CN106786866A - A kind of unmanned plane charging system and method, charging streetlamp - Google Patents
A kind of unmanned plane charging system and method, charging streetlamp Download PDFInfo
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- CN106786866A CN106786866A CN201611154275.6A CN201611154275A CN106786866A CN 106786866 A CN106786866 A CN 106786866A CN 201611154275 A CN201611154275 A CN 201611154275A CN 106786866 A CN106786866 A CN 106786866A
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Classifications
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- 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
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S9/00—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply
- F21S9/02—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator
- F21S9/03—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light
- F21S9/035—Lighting devices with a built-in power supply; Systems employing lighting devices with a built-in power supply the power supply being a battery or accumulator rechargeable by exposure to light the solar unit being integrated within the support for the lighting unit, e.g. within or on a pole
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
- H01M10/44—Methods for charging or discharging
-
- 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
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
- H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
- H02S20/32—Supporting structures being movable or adjustable, e.g. for angle adjustment specially adapted for solar tracking
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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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/70—Hybrid systems, e.g. uninterruptible or back-up power supplies integrating renewable energies
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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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/72—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps in street lighting
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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
-
- 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
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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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
- 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
-
- 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
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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Abstract
The present invention relates to a kind of unmanned plane charging system and method, charging streetlamp, the charging system be arranged on lamppost and including：Charging positive electrode mechanism, charging negative electrode mechanism, administration of power supply, induction mechanism and master controller, wherein, charging positive electrode mechanism includes charging positive electrode plate, charging positive electrode plate fixed mount, the first power unit and the second power unit, and charging negative electrode mechanism includes：Charging negative electrode plate, charging negative electrode plate fixed mount and the 3rd power unit, administration of power supply include the solar charging panel at the back side for being attached to the charging negative electrode plate, and induction mechanism includes the first inductor for sensing unmanned plane charge request signal.The present invention is unmanned plane charging using solar street light, with unrivaled spatter property, the security of height, the relative popularity of the energy and abundance.
Description
Technical field
The present invention relates to unmanned plane charging technique field, and in particular to a kind of unmanned plane charging system and method, charging circuit
Lamp.
Background technology
In high-altitude flight, unmanned plane is one of direction of following aviation field development, and the development of unmanned plane is modern nowadays
Military developing status more and more higher.Unmanned plane shows flexibility in the tasks such as monitoring, scout-attack, convenient
Property and high efficiency, the present age and future military war in have extremely important strategic importance, as contemporary military affairs " lifting
Device ".The endurance of unmanned plane is improved, is the big important topic for developing unmanned plane；The charging modes of current unmanned plane are main
Have following several：1) wireless charging, due to the half that charge efficiency is traditional charge efficiency, so wireless charging be difficult to so far it is general
And；2) power transmission line is charged, i.e., ordinary high pressure electric wire charges, and unmanned plane can rested in and charged on high-tension bus-bar, more convenient, efficiency
It is very high, it is a kind of original charging modes, due to power transmission line damage electric wire easy to charge, then the consequence for damaging high-tension bus-bar is light
Then influence people life, heavy then harm safety；3) unmanned plane wire is charged, and the flight model of unmanned plane is charged such that due to this
Enclose and be very restricted, so there is significant limitation.4) unmanned plane positioning charges.Unmanned plane positions the characteristics of charging
Orderly manageability, the gps system on unmanned plane is oriented to its charging station of flying to and is charged, and completes to charge using chip docking.
But under the influence of actual various factors, unmanned plane cannot often accomplish accurate docking, and this is always unmanned plane in technical elements
One important topic of researcher, so the positioning of unmanned plane charges also needs to further research.
The content of the invention
It is an object of the invention to provide a kind of unmanned plane charging system and method, charging streetlamp, it is used to solve existing due to existing
The shortcoming of some charging modes causes the problem that the limited endurance for making unmanned plane of charging modes reduces.
To achieve the above object, a kind of unmanned plane charging system disclosed by the invention, specifically, the charging system includes：
Charging positive electrode mechanism, including：Charging positive electrode plate, charging positive electrode plate fixed mount, the first power unit and the second power list
Unit, the charging positive electrode plate is rotatably affixed to the charging positive electrode plate fixed mount outer end by the first rotary shaft, described
Charging positive electrode plate fixed mount is slidably mounted to the slide rail being fixed on lamppost, first power unit along the vertical direction
The outer end of the charging positive electrode plate is connected to, second power unit is connected to the upper of the charging positive electrode plate fixed mount
End；Charging negative electrode mechanism, including：Charging negative electrode plate, charging negative electrode plate fixed mount and the 3rd power unit, the charging
Negative electrode plate is rotatably affixed to the 3rd power unit by the second rotary shaft, and the 3rd power unit is fixed to described
On charging negative electrode plate fixed mount, the charging negative electrode plate fixed mount is fixed to below the charging positive electrode plate fixed mount
On lamppost；Administration of power supply, including it is attached to the solar charging panel at the back side of the charging negative electrode plate；Induction mechanism, bag
The first inductor for sensing unmanned plane charge request signal is included, first inductor is attached on lamppost；Master control
Device, is attached in lamppost；Wherein, the solar charging panel is connected to the charging positive electrode plate and the charging negative electrode
Plate, is provided with the first charging and opens between the solar charging panel and the charging positive electrode plate and the charging negative electrode plate
Close, first power unit, second power unit, the 3rd power unit, first charge switch and described
First inductor is respectively connecting to master controller.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, first power unit includes first
Motor and drawstring, second power unit include the second motor and connecting rod, and first motor and second motor are fixed
To motor fixed column, on the lamppost that the motor fixed column is fixed on below street lamp, the two ends of the drawstring connect respectively
To the outer end of first motor and the charging positive electrode plate, the two ends of the connecting rod be respectively connecting to second motor and
The upper end of the charging positive electrode plate fixed mount, the 3rd power unit includes the 3rd motor, and the 3rd motor is fixed to
On the charging negative electrode plate fixed mount and it is connected to the second rotary shaft, first motor, second motor and described
Three motors are respectively connecting to master controller.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, first power unit includes two
First motor and two drawstrings, second power unit include two the second motors and two connecting rods, described two first electricity
Machine is relatively fixed in the both sides of the motor fixed column, and two drawstrings are located at the both sides of the motor fixed column, every drawing
The two ends of rope are respectively connecting to the outer end of one of them first motor and the charging positive electrode plate, described two second motor phases
Both sides to being fixed on the motor fixed column, described two connecting rods are located at the both sides of the motor fixed column, each connecting rod
Two ends are respectively connecting to the upper end of one of them second motor and the charging positive electrode plate fixed mount.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, the administration of power supply is also supplied including civil power
Electric unit, the mains-supplied unit is connected to the charging positive electrode plate and the charging negative electrode plate, the mains-supplied
The second charge switch is provided between unit and the charging positive electrode plate and the charging negative electrode plate, described second charges opens
Connection is connected to master controller.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, the induction mechanism is also included for feeling
The second inductor of unmanned plane charging current, second inductor is answered to be attached in the lamppost and be connected to master control
Device.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, the induction mechanism is also included for feeling
The 3rd inductor for answering unmanned plane to pay, the 3rd inductor is attached on the lamppost and is connected to master controller.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, the sun is provided with the solar panels
Light tracker, the sunshine tracker is connected with the master controller.
Above-mentioned a kind of unmanned plane charging system disclosed by the invention, further, is provided with the charging positive electrode plate
Multiple point-like charging positive poles are simultaneously distributed with multiple penetrating circular holes or spherical concave surface；Multiple circles are distributed with the charging negative electrode plate
Charging negative pole is provided between tapered protrusion, the projection.
Further, the invention also discloses a kind of unmanned plane charging method, the charging method includes：First inductor sense
The charge request signal of unmanned plane should be arrived and induced signal is sent to master controller；Master controller controls the 3rd motor to start to turn
Dynamic, the 3rd motor drives charging negative electrode plate and solar charging panel to rotate, and makes the direction of charging negative electrode plate upward and the sun
Can charging panel be directed downward；The leg of unmanned plane is drop in the gap of the multiple conical protrusions on charging negative electrode plate simultaneously
Connected with the charging cathode contact between projection as the negative pole of unmanned plane charge port；Unmanned plane stabilization drop to charging negative electrode plate
Afterwards, sense and pay by the 3rd inductor；3rd inductor unmanned plane is paid the signal for completing and is sent to master controller；Always
Controller controls the first motor to rotate, and the first motor decontrols drawstring is rotated down charging positive electrode plate until in horizontal
State, and control the first charge switch of closure to connect solar charging panel and charging positive electrode plate and charging negative electrode plate, or control
System the second charge switch of closure connects mains-supplied unit and charging positive electrode plate and charging negative electrode plate；Master controller is controlled
Second motor is rotated, and the second motor pushes down on connecting rod, and charging positive electrode plate and charging positive electrode plate fixed mount are along lamppost
On slide rail move down；Penetrating circular hole or spherical concave surface below charging positive electrode plate touch filling for unmanned plane wing tip
The spherical on power port positive terminal top, unmanned plane is started to charge up and produces charging current；Second inductor senses charging electricity
Miscarriage is raw and sends to master controller this induced signal；What the charging current that master controller receives the transmission of the second inductor was produced
The first motor and the second motor are controlled after induced signal to carry out self-locking and stops operating；After unmanned plane charging complete, charging current
Diminish or disappear, the second inductor senses that charging current diminishes or disappears and send to master controller this induced signal；Always
Controller receive the transmission of the second inductor charging current diminish or the induced signal that disappears after, control the first charge switch of opening
Solar charging panel and charging positive electrode plate and charging negative electrode plate are disconnected, or control is opened the second charge switch and supplies civil power
Electric unit disconnects with charging positive electrode plate and charging negative electrode plate；Master controller controls the second motor to rotate, and the second motor is upward
Connecting rod is pulled, charging positive electrode plate and charging positive electrode plate fixed mount are move upwardly until along the slide rail on lamppost and touch
Motor fixed column；Master controller controls the first motor to rotate, and the first motor tenses drawstring makes charging positive electrode plate rotate up directly
To in plumbness；Unmanned plane takes off and departs from charging negative electrode plate；Master controller controls the 3rd motor to start to rotate, the 3rd electricity
Machine drives charging negative electrode plate and solar charging panel to rotate, and makes being directed downward and solar charging panel for charging negative electrode plate
Direction is upward；Solar charging panel direction receives solar energy and converts solar energy into electrical energy upward；In solar charging panel side
During solar energy is received upward, sensed by sunshine tracker and receive the intensity of sunshine and will sense too
Sunlight strength feeds back to master controller, and master controller makes solar charging panel be moved with the sun by controlling the rotation of the 3rd motor
And rotate, solar charging panel is farthest utilized sunshine.
Still further aspect, the invention also discloses a kind of unmanned plane charging streetlamp, including above-mentioned one kind disclosed by the invention
Unmanned plane charging system.
The invention has the advantages that：
The present invention is unmanned plane charging using solar street light, with unrivaled spatter property, the security of height, energy
Advantage not available for other conventional energy resources such as the relative popularity and abundance in source, long-life and non-maintaining property；Using existing
There is resource space, simplify charging, rationalize, charging platform, the suffered space-time shadow of unmanned plane charging are set on streetlamp foundation
Sound can be preferably minimized.
Brief description of the drawings
Fig. 1 is a kind of structured flowchart of unmanned plane charging system disclosed by the invention.
Fig. 2 is a kind of structural representation of unmanned plane charging system disclosed by the invention.
Fig. 3 is the partial enlarged drawing that a kind of unmanned plane charging system disclosed by the invention is under unmanned plane charged state.
Fig. 4 charges with finishing and flies away from charging negative electrode plate for a kind of unmanned plane charging system disclosed by the invention is in unmanned plane
Partial enlarged drawing under state.
Fig. 5 is the structure for being suitable for the application of a kind of four wings unmanned plane that a kind of unmanned plane charging system disclosed by the invention charges
Figure.
Fig. 6 is that the charge port positive pole for being suitable for the application of the unmanned plane that a kind of unmanned plane charging system disclosed by the invention charges connects
The structure chart of head.
Fig. 7 is the partial enlarged drawing of the unmanned plane charge port positive terminal disclosed in Fig. 6.
Fig. 8 is the structural representation for carrying out the plug of indoor charging to unmanned plane disclosed by the invention.
Specific embodiment
Following examples are used to illustrate the present invention, but are not limited to the scope of the present invention.
Embodiment 1
With reference to Fig. 1 and Fig. 2, a kind of unmanned plane charging system includes disclosed in the present embodiment：Charging positive electrode mechanism, fill
Electric negative electrode mechanism, administration of power supply, induction mechanism and master controller 01, wherein, charging positive electrode mechanism includes：Charging positive electrode
Plate 02, charging positive electrode plate fixed mount 03, the first power unit and the second power unit, charging positive electrode plate 02 is by the first rotation
Rotating shaft 04 is rotatably affixed to the outer end of charging positive electrode plate fixed mount 03, and charging positive electrode plate fixed mount 03 can be slided along the vertical direction
Dynamic to be attached on slide rail 06, slide rail 06 is fixed on lamppost 05, and the first power unit is connected to the outer of charging positive electrode plate 02
End, the second power unit is connected to the upper end of charging positive electrode plate fixed mount 03；Charging negative electrode mechanism includes：Charging negative electrode
Plate 07, charging negative electrode plate fixed mount 08 and the 3rd power unit, charging negative electrode plate 07 are rotatable by the second rotary shaft 09
The 3rd power unit is fixed to, the 3rd power unit is fixed on charging negative electrode plate fixed mount 08, and charging negative electrode plate is fixed
Frame 08 is fixed on the lamppost 05 of the lower section of charging positive electrode plate fixed mount 03；Administration of power supply includes being attached to charging negative electrode plate
The solar charging panel 10 at 07 back side；Induction mechanism includes the first inductor for sensing the charge request signal of unmanned plane 11
12, the first inductor 12 is attached to lamppost top, beneficial to the signal for receiving unmanned plane；Master controller 01 is attached to lamppost 05
It is interior；Wherein, solar charging panel 10 is connected to charging positive electrode plate 02 and charging negative electrode plate 07, solar charging panel 10 with fill
The first charge switch 13, the first power unit, the second power list are provided between electric positive electrode plate 02 and charging negative electrode plate 07
Unit, the 3rd power unit, the first charge switch 13 and the first inductor 12 are respectively connecting to master controller 01.
Further, the first power unit includes the first motor 14 and drawstring 15, and the second power unit includes the second motor
16 and connecting rod 17, the first motor 14 and the second motor 16 are fixed in motor fixed column 18, and motor fixed column 18 is fixed on street lamp
On the lamppost 05 of 19 lower sections, the two ends of drawstring 15 are respectively connecting to the outer end of the first motor 14 and charging positive electrode plate 02, even
The two ends of bar 17 are respectively connecting to the upper end of the second motor 16 and charging positive electrode plate fixed mount 03, and the 3rd power unit includes the
Three motors 20, the 3rd motor 20 is fixed on charging negative electrode plate fixed mount 08 and is connected to the second rotary shaft 09, the first motor
14th, the second motor 16 and the 3rd motor 20 are respectively connecting to master controller 01.First motor 14, the second motor 16 and the 3rd motor
20 are also not necessarily limited to motor certainly, can be any mechanisms that electric energy can be made to be converted to kinetic energy.
In the present embodiment, the first power unit includes two the first motors 14 and two drawstrings 15, the second power unit
Including two the second motors 16 and two connecting rods 17, two the first motors 14 are relatively fixed in the both sides of motor fixed column 18, two
Bar drawstring 15 is located at the both sides of motor fixed column 18, and the two ends of every drawstring 18 are respectively connecting to one of them He of the first motor 14
The outer end of charging positive electrode plate 02, two the second motors 16 are relatively fixed in the both sides of motor fixed column 18, two 17, connecting rods
In the both sides of motor fixed column 18, the two ends of each connecting rod 17 are respectively connecting to one of them second motor 16 and charging positive electrode
The upper end of plate fixed mount 03.
Further, administration of power supply also includes mains-supplied unit 21, and mains-supplied unit 21 is connected to charging positive electrode
Plate 02 and charging negative electrode plate 07, are provided between mains-supplied unit 21 and charging positive electrode plate 02 and charging negative electrode plate 07
Second charge switch 22, the second charge switch 22 is connected to master controller 01.
Further, induction mechanism also includes the second inductor 23 for sensing the charging current of unmanned plane 11, the second sense
Answer device 23 to be attached in lamppost 05 and be connected to master controller 01.
Further, induction mechanism also includes the 3rd inductor 24 for sensing the payment of unmanned plane 11, the 3rd inductor
24 are attached on lamppost 05 and are connected to master controller 01.
Further, sunshine tracker is provided with solar panels 10, sunshine tracker is connected with master controller 01,
Not shown in figure.
Further, with reference to Fig. 3 and Fig. 4, multiple point-like charging positive poles are provided with charging positive electrode plate 02 and are distributed with
Multiple penetrating circular holes or spherical concave surface 27；Multiple conical protrusions 28 are distributed with charging negative electrode plate 07, are set between raised 28
There is charging negative pole.
Referring to figs. 1 to Fig. 4, the invention also discloses a kind of unmanned plane charging method, the charging method includes：First sensing
Device 12 senses the charge request signal of unmanned plane 11 and sends to master controller 01 induced signal；The control of master controller 01 the
Three motors 20 start to rotate, and the 3rd motor 20 drives charging negative electrode plate 07 and solar charging panel 10 to rotate, and makes charging negative electricity
The direction of pole plate 07 is upward and solar charging panel 10 is directed downward；The leg 25 of unmanned plane 11 drop to charging negative electrode plate
The charging negative pole between negative pole and raised 28 in the gap of the multiple conical protrusions 28 on 07 and as the charge port of unmanned plane 11
Contact connection；On the other hand, when unmanned plane 11 drops to charging negative electrode plate 07, these projections 11 just can be to unmanned plane 11
The level of carrying out is fixed；After the stabilization of unmanned plane 11 drop to charging negative electrode plate 07, sense and pay by the 3rd inductor 24；The
Three inductors 24 unmanned plane are paid the signal for completing and are sent to master controller 01, can on the 3rd inductor 24 in the present embodiment
To be provided with Quick Response Code；Master controller 01 controls the first motor to rotate 14, and the first motor 14 decontrols drawstring 15 makes charging positive electrode
Plate 02 is rotated down until being in horizontality, and control the first charge switch 13 of closure by solar charging panel 10 and charge just
Battery lead plate 02 is connected with charging negative electrode plate 07, or control the second charge switch 22 of closure is by mains-supplied unit 21 and charges just
Battery lead plate 02 is connected with charging negative electrode plate 07；Master controller 01 controls the second motor 16 to rotate, and the second motor 16 is pushed down on
Connecting rod 17, charging positive electrode plate 02 and charging positive electrode plate fixed mount 03 are moved down along the slide rail 06 on lamppost 05；Fill
Penetrating circular hole or spherical concave surface 27 below electric positive electrode plate 02 touch the charge port positive terminal of the wing tip of unmanned plane 11
The spherical on 26 tops, unmanned plane 11 is started to charge up and produces charging current, in addition, penetrating circular hole or spherical concave surface 27 also can use
In fixed unmanned plane 11；Second inductor 23 senses that charging current is produced and sends to master controller 01 this induced signal；
The first motor 14 and second is controlled after the induced signal that the charging current that master controller 01 receives the transmission of the second inductor 23 is produced
Motor 16 carries out self-locking and stops operating；After the charging complete of unmanned plane 11, charging current diminishes or disappears, and the second inductor 23 is felt
Should diminish to charging current or disappear and send to master controller 01 this induced signal；Master controller 01 receives the second inductor
23 charging currents for sending diminish or the induced signal that disappears after, control open the first charge switch 13 by solar charging panel and
Charging positive electrode plate 02 and charging negative electrode plate 07 disconnect, or control open the second charge switch 22 by mains-supplied unit 21 with
Charging positive electrode plate 02 and charging negative electrode plate 07 disconnect；Master controller 01 control the second motor 16 rotate, the second motor 16 to
Upper pulling connecting rod 17, charging positive electrode plate 02 and charging positive electrode plate fixed mount 03 are moved upwards along the slide rail 06 on lamppost 05
Move until touching motor fixed column 18；Master controller 01 controls the first motor 14 to rotate, and the first motor 14 tenses drawstring 15 to be made
Charging positive electrode plate 02 is rotated up until in plumbness；Unmanned plane 11 takes off and departs from charging negative electrode plate 07；Master control
Device 01 controls the 3rd motor 20 to start to rotate, and the 3rd motor 20 drives charging negative electrode plate 07 and solar charging panel 10 to rotate,
Make charging negative electrode plate 07 be directed downward and solar charging panel 10 direction upward；The direction of solar charging panel 10 connects upward
Receive solar energy and convert solar energy into electrical energy；During the direction of solar charging panel 10 receives solar energy upward, pass through
Sunshine tracker, the sunlight intensity that sensing receives the intensity of sunshine and will sense feeds back to master controller 01, always
Controller 01 is rotated by controlling the rotation of the 3rd motor 20 solar charging panel 10 is moved with the sun, makes solar recharging
Plate 10 farthest utilizes sunshine.
With reference to Fig. 5, technical scheme disclosed in the present embodiment can be to be charged with four unmanned planes 29 of rotary wings 30；Charge
Mouth positive terminal 26 is attached to four tops of rotary wings 30, and when unmanned plane 29 is parked, charging positive electrode plate 02 touches wing
On charge port positive terminal 26 when, unmanned plane 29 is started to charge up；Four unmanned plane rotary wings 30 and four unmanned plane legs 31
Four pairs of charge circuits of both positive and negative polarity are just formed, unmanned plane 29 can configure multiple batteries, on the one hand increase the storage of unmanned plane 29
Electric energy power, while unmanned plane 29 can substantially increase charging effect simultaneously for multiple storage batteries charge on charging electrode plate
Rate, improves unmanned plane endurance.
With reference to Fig. 6 and Fig. 7, the top of the charge port positive terminal 26 of the wing upper end of unmanned plane 11 or 29 in the present embodiment
Spherical part 32 can be designed to spring connection, as illustrated, charge port positive terminal 26 is including spherical part 32 and outward
Set part 33, spherical part 32 and coat part 33 connect together, and spherical part 32 is internally provided with buffer spring 34,
The upper end of buffer spring 34 is fixed to inside spherical part 32, the wing upper end of 34 times end in contact unmanned planes of buffer spring 11 or 29,
When charging positive electrode plate 02 is pushed, buffer spring 34 can be with compensator or trimmer pressure, it is to avoid charging positive electrode plate 02 the process for pushing by
In buffer it is excessive and cause unmanned plane 11 or 29 damage.
In the present embodiment, the unmanned plane charging system preferentially takes solar powered, it is impossible to can when taking solar powered
To take mains-supplied, it is ensured that energy-conservation while system can normally be run.In addition, in the present embodiment on the wing of unmanned plane 11 or 29
A round and smooth charge port 35 is respectively designed in the both sides of the charge port positive terminal 26 at end, also there is both sides respectively in this charge port 35
One spring pressuring plate 36, for locking charging plug 37, the spring pressuring plate 36 inside this charge port 35 is directly connected to unmanned plane
The both positive and negative polarity of charge power supply, when charging plug 37 is inserted into charge port 35, all has wire 38, when connecting with the mains just on charging plug 37
Quick charge can be carried out, this charging modes are applied to indoor charging, or have socket Anywhere.
Although the present invention is described in detail above to have used general explanation and specific embodiment, at this
On the basis of invention, it can be made some modifications or improvements, this will be apparent to those skilled in the art.Therefore,
These modifications or improvements, belong to the scope of protection of present invention without departing from theon the basis of the spirit of the present invention.
Claims (10)
1. a kind of unmanned plane charging system, it is characterised in that the charging system includes：
Charging positive electrode mechanism, including：Charging positive electrode plate, charging positive electrode plate fixed mount, the first power unit and second move
Power unit, the charging positive electrode plate is rotatably affixed to the charging positive electrode plate fixed mount outer end by the first rotary shaft,
The charging positive electrode plate fixed mount is slidably mounted to the slide rail being fixed on lamppost, first power along the vertical direction
Unit is connected to the outer end of the charging positive electrode plate, and second power unit is connected to the charging positive electrode plate fixed mount
Upper end；
Charging negative electrode mechanism, including：Charging negative electrode plate, charging negative electrode plate fixed mount and the 3rd power unit, it is described to fill
Electric negative electrode plate is rotatably affixed to the 3rd power unit by the second rotary shaft, and the 3rd power unit is fixed to institute
State on charging negative electrode plate fixed mount, the charging negative electrode plate fixed mount is fixed to the charging positive electrode plate fixed mount lower section
Lamppost on；
Administration of power supply, including it is attached to the solar charging panel at the back side of the charging negative electrode plate；
Induction mechanism, including for sensing the first inductor of unmanned plane charge request signal, first inductor is attached to
On lamppost；
Master controller, is attached in lamppost；
Wherein, the solar charging panel is connected to the charging positive electrode plate and the charging negative electrode plate, the solar energy
The first charge switch, first power are provided between charging panel and the charging positive electrode plate and the charging negative electrode plate
Unit, second power unit, the 3rd power unit, first charge switch and first inductor connect respectively
It is connected to master controller.
2. a kind of unmanned plane charging system as claimed in claim 1, it is characterised in that：First power unit includes first
Motor and drawstring, second power unit include the second motor and connecting rod, and first motor and second motor are fixed
To motor fixed column, on the lamppost that the motor fixed column is fixed on below street lamp, the two ends of the drawstring connect respectively
To the outer end of first motor and the charging positive electrode plate, the two ends of the connecting rod be respectively connecting to second motor and
The upper end of the charging positive electrode plate fixed mount, the 3rd power unit includes the 3rd motor, and the 3rd motor is fixed to
On the charging negative electrode plate fixed mount and it is connected to the second rotary shaft, first motor, second motor and described
Three motors are respectively connecting to master controller.
3. a kind of unmanned plane charging system as claimed in claim 2, it is characterised in that：First power unit includes two
First motor and two drawstrings, second power unit include two the second motors and two connecting rods, described two first electricity
Machine is relatively fixed in the both sides of the motor fixed column, and two drawstrings are located at the both sides of the motor fixed column, every drawing
The two ends of rope are respectively connecting to the outer end of one of them first motor and the charging positive electrode plate, described two second motor phases
Both sides to being fixed on the motor fixed column, described two connecting rods are located at the both sides of the motor fixed column, each connecting rod
Two ends are respectively connecting to the upper end of one of them second motor and the charging positive electrode plate fixed mount.
4. a kind of unmanned plane charging system as claimed in claim 1, it is characterised in that：The administration of power supply is also supplied including civil power
Electric unit, the mains-supplied unit is connected to the charging positive electrode plate and the charging negative electrode plate, the mains-supplied
The second charge switch is provided between unit and the charging positive electrode plate and the charging negative electrode plate, described second charges opens
Connection is connected to master controller.
5. a kind of unmanned plane charging system as claimed in claim 1, it is characterised in that：The induction mechanism is also included for feeling
The second inductor of unmanned plane charging current, second inductor is answered to be attached in the lamppost and be connected to master control
Device.
6. a kind of unmanned plane charging system as claimed in claim 5, it is characterised in that：The induction mechanism is also included for feeling
The 3rd inductor for answering unmanned plane to pay, the 3rd inductor is attached on the lamppost and is connected to master controller.
7. a kind of unmanned plane charging system as claimed in claim 1, it is characterised in that：The sun is provided with the solar panels
Light tracker, the sunshine tracker is connected with the master controller.
8. a kind of unmanned plane charging system as claimed in claim 1, it is characterised in that：It is provided with the charging positive electrode plate
Multiple point-like charging positive poles are simultaneously distributed with multiple penetrating circular holes or spherical concave surface；Multiple circles are distributed with the charging negative electrode plate
Charging negative pole is provided between tapered protrusion, the projection.
9. a kind of unmanned plane charging method, it is characterised in that：The charging method includes：
First inductor senses the charge request signal of unmanned plane and sends to master controller induced signal；
Master controller controls the 3rd motor to start to rotate, and the 3rd motor drives charging negative electrode plate and solar charging panel to rotate,
Make the direction of charging negative electrode plate upward and solar charging panel is directed downward；
The leg of unmanned plane drop in the gap of the multiple conical protrusions on charging negative electrode plate and is charged as unmanned plane
The negative pole of mouth is connected with the charging cathode contact between projection；
After unmanned plane stabilization drop to charging negative electrode plate, sense and pay by the 3rd inductor；
3rd inductor unmanned plane is paid the signal for completing and is sent to master controller；
Master controller controls the first motor to rotate, and the first motor decontrols drawstring is rotated down charging positive electrode plate until in water
Level state, and control the first charge switch of closure to connect solar charging panel and charging positive electrode plate and charging negative electrode plate,
Or control the second charge switch of closure connects mains-supplied unit and charging positive electrode plate and charging negative electrode plate；
Master controller controls the second motor to rotate, and the second motor pushes down on connecting rod, charging positive electrode plate and charging positive electrode plate
Fixed mount is moved down along the slide rail on lamppost；
Penetrating circular hole or spherical concave surface below charging positive electrode plate touch the charge port positive terminal of unmanned plane wing tip
The spherical on top, unmanned plane is started to charge up and produces charging current；
Second inductor senses that charging current is produced and sends to master controller this induced signal；
The first motor and the second electricity are controlled after the induced signal that the charging current that master controller receives the transmission of the second inductor is produced
Machine carries out self-locking and stops operating；
After unmanned plane charging complete, charging current diminishes or disappears, and the second inductor senses that charging current diminishes or disappears simultaneously
This induced signal is sent to master controller；
Master controller receive the transmission of the second inductor charging current diminish or the induced signal that disappears after, control opening first is filled
Electric switch disconnects solar charging panel and charging positive electrode plate and charging negative electrode plate, or control the second charge switch of opening will
Mains-supplied unit disconnects with charging positive electrode plate and charging negative electrode plate；
Master controller controls the second motor to rotate, and the second motor pulls up connecting rod, charging positive electrode plate and charging positive electrode plate
Fixed mount is move upwardly until along the slide rail on lamppost and touches motor fixed column；
Master controller the first motor of control is rotated, and the first motor tenses drawstring rotates up charging positive electrode plate until in vertical
Straight state；
Unmanned plane takes off and departs from charging negative electrode plate；
Master controller controls the 3rd motor to start to rotate, and the 3rd motor drives charging negative electrode plate and solar charging panel to rotate,
Make charging negative electrode plate be directed downward and solar charging panel direction upward；
Solar charging panel direction receives solar energy and converts solar energy into electrical energy upward；
During solar charging panel direction receives solar energy upward, sensed by sunshine tracker and receive sunshine
Intensity and the sunlight intensity that will sense feeds back to master controller, master controller is made too by controlling the rotation of the 3rd motor
Positive energy charging panel is moved and rotated with the sun, solar charging panel is farthest utilized sunshine.
10. a kind of unmanned plane charging streetlamp, it is characterised in that：The charging streetlamp is included as described in any one of claim 1 to 8
Unmanned plane charging system.
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| CN201611154275.6A CN106786866B (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle charging system and method and charging street lamp |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611154275.6A CN106786866B (en) | 2016-12-14 | 2016-12-14 | Unmanned aerial vehicle charging system and method and charging street lamp |
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| CN106786866B CN106786866B (en) | 2023-09-08 |
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| CN108282011A (en) * | 2018-03-21 | 2018-07-13 | 歌尔股份有限公司 | A kind of robot charging method, robot and charging pile |
| CN114228521A (en) * | 2021-12-20 | 2022-03-25 | 歌尔科技有限公司 | Unmanned aerial vehicle equipment and wireless charging device thereof |
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|---|---|
| CN106786866B (en) | 2023-09-08 |
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