CN108100268A - It leaves blank flight instruments for a long time - Google Patents
It leaves blank flight instruments for a long time Download PDFInfo
- Publication number
- CN108100268A CN108100268A CN201711319516.2A CN201711319516A CN108100268A CN 108100268 A CN108100268 A CN 108100268A CN 201711319516 A CN201711319516 A CN 201711319516A CN 108100268 A CN108100268 A CN 108100268A
- Authority
- CN
- China
- Prior art keywords
- fuselage cover
- energy
- shell
- storage battery
- wing shell
- 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.)
- Withdrawn
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Classifications
-
- 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
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
- G05D1/0022—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement characterised by the communication link
Abstract
It leaves blank flight instruments the invention discloses a kind of long-time, it includes the ground transmission station being in communication with each other and aerial receiving terminal two parts, aerial receiving terminal includes fuselage cover, wing shell, empennage shell, the wing shell is located at fuselage cover front end, the empennage shell is located at fuselage cover rear end, the fuselage cover afterbody is equipped with propeller, there are one sender units for dress inside the fuselage cover, one controller and a data processor, the sender unit is located at data processor rear, the controller is located at the front of data processor, the wing shell outer layer is equipped with energy-storage battery, overlay film photovoltaic cell, lift fan, the overlay film photovoltaic cell is located at the top of wing shell top and bottom, the energy-storage battery is located on the inside of overlay film photovoltaic cell.The present invention realizes that long-time high-altitude is left blank, and realizes the high quality beam of high-power near-infrared eye-safe, transfers more accurate, low-power.
Description
Technical field
The present invention relates to a kind of flight instruments, leave blank flight instruments more particularly to a kind of long-time.
Background technology
Existing aircraft can not realize that especially high-altitude is left blank for a long time, and have discharge using chemical fuel, cost
The problem of.Aircraft using solar energy as power needs to carry substantial amounts of energy-storage battery, and photovoltaic conversion efficiency, during sunshine
Between, air velocity, the influences such as weather cloud layer are also effectively left blank than long-time relatively difficult to achieve.The speed of Near Earth Orbit Satellites is too fast,
Single satellite can not realize that effectively stablizes leaves blank to realize the functions such as its communication monitoring, and satellite group is high there is also cost, nothing
The problems such as method effectively recycles, space trash.Geostationary orbit can not complete big data then apart from earth surface apart from too far
The functions such as amount transmission and other fine remote sensing monitorings.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of long-time and leave blank flight instruments, realize long-time high-altitude
It leaves blank, realizes the high quality beam of high-power near-infrared eye-safe, transfer more accurate, low-power.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of long-time is left blank flight instruments,
It is characterized in that, it includes the ground transmission station being in communication with each other and aerial receiving terminal two parts, aerial receiving terminal is included outside fuselage
Shell, wing shell, empennage shell, the wing shell is located at fuselage cover front end, after the empennage shell is located at fuselage cover
End, the fuselage cover afterbody are equipped with propeller, inside the fuselage cover dress there are one sender unit, a controller and
One data processor, the sender unit is located at data processor rear, before the controller is located at data processor
Side, the wing shell outer layer are equipped with energy-storage battery, overlay film photovoltaic cell, lift fan, and the overlay film photovoltaic cell is located at machine
The top of wing shell top and bottom, the energy-storage battery are located on the inside of overlay film photovoltaic cell, and the lift fan is located at energy-storage battery
Inside is equipped with a high speed light emitting diode, ground launch between the lift fan and energy-storage battery on one side of the wing shell
Stand including high precision tracking holder and condenser lens, the high precision tracking holder is connected with condenser lens, the high-precision with
Image intensifer and signal processor are equipped in track holder, the image intensifer is connected with signal processor.
Preferably, the energy-storage battery uses gallium arsenide cells.
Preferably, the fuselage cover, all elements on wing shell are all connected by conducting wire.
Preferably, optical fiber laser is equipped in the machine condenser lens.
The positive effect of the present invention is：Remote power, which is provided, using high energy laser realizes that long-time high-altitude is stayed
Sky realizes the high quality beam of high-power near-infrared eye-safe using optical fiber laser, in real time the position of accurate tracking hot spot
With on aircraft receiving terminal, aircraft receiving terminal uses GaAs Efficient Conversion luminous energy that signal of communication is passed through optical fiber for electric energy
Amplifier by carrier wave on energy beam, it is more accurate to transfer, and using LED, realizes that the similar solution of low cost is used for
Closer distance, the application of low-power.
Description of the drawings
Fig. 1 is the bottom view of the present invention.
Fig. 2 is the top view of the present invention.
Fig. 3 is the internal structure schematic diagram of the present invention.
Fig. 4 is the structure diagram of the elements such as signal processor.
Specific embodiment
Present pre-ferred embodiments are provided below in conjunction with the accompanying drawings, with the technical solution that the present invention will be described in detail.
As shown in Figures 1 to 4, present invention flight instruments of leaving blank for a long time includes the ground transmission station that is in communication with each other and aerial
Receiving terminal two parts, aerial receiving terminal include fuselage cover 1, wing shell 2, empennage shell 3, and the wing shell 2 is located at machine
1 front end of body shell, the empennage shell 3 are located at 1 rear end of fuselage cover, and 1 afterbody of fuselage cover is equipped with propeller 8, described
There are one 7, controllers 10 of sender unit and a data processor 11, the signal is sent 1 inside dress of fuselage cover
Device 7 is located at 11 rear of data processor, and the controller 10 is located at the front of data processor 11,2 outer layer of wing shell
Equipped with energy-storage battery 4, overlay film photovoltaic cell 6, lift fan 9, the overlay film photovoltaic cell 6 is located at 2 top and bottom of wing shell
Top, the energy-storage battery 4 are located at 6 inside of overlay film photovoltaic cell, and the lift fan 9 is located at 4 inside of energy-storage battery, the machine
A high speed light emitting diode 5 is equipped between the lift fan 9 on one side of wing shell 2 and energy-storage battery 4, ground transmission station includes height
Precision tracks holder 13 and condenser lens 12, and the high precision tracking holder 13 is connected with condenser lens 12, the high-precision with
Image intensifer 14 and signal processor 15 are equipped in track holder 13, the image intensifer 14 is connected with signal processor 15.
The energy-storage battery 4 uses gallium arsenide cells, and Efficient Conversion luminous energy is electric energy.
All elements on the fuselage cover 1, wing shell 2 are all connected by conducting wire, form complete circuit, convenient
Control and offer electric energy.
Optical fiber laser is equipped in the machine condenser lens 12, realizes the high-quality light of high-power near-infrared eye-safe
Beam.
The confined space formed in fuselage cover, wing shell, empennage shell, energy-storage battery are used to store overlay film photovoltaic electric
The electric energy and provide electric energy that pond is collected, provide remote power and realize that long-time high-altitude is left blank.High speed light emitting diode is used to sense
The optical signal that condenser lens transmits on the high precision tracking holder on ground, propeller provide the forward power of aircraft, lift fan
There is provided aircraft upward power, the opening and closing of all elements, signal processor believe data on controller control aircraft
Number be converted to optical signal, optical signal amplification is sent to the condenser lens on high precision tracking holder by image intensifer again, at data
The optical signal that reason device senses high speed light emitting diode is handled and is sent to controller, and sender unit shines high speed
The information of diode is sent to data processor.
Present embodiment is divided into ground transmission station and aerial receiving terminal two parts.Ground transmission station is swashed using high-energy optical fiber
Light device（100W-10KW）, wavelength 800-1600nm, main available band is that eye-safe and air vapor absorption are relatively low
1060nm, 1550nm or so, especially 1550 wave bands, wavelength is longer, and by cloud layer, courteous particle influences smaller, to people
Eye is safer, while can load the 1550nm high bandwidths optical signal of optical communication above.Optical-fiber laser has light beam
The advantages of energy is high, good beam quality, transmitting aperture is small, formation dispersion angle is minimum after can it be assembled with lens swashs
Light beam can be dissipated hot spot control within 5 square metres, with high-precision vibration isolation piezoelectricity 3D holders in 20 kilometers of distances
Control laser beam angle position can real-time tracking on the photoelectric conversion device of receiving terminal.Receiving terminal uses bloom
Photoelectric transformation efficiency（25-45%）GaAs or indium gallium arsenic photocell film in the bottom of aircraft（Or it is equipped with above-mentioned photovoltaic
The aircraft inverted flight of film）And other electric explorers, by the angle for sending position signal guiding ground laser beam in real time
With position to reach maximal received power.The electric energy of conversion can be directly used in power, Huo Zhecun as the supplement of photovoltaic energy
It is stored in energy-storage battery and is used in airborne equipment.Communication photodetector optical signal receiving can be handled after with microwave or
Optical signal amplifier amplifies with being transmitted to after assembling using end（Ground receiving station, other aircraft, satellite etc.）.Another letter
Single application such as single shaft for monitoring and taking photo by plane and multiaxis unmanned plane can also be realized with this structure leaves blank for a long time, simply emits
It brings out in cost, power and the shorter factor of transmission range demand, it is more using assembling visible rays or near-infrared LED, and
It is not optical fiber laser, receiving terminal is then using matching silicon based opto-electronics pond or gallium arsenide photoelectric pond component, pencil tracing
The relatively low holder of precision can also be used to control in part.
The present invention provides remote power using high energy laser or battery and realizes that long-time high-altitude is left blank, using optical-fiber laser
Device realizes the high quality beam of high-power near-infrared eye-safe, in real time the position of accurate tracking hot spot and aircraft receiving terminal
On, aircraft receiving terminal uses GaAs Efficient Conversion luminous energy as electric energy, by signal of communication by fiber amplifier by carrier wave
On energy beam, it is more accurate to transfer, and using LED, realizes the similar solution of low cost for closer distance, low-power
Application.
Particular embodiments described above, the technical issues of to the solution of the present invention, technical solution and advantageous effect carry out
It is further described, it should be understood that the above is only a specific embodiment of the present invention, is not limited to
The present invention, within the spirit and principles of the invention, any modification, equivalent substitution, improvement and etc. done should be included in this
Within the protection domain of invention.
Claims (4)
- The flight instruments 1. a kind of long-time is left blank, which is characterized in that it includes the ground transmission station being in communication with each other and aerial reception Two parts are held, aerial receiving terminal includes fuselage cover, wing shell, empennage shell, before the wing shell is located at fuselage cover End, the empennage shell are located at fuselage cover rear end, and the fuselage cover afterbody is equipped with propeller, is filled inside the fuselage cover There are one sender unit, a controller and a data processor, the sender unit is located at data processor rear, The controller is located at the front of data processor, and the wing shell outer layer is equipped with energy-storage battery, overlay film photovoltaic cell, lift Fan, the overlay film photovoltaic cell are located at the top of wing shell top and bottom, and the energy-storage battery is located in overlay film photovoltaic cell Side, the lift fan are located on the inside of energy-storage battery, are set between the lift fan and energy-storage battery on one side of the wing shell There is a high speed light emitting diode, ground transmission station includes high precision tracking holder and condenser lens, the high precision tracking holder It is connected with condenser lens, image intensifer and signal processor, the image intensifer and letter is equipped in the high precision tracking holder Number processor is connected.
- 2. flight instruments as described in claim 1 of leaving blank for a long time, which is characterized in that the energy-storage battery is using GaAs electricity Pond.
- 3. flight instruments as described in claim 1 of leaving blank for a long time, which is characterized in that on the fuselage cover, wing shell All elements all connected by conducting wire.
- 4. flight instruments as described in claim 1 of leaving blank for a long time, which is characterized in that optical fiber is equipped in the machine condenser lens Laser.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711319516.2A CN108100268A (en) | 2017-12-12 | 2017-12-12 | It leaves blank flight instruments for a long time |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711319516.2A CN108100268A (en) | 2017-12-12 | 2017-12-12 | It leaves blank flight instruments for a long time |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108100268A true CN108100268A (en) | 2018-06-01 |
Family
ID=62215727
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711319516.2A Withdrawn CN108100268A (en) | 2017-12-12 | 2017-12-12 | It leaves blank flight instruments for a long time |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108100268A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502024A (en) * | 2018-10-19 | 2019-03-22 | 东汉太阳能无人机技术有限公司 | A kind of aircraft and unmanned aerial vehicle |
-
2017
- 2017-12-12 CN CN201711319516.2A patent/CN108100268A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502024A (en) * | 2018-10-19 | 2019-03-22 | 东汉太阳能无人机技术有限公司 | A kind of aircraft and unmanned aerial vehicle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180601 |