CN109178312A - Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment - Google Patents
Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment Download PDFInfo
- Publication number
- CN109178312A CN109178312A CN201811207400.4A CN201811207400A CN109178312A CN 109178312 A CN109178312 A CN 109178312A CN 201811207400 A CN201811207400 A CN 201811207400A CN 109178312 A CN109178312 A CN 109178312A
- Authority
- CN
- China
- Prior art keywords
- laser
- fuselage
- remote sensing
- unmanned vehicle
- satellite navigation
- 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.)
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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
- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J50/00—Circuit arrangements or systems for wireless supply or distribution of electric power
- H02J50/30—Circuit arrangements or systems for wireless supply or distribution of electric power using light, e.g. lasers
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- 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
- B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment, including remote sensing unmanned vehicle and laser, remote sensing unmanned vehicle includes fuselage, landing gear, propeller, blade, solar panel, laser charger receiver and battery, three endpoints of fuselage respectively have a propeller, solar panel is equipped on fuselage, there is battery below the fuselage, hemispherical laser charger receiver is fixedly mounted on fuselage bottom, laser includes laser transmitter projects mouth and laser emitter fuselage, laser emitter fuselage end has laser transmitter projects mouth.The present invention, which is matched by photovoltaic power generation with wireless electric laser two ways, charges to unmanned plane, guarantee that unmanned plane stays in the air as navigation remote sensing intermediary as far as possible, navigation signal function can be increased as needed, stable signal is transmitted in corresponding region, and needs mating corresponding ancillary equipment according to real flight conditions and function.
Description
Technical field
The present invention relates to satellite remote sensing fields, and more particularly to cooperation satellite navigation, with laser charging photovoltaic remote sensing, nobody flies
Row device and laser equipment.
Background technique
Unmanned plane can realize the acquisition of high resolution image, make up satellite remote sensing often because cloud cover is obtained less than shadow
While as disadvantage, it is too long to solve conventional satellite remote sensing revisiting period, emergency not in time the problems such as.But its long-time flies
Row, can not charge in time is a urgent problem to be solved, with the continuous development of the high-energy charged technology of laser, it may be considered that design
Corresponding charging equipment can cooperate corresponding to charge to unmanned plane using unmanned vehicle as terminal in this way
Satellite remote sensing, it is contemplated that unmanned plane is expensive as remote sensing equipment and various situations may awing occur, it is therefore desirable to set
Corresponding ancillary equipment is counted to be coped with.
Summary of the invention
In order to solve problem above, the present invention provide cooperation satellite navigation with laser charge photovoltaic remote sensing unmanned vehicle and
Laser equipment is matched with wireless electric laser two ways by photovoltaic power generation and is charged to unmanned plane, guarantees unmanned plane as far as possible
As navigation, remote sensing intermediary is stayed in the air, can carry out circulation flight in fixed area as needed and specific region increases navigation
Semiotic function transmits stable signal in corresponding region, and mating corresponding auxiliary according to real flight conditions and function needs
Equipment is helped, for this purpose, the present invention provides cooperation satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and source, laser apparatus
Standby, including remote sensing unmanned vehicle and laser, GPS navigation chip built in the remote sensing unmanned vehicle and satellite carry out position
Remote sensing, the remote sensing unmanned vehicle include that fuselage, landing gear, propeller, blade, solar panel, laser charger connect
Device and battery are received, the fuselage main body is equilateral triangle, and three endpoints of the fuselage respectively have a propeller, described each
It is arc section on the outside of rotor connected component, the blade is mounted in the shaft of propeller, is equipped with solar energy on the fuselage
There are battery in solar panel, the fuselage lower section, respectively there is a landing gear below three sides of the fuselage, and the hemispherical swashs
Light charger receiver is fixedly mounted on fuselage bottom, the hemispherical laser charger receiver have 3 angularly around fuselage
Center line one week, the laser includes laser transmitter projects mouth and laser emitter fuselage, the laser emitter machine
There is laser transmitter projects mouth in body end, and the laser is hand held laser or pedestal rotary laser device, the holding
Laser emitter fuselage bottom has laser emitter handle, laser emitter in the pedestal rotary laser device in formula laser
Fuselage bottom has rotating shaft electric motor, and the rotating shaft electric motor is mounted in fixing seat.
There are camera in further improvement of the present invention, fuselage main body middle part lower section, and the camera is infrared remote sensing
Camera can carry out landform monitoring since the application is mainly used for fixed area flight, participate in meteorological exploration fire alarm etc.
Work.
There is a circle flexible protection ring in further improvement of the present invention, each propeller outside, has outside each rotor of the present invention
One circle flexible rings, can prevent impact brought by birds collision.
Further improvement of the present invention, the landing gear are that telescopic landing gear includes two air-cylinder types landing telescopic rods,
Each air-cylinder type landing flexible foot pad in telescopic rod bottom end, landing gear, which can according to need, to be stretched, in this way can as far as possible not
Flight is influenced, flexible foot pad, which is arranged, can reduce landing to damage brought by internal part.
Further improvement of the present invention has infra-red detection in the middle part of the arc section on the outside of each rotor connected component
Device is provided with infrared inductor in the middle part of the connected arc end of each rotor of the present invention, when having sensed that object proximity can carry out phase
The evacuation answered.
Further improvement of the present invention, the top of three sides of the fuselage are respectively equipped with a bird repellent sound equipment, this hair
It is bright to be influenced due to will receive birds in flight course, it is provided with sound equipment, when birds are expelled close to noise is released.
The present invention cooperates satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment, may be implemented as follows
Function；
1, it is provided with GPS navigation chip in unmanned plane main body of the present invention, can be used as navigation intermediary and stops for a long time in the sky, root
Circulation flight is carried out in fixed area according to needs and specific region increases navigation signal function；
2, the present invention is matched with wireless electric laser two ways by photovoltaic power generation and is charged to unmanned plane, in this way can be great
Guarantee the cruise duration of unmanned plane, top has solar panel that can carry out solar recharging, and bottom is provided with laser and fills
Electric solar energy solar panel can remotely be charged with laser, so as to greatly guarantee aircraft as navigation intermediary
Cruise duration；
3, unmanned plane main structure of the present invention uses mating three rotors of three-legged structure, is circular arc on the outside of each rotor connected component
Section maximum can reduce influence of the wind-force to unmanned plane in this way, more compact using three rotor design structures and just in case single
Only rotor, which is damaged, can use the progress emergency landing of other two rotor, so as to realize stopping for aerial long period
It stays；
4, using hand held, perhaps fixed A seating both of which promptly can be charged or be passed through in this way laser of the present invention
Rotary fixing base carries out tracking mode charging；
5, infrared remote sensing camera is arranged in bottom of the present invention, since the application is mainly used for fixed area flight, can carry out ground
Shape monitoring participates in the work such as meteorological exploration fire alarm；
6, there are a circle flexible rings outside each rotor of the present invention, impact brought by birds collision can be prevented；
7, it is provided with infrared inductor in the middle part of the connected arc end of each rotor of the present invention, when having sensed that object proximity can carry out
Corresponding evacuation；
8, the connected arc end of each rotor of the present invention can be convenient for naked eyes to find and other aircraft in this way using fluoresent coating
Evacuation；
9, the present invention uses hemispherical charging equipment, as long as superlaser carries out quickly close to that can charge to facilitate
Charging；
10, landing gear of the present invention, which can according to need, stretches, and can not influence to fly so as far as possible；
11, the present invention due to will receive in flight course birds influence, be provided with sound equipment, when birds close to release noise into
Row expels.
Detailed description of the invention
Fig. 1 is overall work schematic diagram of the invention；
Fig. 2 is aircraft schematic diagram of the present invention；
Fig. 3 is hand held laser schematic diagram of the present invention；
Wherein, 7 cylinder of the flexible foot pad of 1 laser transmitter projects mouth, 2 laser emitter fuselage, 3 rotating shaft electric motor, 4 fixing seat, 5 fuselage 6
Formula landing 8 propeller of telescopic rod, 9 blade, 10 bird repellent sound equipment, 11 solar panel, 12 pyroscan, 13 satellite, 14 laser hair
15 16 camera of hemispherical laser charger receiver of emitter handle, 17 battery.
Specific embodiment
Present invention is further described in detail with specific embodiment with reference to the accompanying drawing:
The present invention provides cooperation satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment, passes through photovoltaic power generation
It matches with wireless electric laser two ways and charges to unmanned plane, guarantee that unmanned plane stays in the air as navigation intermediary as far as possible,
It can be imaged by remote sensing technology, high definition transmits corresponding signal, and according to the mating corresponding ancillary equipment of real flight conditions.
As an embodiment of the present invention, the present invention provide a kind of cooperation satellite navigation laser charging photovoltaic remote sensing nobody
Aircraft and laser equipment, including remote sensing unmanned vehicle and laser, GPS navigation chip built in the remote sensing unmanned vehicle
Position remote sensing is carried out with satellite 13, the remote sensing unmanned vehicle includes fuselage 5, landing gear, propeller 8, blade 9, solar energy
Solar panel 11, laser charger receiver 15 and battery 17,5 main body of fuselage be equilateral triangle, the three of the fuselage 5
A endpoint respectively has a propeller 8, is arc section on the outside of each rotor connected component, the blade 9 is mounted on propeller 8
In shaft, it is equipped with solar panel 11 on the fuselage 5, there is battery 17 below the fuselage 5, the three of the fuselage 5
Respectively there is a landing gear below a side, the hemispherical laser charger receiver 15 is fixedly mounted on 5 bottom of fuselage, described
Hemispherical laser charger receiver 15 has 3 angularly around the center line of fuselage 5 one week, and the laser includes Laser emission
Device emission port 1 and laser emitter fuselage 2, there is laser transmitter projects mouth 1 in 2 end of laser emitter fuselage, described to swash
Light device is hand held laser or pedestal rotary laser device, there is 2 bottom of laser emitter fuselage in the hand held laser
Laser emitter handle 4, rotating shaft electric motor 3, the shaft are arranged at 2 bottom of laser emitter fuselage in the pedestal rotary laser device
Motor 3 is mounted in fixing seat 4.
As a kind of specific embodiment of the present invention, the present invention, which provides a kind of cooperation satellite navigation as shown in Figs. 1-3 and uses, to be swashed
Light charges photovoltaic remote sensing unmanned vehicle and laser equipment, including remote sensing unmanned vehicle and laser, the remote sensing nobody fly
GPS navigation chip built in row device and satellite 13 carry out position remote sensing, and the remote sensing unmanned vehicle includes fuselage 5, landing gear, spiral shell
Paddle 8, blade 9, solar panel 11, laser charger receiver 15 and battery 17 are revolved, 5 main body of fuselage is equilateral three
Angular, three endpoints of the fuselage 5 respectively have a propeller 8, there is a circle flexible protection ring, this hair on the outside of each propeller 8
Have a circle flexible rings outside bright each rotor, can prevent birds collision brought by impact, three sides of the fuselage 5 it is upper
Side is respectively equipped with a bird repellent sound equipment 10, and the present invention is influenced due to will receive birds in flight course, is provided with sound equipment, when
Birds are expelled close to noise is released, and are arc section on the outside of each rotor connected component, outside each rotor connected component
There is pyroscan 12 in the middle part of the arc section of side, is provided with infrared induction in the middle part of the connected arc end of each rotor of the present invention
Device, when having sensed that object proximity can be avoided accordingly, the blade 9 is mounted in the shaft of propeller 8, the machine
It is equipped with solar panel 11 on body 5, has battery 17 below the fuselage 5, there is camera shooting in lower section in the middle part of 5 main body of fuselage
First 16, the camera 16 is infrared remote sensing camera, since the application is mainly used for fixed area flight, can carry out landform
Monitoring participates in the work such as meteorological exploration fire alarm, respectively has a landing gear, the drop below three sides of the fuselage 5
Falling frame is that telescopic landing gear includes two air-cylinder types landing telescopic rods 7, each air-cylinder type landing flexible foot in 7 bottom end of telescopic rod
Pad 6, landing gear, which can according to need, to be stretched, and can not influence to fly so as far as possible, and flexible foot pad, which is arranged, can reduce drop
It falls to damage brought by internal part, the hemispherical laser charger receiver 15 is fixedly mounted on 5 bottom of fuselage, described
Hemispherical laser charger receiver 15 has 3 angularly around the center line of fuselage 5 one week, and the laser includes Laser emission
Device emission port 1 and laser emitter fuselage 2, there is laser transmitter projects mouth 1 in 2 end of laser emitter fuselage, described to swash
Light device is hand held laser or pedestal rotary laser device, there is 2 bottom of laser emitter fuselage in the hand held laser
Laser emitter handle 4, rotating shaft electric motor 3, the shaft are arranged at 2 bottom of laser emitter fuselage in the pedestal rotary laser device
Motor 3 is mounted in fixing seat 4.
The above described is only a preferred embodiment of the present invention, being not the limit for making any other form to the present invention
System, and made any modification or equivalent variations according to the technical essence of the invention, still fall within present invention model claimed
It encloses.
Claims (7)
1. satellite navigation is cooperated to be charged photovoltaic remote sensing unmanned vehicle and laser equipment with laser, including remote sensing unmanned vehicle and
Laser, GPS navigation chip built in the remote sensing unmanned vehicle and satellite (13) carry out position remote sensing, which is characterized in that institute
Stating remote sensing unmanned vehicle includes that fuselage (5), landing gear, propeller (8), blade (9), solar panel (11), laser fill
Electric appliance receiver (15) and battery (17), fuselage (5) main body are equilateral triangle, three endpoints of the fuselage (5)
Respectively there is a propeller (8), is arc section on the outside of each rotor connected component, the blade (9) is mounted on propeller (8)
It in shaft, is equipped with solar panel (11) on the fuselage (5), has battery (17), the machine below the fuselage (5)
Respectively there is a landing gear below three sides of body (5), the hemispherical laser charger receiver (15) is fixedly mounted on machine
Body (5) bottom, the hemispherical laser charger receiver (15) have 3 angularly around center line one week of fuselage (5), it is described
Laser includes laser transmitter projects mouth (1) and laser emitter fuselage (2), and laser emitter fuselage (2) end has
Laser transmitter projects mouth (1), the laser are hand held laser or pedestal rotary laser device, the hand held laser
There is laser emitter handle (4) laser emitter fuselage (2) bottom in device, laser emitter in the pedestal rotary laser device
Fuselage (2) bottom has rotating shaft electric motor (3), and the rotating shaft electric motor (3) is mounted on fixing seat (4).
2. cooperation satellite navigation according to claim 1 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: there is camera (16) lower section in the middle part of fuselage (5) main body, the camera (16) is infrared remote sensing camera shooting
Head.
3. cooperation satellite navigation according to claim 1 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: having a circle flexible protection ring on the outside of each propeller (8).
4. cooperation satellite navigation according to claim 1 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: it includes that two air-cylinder types land telescopic rod (7) that the landing gear, which is telescopic landing gear,.
5. cooperation satellite navigation according to claim 4 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: each air-cylinder type landing flexible foot pad in telescopic rod (7) bottom end (6).
6. cooperation satellite navigation according to claim 1 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: having pyroscan (12) in the middle part of arc section on the outside of each rotor connected component.
7. cooperation satellite navigation according to claim 1 laser charging photovoltaic remote sensing unmanned vehicle and laser equipment,
It is characterized by: the top of three sides of the fuselage (5) is respectively equipped with a bird repellent sound equipment (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811207400.4A CN109178312A (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811207400.4A CN109178312A (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109178312A true CN109178312A (en) | 2019-01-11 |
Family
ID=64945549
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811207400.4A Withdrawn CN109178312A (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation laser charging photovoltaic remote sensing unmanned vehicle and laser equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109178312A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109703395A (en) * | 2019-01-22 | 2019-05-03 | 佛山市木记信息技术有限公司 | A kind of primary and secondary unmanned plane operation method and its system |
| CN110435470A (en) * | 2019-08-08 | 2019-11-12 | 西安交通大学 | A kind of the unmanned plane energy supply platform and its operation method of more energy supplying systems |
| CN115241865A (en) * | 2022-09-23 | 2022-10-25 | 中国科学院空天信息创新研究院 | Combined energy power supply circuit applied to aerostat and power supply control method |
-
2018
- 2018-10-17 CN CN201811207400.4A patent/CN109178312A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109703395A (en) * | 2019-01-22 | 2019-05-03 | 佛山市木记信息技术有限公司 | A kind of primary and secondary unmanned plane operation method and its system |
| CN110435470A (en) * | 2019-08-08 | 2019-11-12 | 西安交通大学 | A kind of the unmanned plane energy supply platform and its operation method of more energy supplying systems |
| CN115241865A (en) * | 2022-09-23 | 2022-10-25 | 中国科学院空天信息创新研究院 | Combined energy power supply circuit applied to aerostat and power supply control method |
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Application publication date: 20190111 |