CN110481801A - The device and technology of a kind of automatic conversion energy on aircraft and automatic running - Google Patents
The device and technology of a kind of automatic conversion energy on aircraft and automatic running Download PDFInfo
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- CN110481801A CN110481801A CN201710544681.1A CN201710544681A CN110481801A CN 110481801 A CN110481801 A CN 110481801A CN 201710544681 A CN201710544681 A CN 201710544681A CN 110481801 A CN110481801 A CN 110481801A
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- China
- Prior art keywords
- energy
- battery
- technology
- automatic
- various
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- 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
- H02J7/0013—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries acting upon several batteries simultaneously or sequentially
-
- 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
- H02J7/0068—Battery or charger load switching, e.g. concurrent charging and load supply
-
- 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
-
- 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
- H02J7/36—Arrangements using end-cell switching
-
- 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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention proposes a kind of for various carry-on automatic conversion energy and the device and technology of automatic running.It is characterized in that the device and technology of the carry-on automatic conversion energy and automatic running are by wind, photosynthetic electricity generation system, charge controller, battery, inverter, motor speed control device and driving force motor are sequentially connected in series, the battery is two, is connected in parallel.First using the voltage rating that the converting direct-current power into alternating-current power of battery and boosting are reached to motor, instead of the problem for reaching voltage rating with more battery series connection, a large amount of battery has been saved simultaneously, thus it also has ready conditions and increases a spare circulating storage battery, then wind is utilized, light hybrid power system guarantees that one of electric energy gives battery cycle charging, solve the problems, such as that various aircraft in the prior art need fuel and itself cannot charge, to realize the long-distance flight of various carry-on automatic conversion energy and automatic running.
Description
1. technical field
The present invention relates to the design field of various aircraft, propose it is a kind of for automatic conversion energy on aircraft and from
The device and technology of dynamic operation.
2. background technique
Since the mankind are born, just there is the dream for wishing that oneself can fly as small bird.Then people have started respectively
The trial of kind of flying method is gone up to the sky from initial zither with fair wind and rocket, hot balloon finally to manned fire balloon.Still later with
The progress of science and technology, steam engine, motor, internal combustion engine equal power device come out one after another, and the power resources of balloon obtain
It solves.Then, people have been in full swing to the balloon that can fly --- the research of dirigible.1852, French engineer Ji Fade into
Research is gone.The same year September, Ji Fade have carried out initial test flight and have succeeded.Aerodone test is to the weight for solving manipulation problem
Big contribution.1903 Nian Laite brother's invention aircrafts, realize controllable, dynamic manned for the first time, and the mankind tentatively realize finally
The Beautiful Dream freely circled in the air in the sky.On December 10th, 1910, in the exhibition of Paris, FRA, Rome Leah people graduation
Earliest jet plane is had devised in the Henry of French Ecole De Technologie Superieur.Britain in 1917 succeeds in developing in the world first
Nowadays platform unmanned plane has been widely used among civilian and military for various purposes.The first in the world of nineteen thirty-nine September 14 days
Practical helicopter VS-300 is succeeded in developing by the western Coase of American engineer.After aircraft invention, aircraft has become existing
The bright indispensable delivery vehicle of Valsartan.It changes deeply and affects people's lives.Due to having invented aircraft, the mankind are global
The time of travelling substantially reduces, when 16th century, 1 mankind first time globaetrotting Portuguese Mai Zhelun has totally used 3 years
Between, at the end of the 19th century, Frenchman worldwide travel one week by train also takes 43 day time.And aircraft in 1949 is only used
Just it has orbited the earth within 94 hours one week, to Englishman Pu Sibeite in 1979 with 06 points of supersonic plane 14 hours around ground
Ball has flown one week.Aircraft has also welcome the high speed development stage and aircraft for various purposes has occurred, e.g., seating plane, bomber,
Even there is space shuttle in fighter plane, early warning plane, transporter, unmanned plane etc., and aircraft has become flying for most species now
Row device.Simultaneously as the high speed development of various aircraft also brings energy supply growing tension, while a large amount of exhaust gas simultaneously
Discharge deteriorates ecological environment further, and air environment pollution is on the rise.
However 98% the above are the technologies of fuel oil power plants to have following defects that in existing various aircraft
1. using non-renewable energy resources Aviation Fuel.In the case where petroleum resources are increasingly exhausted, need to find substitution energy
Source, preferably renewable energy；
2. although aeronautical chart, to the very stringent of the exhaust gas measurings of various aircraft, aircraft generally flies in stratosphere
Row, bring pollution are mainly the tail gas that fuel combustion generates, such as carbon dioxide, carbon monoxide, unburned hydrocarbon and particulate matter, nitrogen
Oxide etc..It is more serious to the pollution of atmosphere；
3. the self structure and working principle of aircraft determine that its vibration, noise problem are difficult to solve, this is seriously affected
The work quality and living standard of crewman.
3. summary of the invention
Based on problem above, it is proposed that the device and skill of a kind of automatic conversion energy on aircraft and automatic running
Art is able to solve above-mentioned technical problem.
Present invention aims to overcome that the defect of above-mentioned existing various vehicle technologies, provide one kind can mitigate significantly it is various
The weight of power device on aircraft, reduces the occupied space of power device on various aircraft, reduces the life of various aircraft
Produce cost, and be able to achieve various aircraft long-distance flights carry-on automatic conversion energy and automatic running device and
Technology.
The technical solution adopted to achieve the purpose of the present invention are as follows:
A kind of device and technology for realizing various carry-on automatic conversion energy and automatic running, it is characterised in that should
The device and technology of carry-on automatic conversion energy and automatic running be by wind, light hybrid power system, charge controller,
Battery, inverter, motor speed control device and driving force motor are sequentially connected in series, and the battery is two, and parallel connection is even
It connects.
The device and technology of various carry-on automatic conversion energy and automatic running of the invention, first use will store
The converting direct-current power into alternating-current power of battery and boosting reach the voltage rating of motor, reach instead of with more batteries series connection
To the problem of voltage rating, while a large amount of battery is saved, to mitigate the weight of power device on various aircraft, subtracted
The occupied space of power device, reduces the production cost of various aircraft on small various aircraft, increase by one of thus also having ready conditions
A spare circulating storage battery, then utilizes wind, and light hybrid power system guarantees that one of electric energy gives battery cycle charging, solves
The problem that various aircraft in the prior art of having determined need fuel and itself cannot charge, to realize on various aircraft
Automatic conversion energy and automatic running long-distance flight.
The device and technology of various carry-on automatic conversion energy and automatic running of the invention are replaced with battery
Fuel flight, and the renewable sources of energy are made full use of, environmental pollution is significantly reduced, has saved the energy, and pollution-free, it is noiseless,
It cleans tasteless, there is high Social benefit and economic benefit.
The device and technology of various carry-on automatic conversion energy and automatic running of the invention can be made into different rule
Lattice number is mounted on the various flights of the other kinds purposes such as dirigible, fire balloon, helicopter, various civil aircrafts, military aircraft
On device.
4. Detailed description of the invention
The exemplary embodiment that the present invention will be described in more detail by referring to accompanying drawing, the above and other aspect of the invention and
Advantage will become more easily clear, in the accompanying drawings:
Fig. 1: for various carry-on automatic conversion energy of the invention and the device of automatic running and the principle of technology
Structural schematic diagram；
5. specific embodiment
Hereinafter, now with reference to attached drawing, the present invention is more fully described, and various embodiments are shown in the attached drawings.So
And the present invention can be implemented in many different forms, and should not be construed as limited to embodiment set forth herein.Phase
Instead, it theses embodiments are provided so that the disclosure will be thorough and complete, and fully conveys the scope of the present invention to ability
Field technique personnel.
Hereinafter, the exemplary embodiment that the present invention will be described in more detail with reference to the accompanying drawings.
In conjunction with shown in attached drawing 1, various carry-on automatic conversion energy of the invention and automatic running be by wind,
Light hybrid power system 1, charge controller 2, battery 3, inverter 4, motor speed control device 5 and driving force motor 6, it is various fly
Row device driving 7 is sequentially connected in series.The battery 3 is two, is connected in parallel.The wind, light hybrid power system 1 one
A electricity generation system filled by Wind turbines and silicon solar cell board group.
Wind, one of electric energy in light hybrid power system 1 are distributed concrete principle by charge controller 2 as shown in Figure 1:
It charges to some battery 3 therein, another battery 3 works at this time, i.e., the electric energy of the battery 3 is converted through inverter 4
At alternating current and the operating voltage of motor is boosted to, driving force motor 6 is finally controlled by motor speed control device 5 and drives various fly
Row device 7.
By by wind, light hybrid power system, charge controller, battery, inverter, motor speed control device and power
Motor is sequentially connected in series, and the battery is two, is connected in parallel.This technology, which uses, converts the direct current of battery
At alternating current and the voltage rating of motor is boosted to, while increasing by a standby battery, then utilizes wind, light mixed power generation system
Blanket insurance demonstrate,proves one of electric energy and gives battery cycle charging；Solving various aircraft in the prior art must be by addition fuel
With the fly able problem of external charge, it is not necessarily to refuel with external charge automatic conversion energy simultaneously to realize various aircraft
Automatic running long-distance flight, various carry-on automatic conversion energy of the invention and automatic running and technology are to store
Battery flies instead of fuel, and makes full use of the renewable sources of energy, significantly reduces environmental pollution, has saved the energy, and pollution-free,
Noiseless, cleaning is tasteless, there is high Social benefit and economic benefit.The various carry-on automatic conversion energy and from
The device and technology of dynamic operation are multiple renewable energy sources mixed power generation, are one of following renewable sources of energy or a variety of: wind energy,
Luminous energy waits other renewable energy.The renewable sources of energy are converted to electric energy, by unique battery parallel technology, instead of falling
The method that series connection battery afterwards promotes voltage.By the inverter of unique technology, the direct current of battery is directly changed into
The alternating current that motor operation needs, realizes the renewable energy such as wind energy, luminous energy and is converted into AC energy, and then can be direct
Drive various aircraft.It, will be inverse by various carry-on automatic conversion energy and the device and technological system of automatic running
The alternating current for becoming device inversion and coming is supplied to motor speed control device, and according to the driving needs of various aircraft users, control is each
Kind carry-on power motor, directly drives various aircraft, realizes that various aircraft are not needing addition fuel and external
In the case where charging, allow various aircraft being capable of automatic conversion energy and the continuous long-distance flight of automatic running.
The above description is only an embodiment of the present invention, is not intended to restrict the invention.The present invention can have various conjunctions
Suitable change and variation.Any modification, equivalent substitution, improvement and etc. done within the spirit and principles of the present invention, should all
It is included within protection scope of the present invention.
Claims (6)
1. the device and technology of a kind of automatic conversion energy on various aircraft and automatic running,
It is characterized by:
The present invention relates to various carry-on automatic conversion energy and the devices and technology of automatic running, this is carry-on certainly
The device and technology of turn transducing amount and automatic running are by wind, light hybrid power system, charge controller, battery, inversion
Device, motor speed control device and driving force motor are sequentially connected in series, and the battery is two, are connected in parallel.This technology is adopted
With by the converting direct-current power into alternating-current power of battery and boosting to the voltage rating of motor, while increasing by a standby battery,
Then guarantee one of electric energy to the form of expression of battery cycle charging using wind, light hybrid power system；
Solving various aircraft in the prior art must be by addition fuel and the fly able problem of charging, to realize
Aircraft is not necessarily to add automatic conversion energy and the automatic running long-distance flight of fuel and external charge.
The device and technology of various carry-on automatic conversion energy and automatic running of the invention replace fuel with battery
Flight, and the renewable sources of energy are made full use of, environmental pollution is significantly reduced, has saved the energy, and pollution-free, noiseless, cleaning
It is tasteless, there is high Social benefit and economic benefit.
2. the method as described in claim 1, it is characterised in that:
The device and technology of the various carry-on automatic conversion energy and automatic running mix for multiple renewable energy sources
The various carry-on automatic conversion energy of power generation and the device and technology of automatic running.
3. method according to claim 1 or 2, it is characterised in that:
The multiple renewable energy sources are one of following renewable sources of energy or a variety of: wind energy, other renewable energies such as luminous energy
Source.
4. method as claimed in claim 3, it is characterised in that:
The renewable sources of energy are converted to electric energy, by unique battery parallel technology, are promoted instead of backward series connection battery
The method of voltage.
5. method as claimed in claim 4, it is characterised in that:
By the inverter of unique technology, the direct current of battery is directly changed into the alternating current of motor operation needs, it is real
The renewable energy such as wind energy, luminous energy are showed and have been converted into AC energy, and then aircraft can be directly driven.
6. method as claimed in claim 5, it is characterised in that:
By various carry-on automatic conversion energy and the device and technological system of automatic running, by inverter inversion
Alternating current be supplied to motor speed control device, according to the driving needs of various aircraft users, control various carry-on
Power motor, directly drive various aircraft in the case where not needing refuelling and external charge, allow various aircraft energy
Enough automatic conversion energy and the continuous long-distance flight of automatic running.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710544681.1A CN110481801A (en) | 2017-07-04 | 2017-07-04 | The device and technology of a kind of automatic conversion energy on aircraft and automatic running |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710544681.1A CN110481801A (en) | 2017-07-04 | 2017-07-04 | The device and technology of a kind of automatic conversion energy on aircraft and automatic running |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110481801A true CN110481801A (en) | 2019-11-22 |
Family
ID=68542961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710544681.1A Pending CN110481801A (en) | 2017-07-04 | 2017-07-04 | The device and technology of a kind of automatic conversion energy on aircraft and automatic running |
Country Status (1)
| Country | Link |
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| CN (1) | CN110481801A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112946477A (en) * | 2021-02-04 | 2021-06-11 | 深圳市蜉飞科技有限公司 | Method, device, equipment and medium for determining remaining battery power of unmanned aerial vehicle device |
| CN113815873A (en) * | 2021-10-09 | 2021-12-21 | 中国人民解放军国防科技大学 | A method and system for optimizing the trajectory of an electric aircraft |
-
2017
- 2017-07-04 CN CN201710544681.1A patent/CN110481801A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112946477A (en) * | 2021-02-04 | 2021-06-11 | 深圳市蜉飞科技有限公司 | Method, device, equipment and medium for determining remaining battery power of unmanned aerial vehicle device |
| CN112946477B (en) * | 2021-02-04 | 2022-03-08 | 深圳市蜉飞科技有限公司 | Method, device, equipment and medium for determining remaining battery power of unmanned aerial vehicle device |
| CN113815873A (en) * | 2021-10-09 | 2021-12-21 | 中国人民解放军国防科技大学 | A method and system for optimizing the trajectory of an electric aircraft |
| CN113815873B (en) * | 2021-10-09 | 2023-07-14 | 中国人民解放军国防科技大学 | A trajectory optimization method and system for an electric aircraft |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20191122 |
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| WD01 | Invention patent application deemed withdrawn after publication |