CN108275265A - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN108275265A CN108275265A CN201810087202.2A CN201810087202A CN108275265A CN 108275265 A CN108275265 A CN 108275265A CN 201810087202 A CN201810087202 A CN 201810087202A CN 108275265 A CN108275265 A CN 108275265A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- propeller
- turned
- sensor
- speed
- 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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
- B64C2027/8236—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft including pusher propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- 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
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of unmanned planes, including multiple fixed propellers；Multiple propellers turned to, wherein the propeller that can each turn to is configured as being rotated in 0 to 90 degree ranges according to the direction of motion of unmanned plane；With one group of sensor, the speed of fixed propeller and the propeller that can be turned to can be adjusted according to the speed of wind and direction.The unmanned plane of the present invention is additionally arranged one group of sensor, unmanned plane is allow to automatically adjust the speed of propeller according to the direction of motion of itself, optimize the use of battery, so that unmanned plane fly higher and stay aloft longer time, and the present invention is not necessarily to increase the size of battery compared with traditional technology, can increase the cruising ability of unmanned plane while not increasing take-off weight.The present invention can be widely applied to aircraft field.
Description
Technical field
The present invention relates to aircraft field, especially a kind of unmanned plane.
Background technology
Unmanned plane compares the aircraft such as aircraft or helicopter one kind, is flown by the control signal of radio wave
Rather than it is driven by the mankind on board the aircraft.They may carry various articles, such as camera, sensor and communication equipment
Deng.Different unmanned planes may be widely different in terms of size and sophistication.In general, a unmanned plane includes propulsion system, uses
In providing the power source of power, steering mechanism, the controller of telecommunication system and all components of installation for propulsion system
Rack.Small drone generally includes multiple propellers or rotor and drive motor, and the size of unmanned plane is reduced with this,
And increase lift.
However, present unmanned plane is since the limitation of battery cannot fly very high and cannot stay aloft very long
Time, small drone increases the size of battery and unrealistic usually using battery powered motor, because of meeting in this way
Influence the total weight of unmanned plane.
In view of the foregoing, need a kind of flight time that can increase unmanned plane without increasing battery size technical side
Case.
Invention content
In order to solve the above technical problems, the first object of the present invention is：A kind of high-time unmanned plane is provided.
The technical solution used in the present invention is：
A kind of unmanned plane, including：
Multiple fixed propellers；
Multiple propellers turned to, wherein the propeller that can each turn to is configured as the direction of motion according to unmanned plane
It is rotated in 0 to 90 degree ranges；With
One group of sensor, the propeller that fixed propeller can be adjusted according to the speed of wind and direction and can turned to
Speed.
Further, the unmanned plane carries out remote control by using the remote control apparatus of RF technologies.
Further, the unmanned plane includes processor, in order to which user is remote in the application program that its smart mobile phone is run
Process control unmanned plane.
Further, during unmanned plane moves upwards, the propeller that can each turn to can manually or automatically turn
To so that the propeller that can each turn to is parallel to the wing of unmanned plane.
Further, during unmanned plane travels forward, the propeller that can each turn to can manually or automatically turn
To so that wing of the propeller that can each turn to perpendicular to unmanned plane.
Further, further include the camera scanned in the air for executing outdoor environment.
Further, one group of sensor includes at least one in wind transducer, air velocity transducer and direction sensor
Kind
The beneficial effects of the invention are as follows：Including multiple fixed propellers, multiple propellers turned to and one group of sensing
Device, unmanned plane of the invention are additionally arranged one group of sensor so that unmanned plane can automatically adjust spiral shell according to the direction of motion of itself
The speed for revolving paddle, optimizes the use of battery so that unmanned plane can stay aloft the longer time.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of unmanned plane that can be flown upwards of the embodiment of the present invention；
Fig. 2 is a kind of structural schematic diagram of unmanned plane for capableing of flight forward of the embodiment of the present invention；
Fig. 3 is a kind of schematic diagram of the camera of unmanned plane of the embodiment of the present invention.
Specific implementation mode
Referring to Figures 1 and 2, a kind of unmanned plane 100, including：
Multiple fixed propellers (including the first fixation propeller 104c, the second fixation propeller 104d and third are fixed
Propeller 104e)；
Multiple propellers (including first can screw-rudder 104a and second can screw-rudder 104b) turned to,
In the propeller that can each turn to be configured as being rotated in 0 to 90 degree ranges according to the direction of motion of unmanned plane；With
One group of sensor, the propeller that fixed propeller can be adjusted according to the speed of wind and direction and can turned to
Speed.
It is further used as preferred embodiment, the unmanned plane is carried out by using the remote control apparatus of RF technologies
Remote control.
It is further used as preferred embodiment, the unmanned plane includes processor, in order to which user is in its smart mobile phone
Remote control unmanned plane in the application program of operation.
Referring to Fig.1, it is further used as preferred embodiment, during unmanned plane 100 moves upwards, can each be turned
To propeller can manually or automatically turn to so that the propeller that can each turn to is parallel to the wing 102 of unmanned plane.
With reference to Fig. 2, it is further used as preferred embodiment, during unmanned plane 100 travels forward, can each be turned
To propeller can manually or automatically turn to so that wing 102 of the propeller that can each turn to perpendicular to unmanned plane.
With reference to Fig. 3, it is further used as preferred embodiment, further includes the phase scanned in the air for executing outdoor environment
Machine 114.
It is further used as preferred embodiment, one group of sensor includes wind transducer, air velocity transducer and side
To at least one of sensor.
In the following description, in order to be explained to the present invention, many details are elaborated in order to thoroughly understand
The present invention.However to those skilled in the art, it is that can realize the present invention without these specific details
, in other cases, it may be only shown in block diagram form structure and equipment, to avoid the present invention is obscured.
The reference of " one embodiment " or " embodiment " is meaned in the present specification to combine embodiment description
Technical characteristic, structure or characteristic are included at least one embodiment of the invention.The phrase occurred everywhere in specification
" in one embodiment " it is not necessarily all referring to identical embodiment.Nor with mutually exclusive independent of other embodiment or replacing
For embodiment.And some features may be described by certain some embodiment, and other embodiment does not describe.Similarly, some
Certain some embodiment may be directed to without limiting other embodiment by limiting.
The present invention is further detailed with specific embodiment with reference to the accompanying drawings of the specification.
Fig. 1 shows the unmanned plane 100 moved up of an embodiment of the present invention.
Unmanned plane 100 is the fixed-wing unmanned plane for having wing 102 comprising first can screw-rudder 104a, second
It can screw-rudder 104b, the first fixation propeller 104c (reference can be made to Fig. 2), the second fixation propeller 104d and third fixation spiral shell
Revolve paddle 104e (being referred to as propeller below).It will be apparent to one skilled in the art that can will be greater number of
Propeller is added in unmanned plane 100, these obvious embodiments are also in the protection domain of the application.
The motor drive that the propeller can be battery powered by one or more, and respectively in unmanned plane 100
It is upward or provide necessary upward or forward thrust during travelling forward.
In one embodiment, remote control remote control unmanned plane 100 can be passed through using RF technologies.In another reality
Apply in example, unmanned plane 100 include processor so that user can smart phone run application program come remote control nobody
Machine.The processor can control the propeller of unmanned plane.
In one embodiment, unmanned plane 100 includes one or more onboard sensors, as wind transducer, wind speed pass
Sensor, heat-sensitive sensor and direction sensor, to automatically adjust the speed of propeller according to the direction of motion of unmanned plane 100,
Optimize the use of battery so that unmanned plane 100 fly higher and stay aloft longer time.
For example, if 100 downwind of unmanned plane, one or more airborne sensors can sense wind direction, then
Reduce the speed of propeller 104., whereas if 100 headwind flight of unmanned plane, then can increase the speed of propeller.
In one embodiment, unmanned plane 100 carries the camera 112 that can be used for scanning outdoor environment in the air,
The purpose of hollow middle scanning is to generate the two-dimensional/three-dimensional view of outdoor environment.It is aobvious and easy to those skilled in the art
See, other cameras (such as RBG cameras) and sensor can be added in unmanned plane 100, these obvious implementations
Mode is also in the protection domain of the application.
Fig. 2 shows a kind of embodiments of the present invention：The unmanned plane 100 of forward movement.
Unmanned plane 100 during travelling forward, first can screw-rudder 104a and second can screw-rudder
104b can be turned to manually or automatically, described first can screw-rudder 104a and second can screw-rudder 104b can be with
Rotation in the plane vertical with wing 102, described first can screw-rudder 104a and second can screw-rudder 104b exist
When 100 flight forward of unmanned plane, in the plane vertical with wing 102, described first can screw-rudder 104a and second
Can screw-rudder 104b provide forward thrust to unmanned plane 100, convenient for unmanned plane 100 stay aloft longer time, with
Promote the use of the flight time and optimization battery of unmanned plane 100.
Fig. 3 shows to be embedded in an embodiment of the present invention in unmanned plane 100 and be swept for executing the aerial of outdoor environment
The built-in camera 114 retouched.
It will be apparent to one skilled in the art that unmanned plane 100 can be used in addition to capturing video or figure
Other application as other than, these obvious embodiments are also in the protection domain of the application.Such as unmanned plane 100 can be used
In remote sensing reference, transmission application, aviation monitoring, business, animated film making, energy exploration (including oil, natural gas and mine
Production), the disaster relief, real estate, building and recreational use.
There have been described herein many concrete details in order to understand thoroughly the multiple possible of the unmanned plane in the present invention
Embodiment.However, those skilled in the art can implement these embodiments without these specific details.At other
In the case of, well known method, process, component and circuit are not described in detail, in order to avoid obscure embodiment.In addition, public in embodiment
The specific structure and function details opened are representative, but are not intended that the invention be limited to the model of these embodiments
It encloses.
It is to be illustrated to the preferable implementation of the present invention, but the present invention is not limited to the embodiment above, it is ripe
Various equivalent variations or replacement can also be made under the premise of without prejudice to spirit of that invention by knowing those skilled in the art, this
Equivalent deformation or replacement are all contained in the application claim limited range a bit.
Claims (7)
1. a kind of unmanned plane, which is characterized in that including：
Multiple fixed propellers；
Multiple propellers turned to, wherein the propeller that can each turn to is configured as the direction of motion according to unmanned plane 0
It is rotated within the scope of to 90 degree；With
One group of sensor can adjust the speed of fixed propeller and the propeller that can be turned to according to the speed of wind and direction
Degree.
2. a kind of unmanned plane according to claim 1, it is characterised in that：The unmanned plane is long-range by using RF technologies
Control device carries out remote control.
3. a kind of unmanned plane according to claim 1, it is characterised in that：The unmanned plane includes processor, in order to
Family remote control unmanned plane in the application program that its smart mobile phone is run.
4. a kind of unmanned plane according to claim 1, it is characterised in that：During unmanned plane moves upwards, each
The propeller that can be turned to can be turned to manually or automatically, so that the propeller that can each turn to is parallel to the wing of unmanned plane.
5. a kind of unmanned plane according to claim 1, it is characterised in that：During unmanned plane travels forward, each
The propeller that can be turned to can be turned to manually or automatically, so that wing of the propeller that can each turn to perpendicular to unmanned plane.
6. a kind of unmanned plane according to claim 1, it is characterised in that：Further include being swept for executing the aerial of outdoor environment
The camera retouched.
7. a kind of unmanned plane according to claim 1, it is characterised in that：One group of sensor include wind transducer,
At least one of air velocity transducer and direction sensor.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201762595608P | 2017-12-07 | 2017-12-07 | |
| US62/595,608 | 2017-12-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108275265A true CN108275265A (en) | 2018-07-13 |
Family
ID=62805709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810087202.2A Pending CN108275265A (en) | 2017-12-07 | 2018-01-30 | A kind of unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN108275265A (en) |
| WO (1) | WO2019109621A1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2597786B (en) * | 2020-08-06 | 2024-04-10 | Vertical Aerospace Group Ltd | Flying vehicle rotor arrangement |
| TWI786978B (en) * | 2021-12-07 | 2022-12-11 | 國立虎尾科技大學 | System for controlling powerless fixed-wing airplane |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014045276A1 (en) * | 2012-09-23 | 2014-03-27 | Israel Aerospace Industries Ltd. | A system, a method and a computer program product for maneuvering of an air vehicle |
| CN105867416A (en) * | 2016-04-20 | 2016-08-17 | 北京博瑞爱飞科技发展有限公司 | Flying control method and device of unmanned aerial vehicle and unmanned aerial vehicle |
| CN205738117U (en) * | 2016-06-27 | 2016-11-30 | 江苏冰城氢能科技有限公司 | Fixed-wing unmanned plane |
| CN206125423U (en) * | 2016-11-02 | 2017-04-26 | 北京航空航天大学 | VTOL fixed wing uavs with power device verts |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149982B (en) * | 2014-04-11 | 2017-02-01 | 陕西科技大学 | Air quality detector based on quadcopter |
| CN106627010A (en) * | 2016-11-17 | 2017-05-10 | 苏州航天系统工程有限公司 | Water-air amphibious unmanned aerial vehicle |
| CN106527484B (en) * | 2016-12-13 | 2019-08-09 | 安徽天德无人机科技有限公司 | A kind of unmanned plane during flying lane management system based on electromechanical integration |
| CN106527486B (en) * | 2016-12-16 | 2018-01-02 | 常州市环境监测中心 | A kind of unmanned plane for sample detecting of being dwelt more for land and water |
| CN106809382B (en) * | 2017-01-20 | 2019-01-15 | 亿航智能设备（广州）有限公司 | A kind of aircraft and its control method |
-
2018
- 2018-01-30 CN CN201810087202.2A patent/CN108275265A/en active Pending
- 2018-06-15 WO PCT/CN2018/091590 patent/WO2019109621A1/en active Application Filing
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014045276A1 (en) * | 2012-09-23 | 2014-03-27 | Israel Aerospace Industries Ltd. | A system, a method and a computer program product for maneuvering of an air vehicle |
| CN105867416A (en) * | 2016-04-20 | 2016-08-17 | 北京博瑞爱飞科技发展有限公司 | Flying control method and device of unmanned aerial vehicle and unmanned aerial vehicle |
| CN205738117U (en) * | 2016-06-27 | 2016-11-30 | 江苏冰城氢能科技有限公司 | Fixed-wing unmanned plane |
| CN206125423U (en) * | 2016-11-02 | 2017-04-26 | 北京航空航天大学 | VTOL fixed wing uavs with power device verts |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019109621A1 (en) | 2019-06-13 |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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Application publication date: 20180713 |