CN206384144U - Plant protection unmanned plane based on solar recharging system - Google Patents
Plant protection unmanned plane based on solar recharging system Download PDFInfo
- Publication number
- CN206384144U CN206384144U CN201720049380.7U CN201720049380U CN206384144U CN 206384144 U CN206384144 U CN 206384144U CN 201720049380 U CN201720049380 U CN 201720049380U CN 206384144 U CN206384144 U CN 206384144U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- solar panel
- frame
- plant protection
- solar
- 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.)
- Expired - Fee Related
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Classifications
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- 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
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides a kind of plant protection unmanned plane based on solar recharging system, to solve the power issue of current unmanned plane operationally, ensure that unmanned plane can continue efficient operation, including the frame with rotor, the battery powered for rotor, solar panel with inverter, the solar panel is C-shaped to be bent and is buckled in the frame, and the left and right sides of the both ends of the solar panel respectively with frame direction of advance is fixedly connected, inverter on the solar panel passes sequentially through transformer, charger is electrically connected with the battery.
Description
Technical field
The utility model is related to a kind of unmanned plane, more particularly to a kind of plant protection unmanned plane based on solar recharging system.
Background technology
With the rise of unmanned plane industry, application field is also more and more wider.The form that present unmanned plane provides the energy has
Two kinds：Electric energy, oil are dynamic, wherein the dynamic unmanned plane horsepower foot of oil, but use the dynamic unmanned plane of oil heavy, and life-span of engine is also very
Short, the waste gas discharged during work can be polluted to environment；Therefore electronic unmanned plane has unrivaled advantage.Electronic nothing
Man-machine use battery-powered, the loss to motor is very small, greatly enhances the operating efficiency of unmanned plane.But nobody
The operating environment of machine is that in the air, stability, efficiency are required for taking into account, and the discharge parameter of battery is had higher requirements, at present, though
The research and development of right battery unusual forward position, but it is used in a practical situation or based on lithium battery, and lithium battery is because tool
There is the series of advantages such as energy height, long lifespan, high power endurance, lightweight, become the main flow selection of world today's battery.
Unmanned plane application is high-rate polymer lithium battery, and the continuous discharge electric current of the discharge parameter of the battery is up to 400A or so；
The discharge parameter of superelevation has led to a problem：The working time of battery is shorter, if in the UAS of a set of matching
In, a Battery pack working time is 5-30 minutes, but the charge rate of battery is very slow (relative to discharge time),
One piece of battery is fully charged at 40-120 minutes, is needed at work which results in unmanned plane while preparing many Battery packs
Used to supply a unmanned plane, waste many resources.Present invention seek to address that the power issue of unmanned plane operationally, is protected
Card unmanned plane can continue efficient operation.
The content of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, adapts to real needs and be based on the sun there is provided one kind
The plant protection unmanned plane of energy charging system, to solve the power issue of current unmanned plane operationally, it is ensured that unmanned plane can continue
Efficient operation.
In order to realize the purpose of this utility model, the technical scheme that the utility model is used for：
A kind of plant protection unmanned plane based on solar recharging system of design, including the frame with rotor, power for rotor
Battery, the solar panel with inverter, C-shaped bend of the solar panel be simultaneously buckled in the frame,
And the left and right sides of the both ends of the solar panel respectively with frame direction of advance is fixedly connected, the solar cell
Inverter on plate passes sequentially through transformer, charger and is electrically connected with the battery.
It is preferred that, it is triangular in shape provided with section on the crooked end of the solar panel in the frame direction of advance
Wind deflector, the wind deflector is buckled on the end of sweeping solar panel.
It is preferred that, with being also provided with described on the end of the solar panel in the reverse direction of the frame direction of advance
Wind deflector.
It is preferred that, the battery, transformer and charger are respectively positioned in the frame below the solar panel.
The beneficial effects of the utility model are：
It is the design its novel in structural design, simple, relative to plant protection unmanned plane of the prior art, in its continuation of the journey of the design
Cheng Gengyuan, it is more efficient, it can be good at being adapted in the crop operations of large area, and produce to improving operating efficiency, reducing
Cost has important effect.
Brief description of the drawings
Fig. 1 is primary structure schematic front view of the present utility model；
Fig. 2 is the solar panel in the utility model and wind deflector structure schematic diagram thereon；
Fig. 3 is the solar panel in the utility model and wind deflector cross section structure schematic diagram thereon；
Fig. 4 is the solar panel and the electric connection principle schematic of battery in the utility model；
In figure：1. frame；2. solar panel；3. battery；4. charger；5. transformer；6. wind deflector.
Embodiment
The utility model is further illustrated with reference to the accompanying drawings and examples：
Embodiment 1：A kind of plant protection unmanned plane based on solar recharging system, referring to Fig. 1 to Fig. 4；It includes having rotation
The frame 1 of the wing, battery 3, the solar panel 2 with inverter powered for rotor, the design is, above-described
Solar panel 2 it is C-shaped bend simultaneously be buckled in the frame 1, and the solar panel 2 both ends respectively with frame
The left and right sides of direction of advance is fixedly connected, because in view of having digital transmission module at the top of unmanned plane, in order to avoid there is electrostatic sheild
The situation covered, therefore the design uses curved solar energy cell panel, rather than sphere solar panel, furthermore, curved surface is too
Positive energy cell panel also has certain effect to reduction windage；By this design, by the installation direction of solar panel perpendicular to
The direction of head --- tail is installed and can be preferably minimized the resistance of wind, further, as shown in figure 3, the design can also be in institute
The crooked end for the solar panel 2 in the direction of advance of frame 1 stated is described provided with section wind deflector 6 triangular in shape
Wind deflector 6 is buckled on the end of sweeping solar panel, likewise, the design with the frame direction of advance
Described wind deflector can also be set on the end of solar panel in the reverse direction.
And the inverter on above-described solar panel 2 passes sequentially through transformer 4, charger 5 and the electric power storage
Pond 4 is electrically connected with, meanwhile, described battery, transformer and charger is respectively positioned on the frame below the solar panel
On, designed by this, solar panel 2 can provide for battery, transformer and charger and block and protect, help to prolong
The service life of long three.
The unmanned plane of the design is in operation because its carrying is fixed on the curved solar energy cell panel at the top of unmanned plane, and this is too
Positive energy cell panel is sustainable to generate electricity and is inputted after transformer into charger, finally the battery by charger to unmanned plane
Charging, can increase the course continuation mileage of unmanned plane by this mode.
What embodiment of the present utility model was announced is preferred embodiment, but is not limited thereto, the common skill of this area
Art personnel, easily according to above-described embodiment, understand spirit of the present utility model, and make different amplifications and change, but as long as
Spirit of the present utility model is not departed from, all in protection domain of the present utility model.
Claims (4)
1. a kind of plant protection unmanned plane based on solar recharging system, including the frame with rotor, the electric power storage powered for rotor
Pond, the solar panel with inverter, it is characterised in that：The solar panel is C-shaped to be bent and is buckled in the machine
On frame, and the left and right sides of the both ends respectively with frame direction of advance of the solar panel is fixedly connected, the sun
Inverter on energy cell panel passes sequentially through transformer, charger and is electrically connected with the battery.
2. the plant protection unmanned plane as claimed in claim 1 based on solar recharging system, it is characterised in that：Before the frame
The crooked end of the solar panel entered on direction is buckled in curved provided with section wind deflector triangular in shape, the wind deflector
On the end of curved solar panel.
3. the plant protection unmanned plane as claimed in claim 2 based on solar recharging system, it is characterised in that：With the frame
Also the wind deflector is provided with the end of the solar panel in the reverse direction of direction of advance.
4. the plant protection unmanned plane as claimed in claim 1 based on solar recharging system, it is characterised in that：The battery,
Transformer and charger are respectively positioned in the frame below the solar panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720049380.7U CN206384144U (en) | 2017-01-16 | 2017-01-16 | Plant protection unmanned plane based on solar recharging system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720049380.7U CN206384144U (en) | 2017-01-16 | 2017-01-16 | Plant protection unmanned plane based on solar recharging system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206384144U true CN206384144U (en) | 2017-08-08 |
Family
ID=59492753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720049380.7U Expired - Fee Related CN206384144U (en) | 2017-01-16 | 2017-01-16 | Plant protection unmanned plane based on solar recharging system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206384144U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927891A (en) * | 2017-12-18 | 2019-06-25 | 国鹄航空科技(杭州)股份有限公司 | A kind of miniature drone with solar recharging |
-
2017
- 2017-01-16 CN CN201720049380.7U patent/CN206384144U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109927891A (en) * | 2017-12-18 | 2019-06-25 | 国鹄航空科技(杭州)股份有限公司 | A kind of miniature drone with solar recharging |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20170808 Termination date: 20180116 |