unmanned Aerial Vehicle | |
| CA2315524A1 (en) | Personal hoverplane having four tiltmotors | |
| CN109305356A (en) | A kind of tilting type vertical take-off and landing drone |
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: 20170818 |