CN206498228U - A kind of vehicle-mounted unmanned aerial vehicle charging system - Google Patents
A kind of vehicle-mounted unmanned aerial vehicle charging system Download PDFInfo
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- CN206498228U CN206498228U CN201720138131.5U CN201720138131U CN206498228U CN 206498228 U CN206498228 U CN 206498228U CN 201720138131 U CN201720138131 U CN 201720138131U CN 206498228 U CN206498228 U CN 206498228U
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- unmanned plane
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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
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
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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
- Y02E70/00—Other energy conversion or management systems reducing GHG emissions
- Y02E70/30—Systems combining energy storage with energy generation of non-fossil origin
-
- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model is related to a kind of vehicle-mounted unmanned aerial vehicle charging system, it is characterized in that:At least include:Unmanned plane vehicle-mounted frame, it is fixed on the roof of vehicle, there is onboard wireless charge coil on unmanned plane vehicle-mounted frame, onboard wireless charge coil is electrically connected with vehicle-mounted charge control circuit, vehicle-mounted charge controls circuit that the electric energy of the first on-vehicle battery is converted into the alternating voltage of charging, is coupled to and is electrically charged in load by onboard wireless charge coil;One unmanned plane charging induction coil; it is fixed in the housing in the middle of unmanned landing chassis; unmanned plane charging induction coil is socketed on charging magnet ring; charging magnet ring and unmanned plane charging induction coil are protected by housing; when on the onboard wireless charge coil of UAV Landing to unmanned plane vehicle-mounted frame, unmanned aerial vehicle (UAV) control circuit charges the electric energy that onboard wireless charge coil is received to unmanned machine battery.The features such as it has charging convenience, need not artificially participated in.
Description
Technical field
The utility model is related to a kind of unmanned plane charging technique, particularly a kind of vehicle-mounted unmanned aerial vehicle charging system.
Background technology
Disclosed in the patent that I has applied《Can by set point automatic Landing unmanned plane method and device》, its Shen
Please number be:201610879924.2.
This application patent obtains the coordinate information of landing chassis by unmanned plane, and positioning or high-precision is recognized by high precision image
The positioning that audio positioning completes the several Centimeter Levels of 1- is spent, the takeoff and landing automatic process control of unmanned plane body is realized.It is not
Only it is adapted to road conditions spy to patrol, also is adapted for geodesic survey and exploration.
Above-mentioned technology solve only the high-precision landing problems of unmanned plane, but for being charged by battery powered unmanned plane,
Can only be by the way of manually charging, it defines this technology broader practice.
Utility model content
The purpose of this utility model is to provide a kind of vehicle-mounted unmanned aerial vehicle Charging that is convenient, need not artificially participating in that charges
System, so that the application of automatic Landing unmanned plane more facilitates.
The purpose of this utility model is achieved in that a kind of vehicle-mounted unmanned aerial vehicle charging system, it is characterized in that:At least wrap
Include:Unmanned plane vehicle-mounted frame, is fixed on the roof of vehicle, there is onboard wireless charge coil, vehicle-mounted nothing on unmanned plane vehicle-mounted frame
Line charge coil is electrically connected with vehicle-mounted charge control circuit, and the electric energy of the first on-vehicle battery is converted into by vehicle-mounted charge control circuit
The alternating voltage of charging, is coupled to by onboard wireless charge coil and is electrically charged in load;
One unmanned plane charging induction coil, is fixed in the housing in the middle of unmanned landing chassis, unmanned plane charging induction coil
Be socketed in charging magnet ring on, charging magnet ring and unmanned plane charging induction coil protected by housing, when UAV Landing to nobody
When on the onboard wireless charge coil of locomotive carrier, unmanned aerial vehicle (UAV) control circuit fills the electric energy that onboard wireless charge coil is received
Supply electricity to unmanned machine battery.
Described onboard wireless charge coil is socketed on the first magnetic, unmanned plane charging induction coil and the first magnetic
Body is protected in housing by housing, onboard wireless charge coil and the first magnetic and unmanned plane charge induction coil and
Charging magnet ring constitutes high frequency transformer when overlapping.
There is sound omniselector on unmanned plane vehicle-mounted frame, sound navigation device at least includes three audio emission sources, three sounds
Take place frequently the different coordinate positions for penetrating source distribution in unmanned plane vehicle-mounted frame.
The external diameter of the first described magnetic is more than or equal to the external diameter of charging magnet ring, the internal diameter of described the first magnetic
Less than or equal to the internal diameter of charging magnet ring.
Wind-driven generator is fixed with described unmanned plane vehicle-mounted frame, the motor shaft sleeve of wind-driven generator is connected to fan blade, wind
Leaf is fixed on the lower end of unmanned plane vehicle-mounted frame, and fan blade is travelled with vehicle and rotated windward, and fan blade drives motor shaft to rotate, by wind-force
Electrical power generators control circuit to control to the first charging on-vehicle battery by wind-power electricity generation.
The housing forward end of described fan blade has an air inlet, and there is an air outlet rear end, and air inlet is oriented to by wind-guiding makes wind
Leaf is rotated to a direction, and in vehicle traveling, the wind of generation is entered by air inlet, is acted on fan blade, fan blade is rotated hair
Electricity, wind is discharged from air outlet.
There is optical alignment mark on transverse plane on unmanned plane vehicle-mounted frame.
Described optical alignment mark is in the middle of circular shape concentric bar code or Quick Response Code, circular shape concentric bar code or Quick Response Code
There is graphics wizard pattern.
Described graphics wizard is circular with pattern, when unmanned plane is navigated by graphics wizard with pattern to land, makes nothing
Man-machine charging induction coil is in concentric position with graphics wizard with pattern.
There is LED illumination light source below transverse plane on unmanned plane vehicle-mounted frame, when at night or when light is bad, shone by LED
Mingguang City source makes the optical alignment of transverse plane identify brightness raising, and the imaging sensor of unmanned plane can obtain optical alignment mark
Information.
The utility model has the advantages that:By fixing onboard wireless charge coil on unmanned plane vehicle-mounted frame, by nothing
Unmanned plane charging induction coil is fixed in the lower end of man-machine unmanned landing chassis, when UAV Landing to the vehicle-mounted of unmanned plane vehicle-mounted frame
When on Wireless charging coil, unmanned aerial vehicle (UAV) control circuit charges the electric energy that onboard wireless charge coil is received to unmanned electromechanical
Pond.
Meanwhile, by designing wind power generation unit on unmanned plane vehicle-mounted frame, the fan blade of wind power generation unit is with vehicle row
Sail and rotate windward, fan blade drives generator shaft to rotate, and is generated electricity from wind power generation unit to the first charging on-vehicle battery.So not
Need to charge to unmanned plane by the battery of vehicle in itself, it is not required that the self-contained battery on vehicle.
Brief description of the drawings
With reference to embodiment accompanying drawing, the utility model is described in further detail:
Fig. 1 is the structural representation of the utility model embodiment one;
Fig. 2 is unmanned landing chassis structural representation;
Fig. 3 is unmanned plane vehicle-mounted frame structural representation;
Fig. 4 is unmanned plane vehicle-mounted frame A-A profiles;
Fig. 5 is the fundamental diagram of the utility model embodiment;
Fig. 6 is the circular bar code schematic diagram of vehicle-mounted frame;
Fig. 7 is that vehicle-mounted frame uses the circular bar code schematic diagram of LED illumination under conditions of light is bad;
Fig. 8 is that the housing forward end of protection fan blade has an air inlet, rear end in order that being rotated when fan blade is rotated to a direction
There is an air outlet schematic diagram;
Fig. 9 is the vehicle structure schematic diagram for being applied to the fields such as agricultural, forestry;
Figure 10 is the square bar code schematic diagram of vehicle-mounted frame.
In figure, 1, unmanned landing chassis;2nd, unmanned plane vehicle-mounted frame;3rd, the magnetic line of force;4th, vehicle;5th, unmanned plane.
Embodiment
Embodiment 1
As shown in figure 1, a kind of vehicle-mounted unmanned aerial vehicle charging system, at least includes:Unmanned plane vehicle-mounted frame 2, is fixed on vehicle 4
On roof, there are onboard wireless charge coil 209, onboard wireless charge coil 209 and vehicle-mounted charge control on unmanned plane vehicle-mounted frame 2
Circuit 206 processed is electrically connected, and vehicle-mounted charge controls the alternating current that the electric energy of the first on-vehicle battery 205 is converted into charging by circuit 206
Pressure, is coupled to by onboard wireless charge coil 209 and is electrically charged in load;
One unmanned plane charging induction coil 102, is fixed in the housing 104 in the middle of unmanned landing chassis 1, unmanned plane charging sense
Coil 102 is answered to be socketed on charging magnet ring 103, charging magnet ring 103 and unmanned plane charging induction coil 102 are protected by housing 104
Shield.When on the onboard wireless charge coil 209 of UAV Landing to unmanned plane vehicle-mounted frame 2, unmanned aerial vehicle (UAV) control circuit will be vehicle-mounted
The electric energy that Wireless charging coil 209 is received charges to unmanned machine battery.
Embodiment 2
As shown in figure 1, a kind of vehicle-mounted unmanned aerial vehicle charging system, at least includes:Unmanned plane vehicle-mounted frame 2, is fixed on vehicle 4
On roof, there are onboard wireless charge coil 209, onboard wireless charge coil 209 and vehicle-mounted charge control on unmanned plane vehicle-mounted frame 2
Circuit 206 processed is electrically connected, and vehicle-mounted charge controls the alternating voltage that the electric energy of the first on-vehicle battery 205 is converted into charging by circuit 206,
Unmanned plane charging induction coil 102 is coupled to by onboard wireless charge coil 209;In order to increase coupling efficiency, onboard wireless
Charge coil 209 is socketed on the first magnetic 210, and unmanned plane charges the magnetic 210 of induction coil 102 and first in housing
In 201, protected by housing 201.
The induction coil 102 as shown in Fig. 2 a unmanned plane charges, is fixed in the housing 104 in the middle of unmanned landing chassis 1, nothing
Man-machine charging induction coil 102 is socketed on charging magnet ring 103, and charging magnet ring 103 and unmanned plane charging induction coil 102 pass through
Housing 104 is protected.When unmanned plane 5 lands onto the onboard wireless charge coil 209 of unmanned plane vehicle-mounted frame 2, unmanned aerial vehicle (UAV) control
Circuit charges the electric energy that onboard wireless charge coil 209 is received to unmanned machine battery.
In embodiment 1 and embodiment 2, magnetic is ring bodies magnet ring or discoid magnetic sheet.The first described magnetic
210 external diameter is more than or equal to the external diameter of charging magnet ring 103, and the internal diameter of the first described magnetic 12 is less than or equal to charging magnetic
The internal diameter of ring 103.
Embodiment 3
As shown in Figure 3 and Figure 4, on unmanned plane vehicle-mounted frame 2, the roof for being fixed on vehicle 4, have on unmanned plane vehicle-mounted frame 2
Onboard wireless charge coil 209, onboard wireless charge coil 209 is electrically connected with vehicle-mounted charge control circuit 206, vehicle-mounted charge control
The electric energy of first on-vehicle battery 205 is converted into the alternating voltage of charging by circuit 206 processed, passes through the lotus root of onboard wireless charge coil 209
Close unmanned plane charging induction coil 102;In order to increase coupling efficiency, onboard wireless charge coil 209 is socketed in the first magnetic
On body 210, unmanned plane charges the magnetic 210 of induction coil 102 and first in housing 201, is protected by housing 201.
Wind-driven generator 208 is fixed with unmanned plane vehicle-mounted frame 2, the motor shaft 203 of wind-driven generator 208 is socketed with fan blade
202, fan blade 202 is fixed on the lower end of unmanned plane vehicle-mounted frame 2, and fan blade 202 is travelled with vehicle 4 and rotated windward, and fan blade 202 drives
Motor shaft 203 is rotated, and is generated electricity from wind-driven generator 208 and is controlled circuit 207 to control to the first on-vehicle battery 205 by wind-power electricity generation
Charging.
As shown in figure 8, in order that being rotated when fan blade 202 is rotated to a direction, the housing forward end of protection fan blade 202 has
There is an air outlet 216 one air inlet 217, rear end, and air inlet 217 is oriented to by wind-guiding makes fan blade 202 be rotated to a direction, car
In 4 travelings, the wind of generation is entered by air inlet 217, is acted on fan blade 202, fan blade 202 is rotated generating, wind from
Air outlet 216 is discharged.Air inlet 217 plays wind-guiding effect, rotates fan blade 202.
Embodiment 4
As shown in Fig. 4, Fig. 6 and Fig. 7, unmanned plane vehicle-mounted frame 2, on the roof for being fixed on vehicle 4, in unmanned plane vehicle-mounted frame 2
On have an onboard wireless charge coil 209, onboard wireless charge coil 209 is electrically connected with vehicle-mounted charge control circuit 206, vehicle-mounted to fill
The electric energy of first on-vehicle battery 205 is converted into the alternating voltage of charging by electric control circuit 206, passes through onboard wireless charge coil
209 are coupled to unmanned plane charging induction coil 102;In order to increase coupling efficiency, onboard wireless charge coil 209 is socketed in first
On magnetic 210, unmanned plane charges the magnetic 210 of induction coil 102 and first in housing 201, is protected by housing 201
Shield.
Wind-driven generator 208 is fixed with unmanned plane vehicle-mounted frame 2, the motor shaft 203 of wind-driven generator 208 is socketed with fan blade
202, fan blade 202 is fixed on the lower end of unmanned plane vehicle-mounted frame 2, and fan blade 202 is travelled with vehicle 4 and rotated windward, and fan blade 202 drives
Motor shaft 203 is rotated, and is generated electricity from wind-driven generator 208 and is controlled circuit 207 to control to the first on-vehicle battery 205 by wind-power electricity generation
Charging.
As shown in Fig. 5 and Figure 10, there is optical alignment mark 214 on transverse plane 212 on unmanned plane vehicle-mounted frame 2, it is described
Optical alignment mark 214 is circular shape concentric bar code or square concentric bar code, and there are graphics wizard pattern 213, figure in centre
Navigation pattern 213 is circular or square, when unmanned plane is navigated by graphics wizard with pattern 213 to land, fills unmanned plane
Electric induction coil 102 is in concentric position with graphics wizard pattern 213.In addition, optical alignment mark 214 can make unmanned plane
5 accurately fall on the unmanned plane vehicle-mounted frame 2 controlled oneself, and it is to obtain light by the imaging sensor of unmanned plane 5 to realize this technology
Positioning mark 214 is learned, is completed by the information processing that 214 are identified to optical alignment.
Unmanned plane vehicle-mounted frame 2 in embodiment 4 can use the embodiment of embodiment 1, can also pass through embodiment 2
Embodiment.The embodiment of embodiment 2 has the characteristics of coupling efficiency is high, the magnetic of onboard wireless charge coil 209 and first
Body 210 constitutes high frequency transformer with unmanned plane charging induction coil 102 and charging magnet ring 103 when overlapping, and realizes that wireless type fills
Electricity Functional.
As shown in figure 5, during work, unmanned plane is dropped on unmanned plane vehicle-mounted frame 2 by space navigation, navigation makes vehicle-mounted nothing
The magnetic 210 of line charge coil 209 and first is in coincidence status with unmanned plane charging induction coil 102 and charging magnet ring 103,
Vehicle-mounted charge controls the alternating voltage that the electric energy of the first on-vehicle battery 205 is converted into charging by circuit 206(High frequency), pass through vehicle-mounted nothing
Line charge coil 209 is coupled to unmanned plane charging induction coil 102;Because the first magnetic 210 and charging magnet ring 103 are overlapped,
Magnetic power in the magnetic circuit that the first magnetic 210 and charging magnet ring 103 are constituted, realizes efficient charge function completely.
Embodiment 5
Embodiment 5 is that have LED illumination light below transverse plane 212 on unmanned plane vehicle-mounted frame 2 as different from Example 4
Source, when at night or when light is bad, making the optical alignment of upper transverse plane 212 identify 214 brightness by LED illumination light source and carry
Height, the imaging sensor of unmanned plane can easily obtain the information of optical alignment mark 214.
Embodiment 6
As shown in figure 9, embodiment 6 is that have container case 218 in the lower end of unmanned plane vehicle-mounted frame 2, container case 218 can be separated into many
Individual space, container case 218 has measuring unit of liquid level and liquid input and output control joint 219, and injection can be distributed in each space
Liquid fertilizer or agricultural chemicals, liquid fertilizer or agricultural chemicals and output chemical fertilizer or agricultural chemicals are injected by liquid input and output control joint 219.
Liquid input and output control joint 219 accesses the bottom of container case 218 by pipeline.Liquid input and output control joint 219 is led to
Cross connection water pump and outwardly or inwardly import and export liquid.Water pump is controlled respectively for two-way pump, or input and output.Embodiment 6 can
It is convenient to be applied to the different fields such as agricultural, forestry.
There is optical alignment to identify 214 on transverse plane 212 on unmanned plane vehicle-mounted frame 2, described optical alignment mark 214 is
There is graphics wizard pattern 213 circular shape concentric bar code, centre, and graphics wizard pattern 213 is circular or square, works as unmanned plane
When being landed by graphics wizard with the navigation of pattern 213, unmanned plane 5 is accurately fallen on the unmanned plane vehicle-mounted frame 2 controlled oneself, realize
This technology is to obtain optical alignment mark 214 by the imaging sensor of unmanned plane, by the letter that 214 are identified to optical alignment
Breath processing is completed.
Embodiment 7
As shown in figure 9, embodiment 7 is also to have container case 218 in the lower end of unmanned plane vehicle-mounted frame 2, container case 218 can be separated into
Multiple spaces, container case 218 has measuring unit of liquid level and liquid input and output control joint 219, and note can be distributed in each space
Enter liquid fertilizer or agricultural chemicals, liquid fertilizer or agricultural chemicals and output chemical fertilizer or agriculture are injected by liquid input and output control joint 219
Medicine.Liquid input and output control joint 219 accesses the bottom of container case 218 by pipeline.Liquid input and output control joint 219
Liquid is outwardly or inwardly imported and exported by connecting water pump.Water pump is two-way pump.Embodiment 6 can be conveniently applied to agricultural, forestry
Etc. different field.
There is sound omniselector 220 on unmanned plane vehicle-mounted frame 2 as different from Example 6, sound navigation device 220 is at least wrapped
Include three audio emission sources, different coordinate positions of three audio emission source distribution in unmanned plane vehicle-mounted frame 2.
Claims (10)
1. a kind of vehicle-mounted unmanned aerial vehicle charging system, it is characterized in that:At least include:Unmanned plane vehicle-mounted frame(2), it is fixed on vehicle(4)
Roof on, in unmanned plane vehicle-mounted frame(2)On have onboard wireless charge coil(209), onboard wireless charge coil(209)With car
Carry charging control circuit(206)Electrical connection, vehicle-mounted charge control circuit(206)By the first on-vehicle battery(205)Electric energy conversion
Into the alternating voltage of charging, pass through onboard wireless charge coil(209)It is coupled to and is electrically charged in load;
One unmanned plane charging induction coil(102), it is fixed on unmanned landing chassis(1)Middle housing(104)It is interior, unmanned plane charging
Induction coil(102)It is socketed in charging magnet ring(103)On, charge magnet ring(103)With unmanned plane charging induction coil(102)Pass through
Housing(104)Protection, when UAV Landing to unmanned plane vehicle-mounted frame(2)Onboard wireless charge coil(209)When upper, unmanned plane
Circuit is controlled by onboard wireless charge coil(209)The electric energy received charges to unmanned machine battery.
2. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 1, it is characterized in that:Described onboard wireless charging wire
Circle(209)It is socketed in the first magnetic(210)On, unmanned plane charging induction coil(102)With the first magnetic(210)In housing
(201)It is interior, by housing(201)Protected, onboard wireless charge coil(209)With the first magnetic(210)Filled with unmanned plane
Electric induction coil(102)With charging magnet ring(103)High frequency transformer is constituted when overlapping.
3. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 1, it is characterized in that:In unmanned plane vehicle-mounted frame(2)On
There is sound omniselector(220), sound navigation device(220)At least include three audio emission sources, three audio emission source distribution exist
Unmanned plane vehicle-mounted frame(2)Different coordinate positions.
4. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 2, it is characterized in that:The first described magnetic
(210)External diameter be more than or equal to charging magnet ring(103)External diameter, the first described magnetic(210)Internal diameter be less than or wait
In charging magnet ring(103)Internal diameter.
5. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 1, it is characterized in that:Described unmanned plane vehicle-mounted frame
(2)On be fixed with wind-driven generator(208), wind-driven generator(208)Motor shaft(203)It is socketed with fan blade(202), fan blade
(202)It is fixed on unmanned plane vehicle-mounted frame(2)Lower end, fan blade(202)With vehicle(4)Travel and rotate windward, fan blade(202)Band
Dynamic motor shaft(203)Rotate, by wind-driven generator(208)Generating controls circuit by wind-power electricity generation(207)Control to the first car
Carry battery(205)Charging.
6. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 5, it is characterized in that:Described fan blade(202)Shell
There is an air inlet body front end(217), there is an air outlet rear end(216), air inlet(217)Being oriented to by wind-guiding makes fan blade(202)
Rotated to a direction, vehicle(4)In traveling, the wind of generation passes through air inlet(217)Into acting on fan blade(202)On, make
Fan blade(202)Rotate and generate electricity, wind is from air outlet(216)Discharge.
7. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 1, it is characterized in that:In unmanned plane vehicle-mounted frame(2)On
Transverse plane(212)On have optical alignment mark(214).
8. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 7, it is characterized in that:Described optical alignment mark
(214)It is to have graphics wizard pattern in the middle of circular shape concentric bar code or Quick Response Code, circular shape concentric bar code or Quick Response Code
(213).
9. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 7, it is characterized in that:Graphics wizard pattern(213)
It is circular, when unmanned plane passes through graphics wizard pattern(213)During navigation landing, make unmanned plane charging induction coil(102)With
Graphics wizard pattern(213)It is in concentric position.
10. a kind of vehicle-mounted unmanned aerial vehicle charging system according to claim 7, it is characterized in that:Unmanned plane vehicle-mounted frame(2)Upper end
Plane(212)There is LED illumination light source below, when at night or when light is bad, upper transverse plane is made by LED illumination light source
(212)Optical alignment mark(214)Brightness is improved, and the imaging sensor of unmanned plane can obtain optical alignment mark(214)'s
Information.
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106786991A (en) * | 2017-02-16 | 2017-05-31 | 刘崇朴 | A kind of vehicle-mounted unmanned aerial vehicle charging system |
CN114228518A (en) * | 2021-10-25 | 2022-03-25 | 广东电网有限责任公司 | Unmanned aerial vehicle's on-vehicle wireless charging device and on-vehicle unmanned aerial vehicle system |
CN115871482A (en) * | 2023-02-03 | 2023-03-31 | 威泊(上海)新能源科技股份有限公司 | Wireless battery pack system and method supporting mobile charging of new energy automobile |
CN115973017A (en) * | 2023-03-01 | 2023-04-18 | 中润新能源(滁州)有限公司 | Intelligent transportation robot is used in battery piece production |
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2017
- 2017-02-16 CN CN201720138131.5U patent/CN206498228U/en active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106786991A (en) * | 2017-02-16 | 2017-05-31 | 刘崇朴 | A kind of vehicle-mounted unmanned aerial vehicle charging system |
CN114228518A (en) * | 2021-10-25 | 2022-03-25 | 广东电网有限责任公司 | Unmanned aerial vehicle's on-vehicle wireless charging device and on-vehicle unmanned aerial vehicle system |
CN115871482A (en) * | 2023-02-03 | 2023-03-31 | 威泊(上海)新能源科技股份有限公司 | Wireless battery pack system and method supporting mobile charging of new energy automobile |
CN115871482B (en) * | 2023-02-03 | 2023-05-16 | 威泊(上海)新能源科技股份有限公司 | Wireless battery pack system and method supporting mobile charging of new energy automobile |
CN115973017A (en) * | 2023-03-01 | 2023-04-18 | 中润新能源(滁州)有限公司 | Intelligent transportation robot is used in battery piece production |
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