CN106314806A - Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system - Google Patents
Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system Download PDFInfo
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- CN106314806A CN106314806A CN201610905825.7A CN201610905825A CN106314806A CN 106314806 A CN106314806 A CN 106314806A CN 201610905825 A CN201610905825 A CN 201610905825A CN 106314806 A CN106314806 A CN 106314806A
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- unmanned plane
- wind
- power generation
- generation plant
- solar
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- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000000295 complement effect Effects 0.000 title abstract description 4
- 238000010248 power generation Methods 0.000 claims abstract description 42
- 241000256259 Noctuidae Species 0.000 claims description 8
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 7
- 229910052744 lithium Inorganic materials 0.000 claims description 7
- 238000006243 chemical reaction Methods 0.000 claims description 5
- 230000005611 electricity Effects 0.000 claims description 5
- 230000005622 photoelectricity Effects 0.000 claims description 5
- 239000013589 supplement Substances 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005183 dynamical system Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
- H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Wind Motors (AREA)
Abstract
The invention relates to a wind-solar complementary generation system of a UAV (unmanned aerial vehicle) and an operation method of the system. A solar cell panel is mounted at the upper part of a UAV rack, a case, a power wing or a horizontal tail, a wind power generation device is mounted at the upper part of the UAV rack or the lower part of the power wing, electric energy generated by the solar cell panel and the wind power generation device is fed back to a storage battery by a power adapter, the cruising ability of the UAV is improved, electric power supplement or supply for the UAV is realized in the wind-solar complementary manner, the system is environment-friendly, the cruising ability of the UAV is improved greatly, and the cruising increase of the UAV is realized on the premise that the weight of the vehicle body is not increased.
Description
Technical field
The present invention relates to a kind of electricity generation system, be specifically related to a kind of unmanned plane wind and solar hybrid generating system and operation side thereof
Method.
Background technology
Unmanned plane can realize the collection of high resolution image, is making up satellite remote sensing often because cloud cover obtains less than shadow
As while shortcoming, solving conventional satellite remote sensing revisiting period long, the emergent problem such as not in time.Unmanned plane be utilize wireless
The most manned aircraft that electrical remote control equipment and the presetting apparatus provided for oneself are handled.Can be divided into from technical standpoint definition: unmanned solid
Fixed wing machine, unmanned VTOL machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..At present
Unmanned plane is adopted by frame, flight controller, dynamical system, electric operation dispatching system, propeller, camera head, aircraft platform system, information
Collecting system and ground control system etc. form.Either four-axle aircraft or aerodone, these unmanned planes are required to automatically controlled system
Electric power needed for system offer equipment completes operation and ensures the stable of each system of fuselage and run.Traditional mode is unmanned plane
Self carrying accumulator is flown, and must terminate the aerial mission of unmanned plane, it is ensured that unmanned plane before accumulator electric-quantity consumption is played
Landing in monitoring range, this restrict cruising time and the efficiently flight of unmanned plane.Carry too much accumulator will increase
The weight of complete machine, causes unmanned plane during flying efficiency to reduce.
Therefore, producing a kind of simple in construction, easy to operate, work and operational efficiency are high, and energy-conserving and environment-protective, method is simple and efficient
Unmanned plane wind and solar hybrid generating system and operation method, there is market prospect widely.
Summary of the invention
For the deficiencies in the prior art, the present invention provides a kind of simple in construction, easy to operate, and work and operational efficiency are high,
Energy-conserving and environment-protective, unmanned plane wind and solar hybrid generating system that method is simple and efficient and operation method thereof, be used for overcoming in prior art
Many defects.
The technology contents of the present invention is achieved in that a kind of unmanned plane wind and solar hybrid generating system, including being arranged on nothing
Accumulator battery on man-machine, described accumulator battery is connected with power supply adaptor by wire, and power supply adaptor passes through wire
It is connected with solar panel and wind power generation plant respectively.
Described solar panel is photoelectricity or the realization generating of light thermo-electric conversion, and described solar panel is extremely
It is one piece less, the solar panel that every piece of solar panel all uses specification to be 12V.
Described wind power generation plant drives electromotor to realize generating by air vane, and wind power generation plant is at least
It is one, the wind power generation plant that each wind power generation plant all uses specification to be 12V.
Described accumulator battery uses 3S Intelligent lithium battery to make.
Described solar panel is arranged on the unmanned plane daylighting position towards top.
Described wind power generation plant is arranged on unmanned plane upper rack or engine underwing.
The operation method of a kind of unmanned plane wind and solar hybrid generating system as above, its operation method is as follows: unmanned
Solar panel is installed on the top of machine frame or casing or power wing or tailplane, at unmanned plane upper rack
Or engine underwing installs wind power generation plant, through power supply adaptor, solar panel and wind power generation plant is sent out
The electric energy feedback gone out, to accumulator battery, increases the flying power of unmanned plane.
The present invention has following good effect: present configuration is simple, easy to operate, in unmanned plane frame or casing
Or solar panel is installed on the top of power wing or tailplane, under unmanned plane upper rack or power wing
Wind power generation plant is installed in portion, through power supply adaptor sun can the electric energy feedback that sends of cell panel and wind power generation plant to storage
Set of cells, increases the flying power of unmanned plane, realizes electric power supply or supply, the skill of unmanned plane by the way of wind light mutual complementing
Energy environmental protection, substantially increases the flying power of unmanned plane simultaneously, can be on the premise of not increasing fuselage weight, it is achieved unmanned plane
Continuation of the journey increases.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is one of use status architecture schematic diagram of the present invention.
Fig. 3 is the two of the use status architecture schematic diagram of the present invention.
Detailed description of the invention
As shown in Figure 1, 2, 3, a kind of unmanned plane wind and solar hybrid generating system, including the accumulator battery being arranged on unmanned plane
4, described accumulator battery 4 is connected with power supply adaptor 3 by wire, power supply adaptor 3 pass through wire respectively with solar energy
Cell panel 1 is connected with wind power generation plant 2.Described solar panel 1 is photoelectricity or the realization generating of light thermo-electric conversion
, described solar panel 1 at least a piece, every piece of solar panel 1 all uses specification to be the solaode of 12V
Plate.Described wind power generation plant 2 drives electromotor to realize generating by air vane, and wind power generation plant 2 is at least
One, each wind power generation plant 2 all uses specification to be the wind power generation plant of 12V.Described accumulator battery 4 uses 3S intelligence
Lithium battery is made.Described solar panel 1 is arranged on the unmanned plane daylighting position towards top.Described wind-power electricity generation
Device 2 is arranged on unmanned plane upper rack or engine underwing.
The operation method of a kind of unmanned plane wind and solar hybrid generating system as above, its operation method is as follows: unmanned
Solar panel 1 is installed on the top of machine frame or casing or power wing or tailplane, in unmanned plane frame
Portion or engine underwing install wind power generation plant 2, through 3 solar panels 1 of power supply adaptor and wind-power electricity generation
The electric energy feedback that device 2 sends, to accumulator battery 4, increases the flying power of unmanned plane.
Embodiment 1: a kind of unmanned plane wind and solar hybrid generating system, including the accumulator battery 4 being arranged on unmanned plane, described
Accumulator battery 4 be connected with power supply adaptor 3 by wire, power supply adaptor 3 pass through wire respectively with solar panel 1
It is connected with wind power generation plant 2.Described solar panel 1 is photoelectricity or the realization generating of light thermo-electric conversion, described
Solar panel 1 at least a piece, every piece of solar panel 1 all uses specification to be the solar panel of 12V.Described
Wind power generation plant 2 drive electromotor to realize generating by air vane, wind power generation plant 2 at least, often
Individual wind power generation plant 2 all uses specification to be the wind power generation plant of 12V.Described accumulator battery 4 uses 3S Intelligent lithium battery
Make.Described solar panel 1 is arranged on the unmanned plane daylighting position towards top.Described wind power generation plant 2
It is arranged on unmanned plane upper rack.Its operation method is as follows: install solar panel in unmanned plane frame or casing top
1, at unmanned plane upper rack, wind power generation plant 2 is installed, through 3 solar panels 1 of power supply adaptor and wind-power electricity generation
The electric energy feedback that device 2 sends, to accumulator battery 4, increases the flying power of unmanned plane.
Fig. 2 is four-axle aircraft unmanned plane, as it can be seen, the general frame of four-axle aircraft is constant, in frame and casing
On increase solar panel 1 to the daylighting position on top, at the corresponding part of propeller, (general propeller up, can
Electromotor is loaded on lower section) or the core increase wind power generation plant 2 of frame, send through power supply adaptor 3 simultaneously
Electric energy feedback to accumulator battery 4, increase the flying power of unmanned plane.Solar panel uses 12V's, if the single sun
The energy not enough method that can use serial or parallel connection of cell panel, wind-driven generator uses 12V, and the battery of unmanned plane uses 3S
Intelligent lithium battery, can reduce to chargeable voltage by power supply adaptor 12V and be charged.
Embodiment 2: a kind of unmanned plane wind and solar hybrid generating system, including the accumulator battery 4 being arranged on unmanned plane, described
Accumulator battery 4 be connected with power supply adaptor 3 by wire, power supply adaptor 3 pass through wire respectively with solar panel 1
It is connected with wind power generation plant 2.Described solar panel 1 is photoelectricity or the realization generating of light thermo-electric conversion, described
Solar panel 1 at least a piece, every piece of solar panel 1 all uses specification to be the solar panel of 12V.Described
Wind power generation plant 2 drive electromotor to realize generating by air vane, wind power generation plant 2 at least, often
Individual wind power generation plant 2 all uses specification to be the wind power generation plant of 12V.Described accumulator battery 4 uses 3S Intelligent lithium battery
Make.Described solar panel 1 is arranged on the unmanned plane daylighting position towards top.Described wind power generation plant 2
It is arranged on unmanned plane engine underwing.Its operation method is as follows: pacify on the top of unmanned plane power wing or tailplane
Dress solar panel 1, installs wind power generation plant 2 at unmanned plane engine underwing, through 3 solar energys of power supply adaptor
The electric energy feedback that cell panel 1 and wind power generation plant 2 send, to accumulator battery 4, increases the flying power of unmanned plane.
As it is shown on figure 3, Fig. 3 is gliding type unmanned plane, on the basis of aerodone, main wing and the tailplane of aerodone
To upper part install solar panel 1, aerodone power section main wing bottom increase wind power generation plant 2, with
Time through 3 electric energy feedbacks sent of power supply adaptor to accumulator battery 4, increase the flying power of unmanned plane.Solaode
Plate uses 12V's, if the not enough method that can use serial or parallel connection of single solar panel, wind-driven generator uses
12V's, the battery of unmanned plane uses 3S Intelligent lithium battery, by power supply adaptor, 12V can be reduced to chargeable voltage and carry out
Charging.
The frame of unmanned plane has been largely fixed this unmanned plane OK use.This patent is not before changing frame
Put, wind-light complementary system is joined the diverse location of frame, it is achieved the most completely and reasonably fly and realize electric energy
Supply.This patent coordinates the flight control system of unmanned plane, dynamical system, electric operation dispatching system, propeller, camera head, aircraft platform system
System, information acquisition system and ground control system, on the premise of too much increasing deadweight, provide electric power supply for unmanned plane, and
Realize the cooperation between element, it is ensured that unmanned plane stable.
Claims (7)
1. a unmanned plane wind and solar hybrid generating system, including the accumulator battery (4) being arranged on unmanned plane, it is characterised in that:
Described accumulator battery (4) is connected with power supply adaptor (3) by wire, power supply adaptor (3) pass through wire respectively with too
Sun can be connected with wind power generation plant (2) by cell panel (1).
Unmanned plane wind and solar hybrid generating system the most according to claim 1, it is characterised in that: described solar panel
(1) it is photoelectricity or the realization generating of light thermo-electric conversion, described solar panel (1) at least a piece, every piece of solar energy
Cell panel (1) all uses specification to be the solar panel of 12V.
Unmanned plane wind and solar hybrid generating system the most according to claim 1, it is characterised in that: described wind power generation plant
(2) electromotor is driven to realize generating by air vane, wind power generation plant (2) at least, each wind-power electricity generation
Device (2) all uses specification to be the wind power generation plant of 12V.
Unmanned plane wind and solar hybrid generating system the most according to claim 1, it is characterised in that: described accumulator battery (4)
3S Intelligent lithium battery is used to make.
Unmanned plane wind and solar hybrid generating system the most according to claim 2, it is characterised in that: described solar panel
(1) unmanned plane daylighting position towards top it is arranged on.
Unmanned plane wind and solar hybrid generating system the most according to claim 3, it is characterised in that: described wind power generation plant
(2) unmanned plane upper rack or engine underwing it are arranged on.
7. the operation method of a unmanned plane wind and solar hybrid generating system as claimed in claim 1, it is characterised in that it runs
Method is as follows: install solar panel on the top of unmanned plane frame or casing or power wing or tailplane
(1), wind power generation plant (2) is installed, through power supply adaptor (3) too at unmanned plane upper rack or engine underwing
The electric energy feedback that sun energy cell panel (1) and wind power generation plant (2) send, to accumulator battery (4), increases the continuation of the journey energy of unmanned plane
Power.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610905825.7A CN106314806A (en) | 2016-10-19 | 2016-10-19 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610905825.7A CN106314806A (en) | 2016-10-19 | 2016-10-19 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106314806A true CN106314806A (en) | 2017-01-11 |
Family
ID=57817788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610905825.7A Pending CN106314806A (en) | 2016-10-19 | 2016-10-19 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
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| Country | Link |
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| CN (1) | CN106314806A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107310724A (en) * | 2017-06-21 | 2017-11-03 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine that is used for wind-power electricity generation and can sow |
| CN113525696A (en) * | 2021-06-02 | 2021-10-22 | 南昌市周静新能源有限公司 | Integrative new forms of energy unmanned aerial vehicle of scene |
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| CN206107581U (en) * | 2016-10-19 | 2017-04-19 | 黄河交通学院 | Complementary power generation system of unmanned aerial vehicle scene |
-
2016
- 2016-10-19 CN CN201610905825.7A patent/CN106314806A/en active Pending
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| JPH10119896A (en) * | 1996-10-21 | 1998-05-12 | Tatsuno Co Ltd | Electric airplane |
| CN101758926A (en) * | 2009-03-13 | 2010-06-30 | 黄灿荣 | Wind energy and solar energy power generation electric airplane |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107310724A (en) * | 2017-06-21 | 2017-11-03 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine that is used for wind-power electricity generation and can sow |
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| CN113525696A (en) * | 2021-06-02 | 2021-10-22 | 南昌市周静新能源有限公司 | Integrative new forms of energy unmanned aerial vehicle of scene |
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Application publication date: 20170111 |