CN205945201U - Unmanned aerial vehicle's solar charging system - Google Patents
Unmanned aerial vehicle's solar charging system Download PDFInfo
- Publication number
- CN205945201U CN205945201U CN201620776920.7U CN201620776920U CN205945201U CN 205945201 U CN205945201 U CN 205945201U CN 201620776920 U CN201620776920 U CN 201620776920U CN 205945201 U CN205945201 U CN 205945201U
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- CN
- China
- Prior art keywords
- manostat
- intelligent controller
- lithium battery
- unmanned plane
- electricity
- 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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- 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
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- Photovoltaic Devices (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle's solar charging system, include: lithium cell, intelligent control ware, solar cell panel, photovoltaic controller and stabiliser, lithium battery output end with the intelligent control ware is connected, solar cell panel pass through photovoltaic controller with the stabiliser is connected, the output of stabiliser with the intelligent control ware is connected, its duration that can strengthen unmanned aerial vehicle.
Description
Technical field
This utility model is related to a kind of solar recharging system of unmanned plane, belongs to unmanned air vehicle technique field.
Background technology
Existing unmanned plane mainly relies on its lithium battery carrying to be powered, but the electricity that lithium battery carries has
Effect, it is difficult to provide enough electricity for the flying for long time of unmanned plane, thus have impact on the endurance of unmanned plane, unmanned plane
Task cannot be executed for a long time.Maked a return voyage using unmanned plane in prior art, take off lithium battery and the mode of connection adaptor is carried out
Charge, this greatly reduces the work efficiency of unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of solar recharging system of unmanned plane, and it can strengthen the continuous of unmanned plane
Boat ability.
To achieve these goals, the technical solution adopted in the utility model：
The solar recharging system of unmanned plane, 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 and institute
State manostat to connect, the outfan of manostat is connected with described intelligent controller.
In the middle of one or more embodiments of the present utility model, when the voltage of manostat output is higher than lithium battery output
During voltage, 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 present utility model, electricity and manostat that intelligent controller exports lithium battery
The electricity of output exports after mixing according to a certain percentage more outward.
In the middle of one or more embodiments of the present utility model, intelligent controller detects the conversion ratio of manostat, intelligence
The ratio of the electricity that controller automatically adjusts lithium battery according to detected conversion ratio and manostat each exports.
In the middle of one or more embodiments of the present utility model, the outfan of described intelligent controller is that electricity adjusts power supply.
This utility model produced beneficial effect compared with background technology：
A confession assisting can be provided by arranging solar panel, photovoltaic controller and manostat with this for unmanned plane
Electricity, thus strengthen the endurance of unmanned plane.And due to using solar energy, its green, environmental protection, meet existing society
Developing trend.
Brief description
Fig. 1 is the schematic diagram of the solar recharging system of unmanned plane in embodiment.
Specific embodiment
Embodiment of the present utility model is described below in detail, described embodiment example is shown in the drawings, wherein ad initio
To the element that same or similar label represents same or similar element or has same or like function eventually.
In description of the present utility model, it should be noted that for the noun of locality, if any term " " center ", " horizontal ",
" longitudinal ", " length ", " width ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertical ", " level ", " top ",
The indicating position such as " bottom ", " 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 and describe this utility model and simplify description, rather than instruction or the device or the element that imply indication
Must have specific orientation, be constructed with particular orientation and operate it is impossible to be interpreted as limiting concrete protection model of the present utility model
Enclose.
Additionally, being only used for describing purpose if any term " first ", " second ", and it is not intended that instruction or hint are relatively heavy
The property wanted or the implicit quantity indicating technical characteristic.Thus, define " first ", " second " feature can be expressed or implicit inclusion
One or more this feature, in this utility model description, " at least " is meant that one or more, unless otherwise bright
Really specifically limit.
In this utility model, except as otherwise clear stipulaties and restriction, if any term " assembling ", " being connected ", " connection " term
Should go to understand as broad sense, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；It can also be machine
Tool connects；Can be to be joined directly together or be connected by intermediary, can be that two element internals are connected.For
For those of ordinary skill in the art, above-mentioned term specifically containing in this utility model can be understood as the case may be
Justice.
In utility model, unless otherwise prescribed and limit, fisrt feature second feature it " on " or D score permissible
Including the first and second feature directly contacts it is also possible to inclusion fisrt feature and second feature are not directly contact but pass through it
Between other characterisation contact.And, fisrt feature includes fisrt feature in second feature " on ", " under " and " above "
Directly over second feature and oblique upper, or it is only to represent that fisrt feature level height is higher than the height of second feature.First
Feature includes fisrt feature immediately below second feature or obliquely downward in second feature " on ", " under " and " below ", or only
Only represent that fisrt feature level height is less than second feature.
With reference to the accompanying drawing of description, by being further described to specific embodiment of the present utility model, make
The technical solution of the utility model and its advantage are clearer, clear and definite.It is to show below with reference to Description of Drawings embodiment
Example property it is intended to explain this utility model, and it is not intended that to restriction of the present utility model.
Refer to shown in Fig. 1, this utility model provides a kind of solar recharging system of unmanned plane, including：Lithium battery,
Intelligent controller, solar panel, photovoltaic controller and manostat, the outfan of lithium battery is with described intelligent controller even
Connect, solar panel is connected with described manostat by photovoltaic controller, the outfan of manostat and described intelligent controller
Connect, the outfan of described intelligent controller is that electricity adjusts power supply, and described electricity calls the rotating speed output in controlled motor.Wherein photovoltaic
Controller is used for converting thermal energy into electric energy, and the voltage swing of lithium battery output does not limit.
Due to the impact of external environment, the conversion ratio of manostat can difference, Based Intelligent Control therefore of the present utility model
Utensil has multiple functions, wherein：
1st, the conversion ratio of manostat is higher, and when the voltage that the voltage of manostat output is higher than lithium battery output, intelligence is controlled
The voltage that device processed exports manostat is adjusted to equal with the voltage of lithium battery output.
2nd, the conversion ratio of manostat is higher general, and the electricity that the electricity that intelligent controller exports lithium battery is exported with manostat is pressed
Certain ratio exports after mixing outward again, and this ratio freely sets according to practical situation.
3rd, intelligent controller also can detect the conversion ratio of manostat, that is, currently arrives by the electric energy that manostat is converted back
Bottom can export how much electric power, and it is each defeated with manostat that intelligent controller automatically adjusts lithium battery according to detected conversion ratio
The ratio of the electricity going out, finally makes intelligent controller can be stably that electricity adjusts power supply.
In the description of description, reference term " unification an embodiment ", " preferably ", " example ", " specific example " or
The description of " some examples " etc. means specific features, structure, material or the feature describing with reference to this embodiment or example, comprises
In at least one embodiment of the present utility model or example, the schematic representation for above-mentioned term differs in this manual
Surely identical embodiment or example are referred to.And, the specific features of description, structure, material or feature can be any
Combine in a suitable manner in one or more embodiments or example.
By the description of above-mentioned structure and principle, person of ordinary skill in the field should be appreciated that this utility model
It is not limited to above-mentioned specific embodiment, adopt the improvement of techniques well known on the basis of this utility model and substitute all
Fall in protection domain of the present utility model, it should be limited by each claim.
Claims (5)
1. the solar recharging system of unmanned plane is it is characterised in that include：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.
2. unmanned plane according to claim 1 solar recharging system it is characterised in that：Voltage when manostat output
Higher than lithium battery output voltage when, the voltage that intelligent controller exports manostat be adjusted to lithium battery output voltage phase
Deng.
3. unmanned plane according to claim 1 solar recharging system it is characterised in that：Intelligent controller is lithium battery
The electricity that the electricity of output is exported with manostat exports after mixing according to a certain percentage more outward.
4. unmanned plane according to claim 1 solar recharging system it is characterised in that：Intelligent controller detects voltage stabilizing
The conversion ratio of device, intelligent controller automatically adjusts, according to detected conversion ratio, the electricity that lithium battery is each exported with manostat
Ratio.
5. the unmanned plane according to claim 1 or 2 or 3 or 4 solar recharging system it is characterised in that：Also include
For the electricity tune of the rotating speed output of controlled motor, the outfan of described intelligent controller is that electricity adjusts power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620776920.7U CN205945201U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle's solar charging system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620776920.7U CN205945201U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle's solar charging system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205945201U true CN205945201U (en) | 2017-02-08 |
Family
ID=57926688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620776920.7U Expired - Fee Related CN205945201U (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle's solar charging system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205945201U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106026344A (en) * | 2016-07-22 | 2016-10-12 | 珠海银通农业科技有限公司 | UAV solar charging system |
-
2016
- 2016-07-22 CN CN201620776920.7U patent/CN205945201U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106026344A (en) * | 2016-07-22 | 2016-10-12 | 珠海银通农业科技有限公司 | UAV solar charging system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 519055 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Patentee after: Zhuhai JETCO UAV Technology Co. Ltd. Address before: 519055 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Patentee before: ZHUHAI YINTONG AGRICULTURAL SCIENCE AND TECHNOLOGY CO., LTD. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170208 Termination date: 20200722 |