CN205986711U - Unmanned aerial vehicle with energy -conserving power supply system - Google Patents
Unmanned aerial vehicle with energy -conserving power supply system Download PDFInfo
- Publication number
- CN205986711U CN205986711U CN201620724218.6U CN201620724218U CN205986711U CN 205986711 U CN205986711 U CN 205986711U CN 201620724218 U CN201620724218 U CN 201620724218U CN 205986711 U CN205986711 U CN 205986711U
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- CN
- China
- Prior art keywords
- power supply
- unmanned plane
- generation module
- controller
- power generation
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- 238000010248 power generation Methods 0.000 claims abstract description 21
- 238000004134 energy conservation Methods 0.000 claims description 11
- 238000005183 dynamical system Methods 0.000 claims description 3
- 239000000463 materials Substances 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims 1
- 238000005516 engineering processes Methods 0.000 description 2
- 239000000446 fuels Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagrams Methods 0.000 description 1
- 238000000034 methods Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
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
- 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
Abstract
The utility model provides an unmanned aerial vehicle with energy -conserving power supply system, includes fuselage, rotor, provides driving system (5), power and the energy -conserving power supply system of power for the rotor. Energy -conserving power supply system wherein includes wind power generation module (1), photovoltaic power generation module (2) and controller (3). Controller (3) are connected with power (4), wind power generation module (1) and photovoltaic power generation module (2) respectively. The charging control is carried out to power (4) in controller (3) control wind power generation module (1), photovoltaic power generation module (2), overcharges and crosses discharge protection power (4) simultaneously.
Description
Technical field
The utility model is related to vehicle technology field, and more particularly, to a kind of endurance is strong, stream time length
Unmanned plane.
Background technology
Unmanned plane is applied to military affairs, scientific research, industry, the field such as civilian more and more widely, and current unmanned plane makes mostly
There is provided power, drive motor or engine rotation with battery or fuel for navigation, then by actuator drives rotor not
The rotation stopping.Under the situation of unmanned plane industry high speed development, but there is a problem of that one is universal it is simply that endurance is too poor,
Stream time is short.Either it is used fuel electric energy to be still used as power source as power source, because unmanned plane is in sky
Middle need are continual to be carried out communication with ground and obtains orientation and control signal, and have also needs to carry a large amount of electronic instruments and set
Standby, so its power consumption is very big, the electricity of battery is often not enough to maintain the long-time continuation of the journey of unmanned plane so that making of unmanned plane
With being restricted.
Therefore it provides a kind of endurance is strong, the unmanned plane of stream time length, just become those skilled in the art urgently
The problem that need to solve.
Utility model content
To achieve these goals, the utility model provides that a kind of endurance is strong, the unmanned plane of stream time length.
The utility model specifically adopts the following technical scheme that：
A kind of unmanned plane with energy conservation and power supply system, including fuselage, rotor, for rotor provide power dynamical system,
Power supply and energy conservation and power supply system；Energy conservation and power supply system includes wind power generation module, photovoltaic generating module and controller, wherein, control
Device processed controls wind power generation module, photovoltaic generating module power supply to be charged control, and carries out overcharge and mistake to power supply simultaneously
Discharge prevention.
Preferably, wind power generation module includes the wind power generating set being connected with rotor.
Preferably, photovoltaic generating module includes film photovoltaic cell, and film photovoltaic cell is attached to external fuselage.
Preferably, film photovoltaic cell is flexible material, is suitable for fitting with fuselage.
Preferably, controller is connected with power supply, wind power generation module and photovoltaic generating module respectively.
Preferably, controller has electric quantity of power supply estimation and cruising time estimation function.
Preferably, controller is wind/light complementation controller, can be with real-time regulation wind power generation module, photovoltaic generating module pair
The charging current of power supply and charge volume.
Preferably, the quantity of rotor is two or more.
Unmanned plane using technique scheme, it is possible to use wind-force in flight course for the unmanned plane and sunlight
Producing electric energy is to power on unmanned plane, it is possible to achieve improve the course continuation mileage of unmanned plane and the purpose of time.
Brief description
Fig. 1 is the schematic diagram of the energy conservation and power supply system of unmanned plane of the present utility model.
Specific embodiment
Below in conjunction with the accompanying drawings the utility model is further detailed.
The unmanned plane with energy conservation and power supply system includes fuselage, rotor, the dynamical system 5 for rotor offer power, power supply
And energy conservation and power supply system.Energy conservation and power supply system therein includes wind power generation module 1, photovoltaic generating module 2 and controller 3.Control
Device 3 processed is connected with power supply 4, wind power generation module 1 and photovoltaic generating module 2 respectively.Controller 3 controls wind power generation module 1, light
Volt electricity generation module 2 is charged to power supply 4 controlling, and carries out overcharge and over to power supply 4 simultaneously.
Wind power generation module 1 includes the wind power generating set being connected with rotor.The quantity of rotor is two or more.
Photovoltaic generating module 2 includes film photovoltaic cell, and film photovoltaic cell is flexible material, to be suitable for being attached to external fuselage.
Controller 3 has electric quantity of power supply estimation and cruising time estimation function.Controller is wind/light complementation controller, can be with real-time regulation
Wind power generation module, photovoltaic generating module are to the charging current of power supply and charge volume.
These are only preferred embodiment of the present utility model, in the situation without departing from spirit and scope of the present utility model
Under, can by with various different in the way of described embodiment is modified.Therefore, above-mentioned accompanying drawing and description should not be construed as
Restriction to the utility model claims.
Claims (8)
1. a kind of unmanned plane with energy conservation and power supply system, including fuselage, rotor, the dynamical system for rotor offer power, electricity
Source and energy conservation and power supply system；It is characterized in that：Energy conservation and power supply system includes wind power generation module, photovoltaic generating module and control
Device, wherein, controller controls wind power generation module, photovoltaic generating module power supply to be charged control, and power supply is carried out simultaneously
Overcharge and over.
2. unmanned plane according to claim 1 is it is characterised in that the wind-force that wind power generation module includes being connected with rotor is sent out
Group of motors.
3. unmanned plane according to claim 1 is it is characterised in that photovoltaic generating module includes film photovoltaic cell, film light
Volt battery is attached to external fuselage.
4. unmanned plane according to claim 3, it is characterised in that film photovoltaic cell is flexible material, is suitable for and fuselage
Laminating.
5. unmanned plane according to claim 1 it is characterised in that controller respectively with power supply, wind power generation module and photovoltaic
Electricity generation module connects.
6. unmanned plane according to claim 1 it is characterised in that controller have electric quantity of power supply estimation estimate with cruising time
Calculate function.
7. unmanned plane according to claim 1, can be with real-time regulation it is characterised in that controller is wind/light complementation controller
Wind power generation module, photovoltaic generating module are to the charging current of power supply and charge volume.
8. unmanned plane according to claim 1 is it is characterised in that the quantity of rotor is two or more.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620724218.6U CN205986711U (en) | 2016-07-12 | 2016-07-12 | Unmanned aerial vehicle with energy -conserving power supply system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620724218.6U CN205986711U (en) | 2016-07-12 | 2016-07-12 | Unmanned aerial vehicle with energy -conserving power supply system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205986711U true CN205986711U (en) | 2017-02-22 |
Family
ID=58023688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620724218.6U Active CN205986711U (en) | 2016-07-12 | 2016-07-12 | Unmanned aerial vehicle with energy -conserving power supply system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205986711U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108778929A (en) * | 2017-05-10 | 2018-11-09 | 深圳市大疆创新科技有限公司 | Battery management system, battery and unmanned vehicle |
-
2016
- 2016-07-12 CN CN201620724218.6U patent/CN205986711U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108778929A (en) * | 2017-05-10 | 2018-11-09 | 深圳市大疆创新科技有限公司 | Battery management system, battery and unmanned vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |