CN106026344A - UAV solar charging system - Google Patents
UAV solar charging system Download PDFInfo
- Publication number
- CN106026344A CN106026344A CN201610581775.1A CN201610581775A CN106026344A CN 106026344 A CN106026344 A CN 106026344A CN 201610581775 A CN201610581775 A CN 201610581775A CN 106026344 A CN106026344 A CN 106026344A
- Authority
- CN
- China
- Prior art keywords
- manostat
- lithium battery
- intelligent controller
- unmanned plane
- controller
- 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
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 24
- 230000005611 electricity Effects 0.000 claims description 15
- 238000006243 chemical reaction Methods 0.000 claims description 9
- 238000001514 detection method Methods 0.000 claims description 2
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 239000003381 stabilizer Substances 0.000 abstract 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012512 characterization method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Classifications
-
- 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
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
- Y02E10/56—Power conversion systems, e.g. maximum power point trackers
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a UAV solar charging system, which comprises a lithium battery, an intelligent controller, a solar cell panel, a photovoltaic controller and a voltage stabilizer, wherein an output end of the lithium battery is connected with the intelligent controller, the solar cell panel is connected with the voltage stabilizer through the photovoltaic controller, and an output end of the voltage stabilizer is connected with the intelligent controller. The UAV solar charging system can enhance the battery life of an unmanned aerial vehicle (UAV).
Description
Technical field
The present invention relates to the solar recharging system of a kind of unmanned plane, belong to unmanned air vehicle technique field.
Background technology
Existing unmanned plane mainly relies on its lithium battery carried to be powered, but the electricity that lithium battery carries has
Effect, it is difficult to for the electricity that the flying for long time offer of unmanned plane is enough, thus have impact on the flying power of unmanned plane, unmanned plane
Task cannot be performed for a long time.Using unmanned plane to make a return voyage in prior art, the mode taking off lithium battery connection adaptor is carried out
Charging, this greatly reduces the work efficiency of unmanned plane.
Summary of the invention
It is an object of the invention to provide the solar recharging system of a kind of unmanned plane, it can strengthen the continuation of the journey energy of unmanned plane
Power.
To achieve these goals, the technical solution used in the present invention: the solar recharging system of unmanned plane, including: lithium
Battery, intelligent controller, solar panel, photovoltaic controller and manostat, the outfan of lithium battery and described intelligence control
Device processed connects, and solar panel is connected with described manostat by photovoltaic controller, the outfan of manostat and described intelligence
Controller connects.
In the middle of one or more embodiments of the invention, when the voltage that the voltage of manostat output exports higher than lithium battery
Time, the voltage that intelligent controller exports manostat is adjusted to equal with the voltage of lithium battery output.
In the middle of one or more embodiments of the invention, the electricity that intelligent controller exports lithium battery exports with manostat
Electricity mix according to a certain percentage after export the most outward.
In the middle of one or more embodiments of the invention, the conversion ratio of intelligent controller detection manostat, Based Intelligent Control
Device is automatically adjusted the ratio of the electricity that lithium battery each exports with manostat according to detected conversion ratio.
In the middle of one or more embodiments of the invention, the outfan of described intelligent controller is for controlling motor
The electricity of rotating speed output adjusts power supply.
The present invention is produced beneficial effect compared with background technology:
Can be the power supply that unmanned plane provides an auxiliary by arranging solar panel, photovoltaic controller and manostat with this,
Thus strengthen the flying power of unmanned plane.And owing to using solar energy, it is green, environmental protection, meets sending out of existing society
Exhibition tends to.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the solar recharging system of unmanned plane in embodiment.
Detailed description of the invention
Embodiments of the invention are described below in detail, and described embodiment example is shown in the drawings, the most from start to finish
Same or similar label represents same or similar element or has the element of same or like function.
In describing the invention, it should be noted that for the noun of locality, if any term " " center ", " laterally ", " vertical
To ", " length ", " width ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ",
The indicating position such as " end ", " interior ", " outward ", " clockwise ", " counterclockwise " and position relationship are based on orientation shown in the drawings or position
Put relation, be for only for ease of the narration present invention and simplification description rather than instruction or the device of hint indication or element is necessary
There is specific orientation, with particular orientation structure and operation, it is impossible to be interpreted as limiting the concrete protection domain of the present invention.
Additionally, be only used for describing purpose if any term " first ", " second ", and it is not intended that indicate or imply relatively heavy
The property wanted or the implicit quantity indicating technical characteristic.Thus, define " first ", " second " feature can be expressed or imply and include
One or more this feature, in the present description, " at least " is meant that one or more, unless otherwise clearly having
The restriction of body.
In the present invention, except as otherwise clear stipulaties and restriction, " assemble " if any term, " being connected ", " connection " term should be made
Broad sense goes to understand, connects for example, it may be fixing, it is also possible to be to removably connect, or be integrally connected；Can also be that machinery connects
Connect；Can be to be joined directly together, it is also possible to be to be connected by intermediary, can be that two element internals are connected.For ability
For the those of ordinary skill of territory, above-mentioned term concrete meaning in the present invention can be understood as the case may be.
In invention, unless otherwise prescribed and limit, fisrt feature second feature it " on " or D score can include
First and second features directly contact, it is also possible to include that fisrt feature is not directly to contact with second feature but by they it
Between other characterisation contact.And, fisrt feature second feature " on ", " under " and " above " include that fisrt feature is
Directly over two features and oblique upper, or be only the height representing fisrt feature level height higher than second feature.Fisrt feature
Second feature " on ", " under " and " below " include fisrt feature immediately below second feature or obliquely downward, or only table
Show that fisrt feature level height is less than second feature.
Below in conjunction with the accompanying drawing of description, by the detailed description of the invention of the present invention is further described, make this
Bright technical scheme and beneficial effect thereof are clearer, clear and definite.It is exemplary for describing embodiment below with reference to accompanying drawing, purport
Explaining the present invention, and be not considered as limiting the invention.
Refer to shown in Fig. 1, the present invention provides the solar recharging system of a kind of unmanned plane, including: lithium battery, intelligence
Controller, solar panel, photovoltaic controller and manostat, the outfan of lithium battery is connected with described intelligent controller,
Solar panel is connected with described manostat by photovoltaic controller, and the outfan of manostat is with described intelligent controller even
Connecing, the outfan of described intelligent controller is the electricity tune power supply for controlling the output of the rotating speed of motor.Wherein photovoltaic controller is used
In converting thermal energy into electric energy, the voltage swing of lithium battery output does not limits.
Due to the impact of external environment, the conversion ratio of manostat can difference, therefore the Based Intelligent Control utensil of the present invention
There is multiple function, wherein:
1, the conversion ratio of manostat is higher, when the voltage that the voltage of manostat output exports higher than lithium battery, and intelligent controller
The voltage of manostat output is adjusted to equal with the voltage of lithium battery output.
2, the conversion ratio of manostat is higher typically, and the electricity that the electricity that intelligent controller exports lithium battery exports with manostat is pressed
Certain ratio exports after mixing the most outward, and this ratio freely sets according to practical situation.
3, intelligent controller also can detect the conversion ratio of manostat, the most currently arrives by the electric energy that manostat is converted back
The end, can export how much electric power, and it is the most defeated with manostat that intelligent controller is automatically adjusted lithium battery according to detected conversion ratio
The ratio of the electricity gone out, finally makes intelligent controller stably can adjust power supply for electricity.
In the description of description, reference term " unification an embodiment ", " preferably ", " example ", " concrete example " or
The description of " some examples " etc. means to combine this embodiment or specific features, structure, material or the feature of example description, comprises
In at least one embodiment or example of the present invention, the schematic representation for above-mentioned term not necessarily refers in this manual
Be identical embodiment or example.And, the specific features of description, structure, material or feature can be at any one
Or multiple embodiment or example combine in a suitable manner.
By above-mentioned structure and the description of principle, person of ordinary skill in the field should be appreciated that the present invention not office
It is limited to above-mentioned detailed description of the invention, uses the improvement of techniques well known and replacement to all fall within this on the basis of the present invention
Bright protection domain, should be limited it by each claim.
Claims (5)
1. the solar recharging system of unmanned plane, it is characterised in that including: lithium battery, intelligent controller, solar panel,
Photovoltaic controller and manostat, the outfan of lithium battery is connected with described intelligent controller, and solar panel passes through photovoltaic
Controller is connected with described manostat, and the outfan of manostat is connected with described intelligent controller.
The solar recharging system of unmanned plane the most according to claim 1, it is characterised in that: when the voltage of manostat output
Higher than lithium battery output voltage time, the voltage that intelligent controller export manostat be adjusted to and lithium battery export voltage phase
Deng.
The solar recharging system of unmanned plane the most according to claim 1, it is characterised in that: intelligent controller is lithium battery
The electricity that the electricity of output and manostat export exports after mixing according to a certain percentage the most outward.
The solar recharging system of unmanned plane the most according to claim 1, it is characterised in that: intelligent controller detection voltage stabilizing
The conversion ratio of device, intelligent controller is automatically adjusted, according to detected conversion ratio, electricity that lithium battery and manostat each export
Ratio.
5. according to the solar recharging system of the unmanned plane described in claim 1 or 2 or 3 or 4, it is characterised in that: described intelligence
The outfan of controller is the electricity tune power supply for controlling the output of the rotating speed of motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610581775.1A CN106026344A (en) | 2016-07-22 | 2016-07-22 | UAV solar charging system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610581775.1A CN106026344A (en) | 2016-07-22 | 2016-07-22 | UAV solar charging system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106026344A true CN106026344A (en) | 2016-10-12 |
Family
ID=57117273
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610581775.1A Pending CN106026344A (en) | 2016-07-22 | 2016-07-22 | UAV solar charging system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106026344A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107707179A (en) * | 2017-10-10 | 2018-02-16 | 浙江聚珖科技股份有限公司 | The photovoltaic temperature difference electricity generation device and its unmanned plane of unmanned plane |
| CN107856860A (en) * | 2017-11-30 | 2018-03-30 | 徐朋 | A kind of solar energy plant protection unmanned plane |
| WO2018094797A1 (en) * | 2016-11-25 | 2018-05-31 | 文锦伟 | Solar quadrotor aircraft |
| ES2673445A1 (en) * | 2016-12-21 | 2018-06-21 | Ismael MONTES RUIZ | STATION FOR UNDERGROUND AERIAL VEHICLES (Machine-translation by Google Translate, not legally binding) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204527624U (en) * | 2015-04-13 | 2015-08-05 | 黄毓琦 | A kind of four-axle aircraft |
| CN104901389A (en) * | 2015-06-23 | 2015-09-09 | 界首市绍恩精机机械有限公司 | Intelligent control system effectively prolonging service lifetime of photovoltaic power generation matched storage battery |
| CN105449822A (en) * | 2015-12-11 | 2016-03-30 | 中国电子科技集团公司第四十八研究所 | Energy system for high-altitude airship and power supply control method |
| CN205945201U (en) * | 2016-07-22 | 2017-02-08 | 珠海银通农业科技有限公司 | Unmanned aerial vehicle's solar charging system |
-
2016
- 2016-07-22 CN CN201610581775.1A patent/CN106026344A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204527624U (en) * | 2015-04-13 | 2015-08-05 | 黄毓琦 | A kind of four-axle aircraft |
| CN104901389A (en) * | 2015-06-23 | 2015-09-09 | 界首市绍恩精机机械有限公司 | Intelligent control system effectively prolonging service lifetime of photovoltaic power generation matched storage battery |
| CN105449822A (en) * | 2015-12-11 | 2016-03-30 | 中国电子科技集团公司第四十八研究所 | Energy system for high-altitude airship and power supply control method |
| CN205945201U (en) * | 2016-07-22 | 2017-02-08 | 珠海银通农业科技有限公司 | Unmanned aerial vehicle's solar charging system |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018094797A1 (en) * | 2016-11-25 | 2018-05-31 | 文锦伟 | Solar quadrotor aircraft |
| ES2673445A1 (en) * | 2016-12-21 | 2018-06-21 | Ismael MONTES RUIZ | STATION FOR UNDERGROUND AERIAL VEHICLES (Machine-translation by Google Translate, not legally binding) |
| CN107707179A (en) * | 2017-10-10 | 2018-02-16 | 浙江聚珖科技股份有限公司 | The photovoltaic temperature difference electricity generation device and its unmanned plane of unmanned plane |
| CN107856860A (en) * | 2017-11-30 | 2018-03-30 | 徐朋 | A kind of solar energy plant protection unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: 519055 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Applicant after: ZHUHAI YINTONG UAV TECHNOLOGY CO.,LTD. Address before: 519055 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Applicant before: ZHUHAI YINTONG AGRICULTURAL SCIENCE AND TECHNOLOGY Co.,Ltd. |
|
| CB02 | Change of applicant information | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161012 |
|
| RJ01 | Rejection of invention patent application after publication |