CN108263235A - A kind of charging system for electric automobile transmitted electricity using guide rail - Google Patents
A kind of charging system for electric automobile transmitted electricity using guide rail Download PDFInfo
- Publication number
- CN108263235A CN108263235A CN201810112314.9A CN201810112314A CN108263235A CN 108263235 A CN108263235 A CN 108263235A CN 201810112314 A CN201810112314 A CN 201810112314A CN 108263235 A CN108263235 A CN 108263235A
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- fan
- vane
- guide rail
- aircraft
- plate
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- 230000005611 electricity Effects 0.000 title claims abstract description 23
- 230000005540 biological transmission Effects 0.000 claims abstract description 22
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 50
- 238000009434 installation Methods 0.000 claims description 34
- 230000000630 rising effect Effects 0.000 claims description 29
- 229910052742 iron Inorganic materials 0.000 claims description 25
- 238000009413 insulation Methods 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 11
- 238000007789 sealing Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L5/00—Current collectors for power supply lines of electrically-propelled vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60M—POWER SUPPLY LINES, AND DEVICES ALONG RAILS, FOR ELECTRICALLY- PROPELLED VEHICLES
- B60M7/00—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway
- B60M7/003—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway for vehicles using stored power (e.g. charging stations)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- H02J7/0027—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- 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
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention belongs to electric vehicle charging fields, more particularly to a kind of charging system for electric automobile transmitted electricity using guide rail, include multiple electric poles being equidistantly vertically installed at along road by road, it is fixedly mounted on guide rail and the multiple trolley components being slidably connected on guide rail being located on electric pole above road, the terminal pad being connect with electric vehicle and multiple aircraft for being used to carry terminal pad movement.The present invention is arranged on by road, can in time be charged to electric vehicle on road, and not by time restriction, and driver can charge to electric vehicle while driving, and save driver and charge the time waited；It is connected by trolley component with power transmission line and is powered to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered.
Description
Technical field
The invention belongs to electric vehicle charging fields, and in particular to a kind of electric vehicle Charging transmitted electricity using guide rail
System.
Background technology
Electric vehicle has the advantages that prominent the problem of existing simultaneously charging aspect as energy-saving and environment-friendly automobile.It is existing
Charging modes are mainly charging pile, but charging pile, since installation site is fixed, electric vehicle can only rest in charging when charging
Stake is nearby charged；And the time that charging pile needs when charging is long, and electric vehicle can not move when charging.
Invention content
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, it provides a kind of defeated using guide rail
The charging system for electric automobile of electricity.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of electronic vapour transmitted electricity using guide rail
Vehicle charging system includes multiple electric poles being equidistantly vertically installed at along road by road, it is upper to be fixedly mounted on electric pole
Guide rail and multiple trolley components being slidably connected on guide rail above road；
The guide rail includes horizontally disposed traveling rail；The traveling rail upper center forms to position the trolley component
Transmission of electricity mounting rail；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail for being useful for power supply；The traveling rail is close to institute
It states electric pole one end and forms position-limited rail for preventing the trolley component from rolling；
The positioning mounting plate inner wall upper end corresponds to and is installed with contact along trolley component length direction at the transmission guide rail
Draw runner, the contact strip are slidably connected with the transmission guide rail；The traveling plate and the power supply installing plate upper surface are respectively
Motor mounting plate there are one being fixedly connected with；The motor mounting plate side is equipped with multiple advance turbin generators；It is each it is described before
Output shaft end into turbin generator is fixedly connected with the feeder wheel that is useful for making trolley component to advance；The traveling plate and the power supply peace
Loading board, which corresponds to, forms multiple square holes for being used to pass through for the feeder wheel at each feeder wheel；The power supply installing plate position
In far from the electric pole side；On trolley length direction described in the traveling plate upper edge is equipped in the multiple and position-limited rail
End face rolls the roller of connection；The feeding pannel upper surface is fixedly connected with the second electromagnet；It is installed on second electromagnet
There is the current electrode of annular；
The trolley component includes the positioning mounting plate being slidably connected on the guide rail, is integrally formed respectively in positioning mounting plate
Lower end both sides and horizontally disposed power supply installing plate and traveling plate and the power supply being fixedly connected on the power supply installing plate
Disk；
Electromobile at top is equipped with wire spool；The charging wire for being useful for charging to electric vehicle is pierced by rear side of the wire spool；
The charging wire other end is connected with terminal pad；The wire spool upper end, which is fixedly connected with, parks disk；The terminal pad moves
It is connected to described park in disk or the trolley component；Further include multiple aircraft for being used to carry terminal pad movement.
Preferably：Each electric pole includes the upright bar of vertical direction setting；The upright bar upper end, which is fixed, to be connected
It is connected to towards the horizontally disposed cross bar of road direction；The crossbar end is fixedly connected with the guide rail；
Feeding pannel upper surface center is painted with for the first telltale mark for the Aerial vehicle position；
Described park is fixedly connected with ring electromagnet on disk；The insulation tank of annular is installed on the ring electromagnet；It is described
The controller of ring electromagnet is mounted on electric vehicle；
The terminal pad is circular disk；The terminal pad upper end is equipped with multigroup iron block slot, and every group of iron block slot is four installations
There is the circular groove of iron block；The terminal pad lower end is equipped with the annular iron block of annular；The annular iron block lower end be equipped with for
First receiving electrode of the feeding pannel electrical connection；
The aircraft, trolley component, electric vehicle are connected by wireless signal and the server communication of system.
Preferably：The aircraft includes main part, and the main part includes the fan installation of tubular
Portion, the connecting tube for four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion and is connected to
Each connecting tube outer end and go out vane with what corresponding position connecting tube was connected；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving wind is installed on the upper bracket
Fan；It is located in the fan mounting portion below connecting tube and is connected with lower carriage, lower driving fan is installed on the lower carriage；
The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion
Diameter is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade diameter of upper driving fan is more than lower driving wind
The fan blade diameter of fan, the interior wind pressure superatmospheric between upper driving fan and lower driving fan of the fan mounting portion,
Wind pressure is formed in vane so that going out；
It is described go out vane include the vane upper shell of sealed connection and vane lower housing, the vane lower housing inner circumferential upper end into
Type has interior curved wall, and there are one air outlet guard board, air outlet guard board upper end and wind by the connection of multiple dowels for the inner circumferential of the interior curved wall
Ring upper shell inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board
The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction and formed
The angle of 5-20 degree, and the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane generates
Direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting group in each connecting tube
Part includes motor, coaxially connected screw rod and the valve plate being connect with screw flight with motor output shaft；The valve plate top
Close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube for periphery；The connecting tube internal upper part into
Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane
The valve plate guide rod that plate is slidably connected；Upper end direction to go out the inclined baffle in vane direction there are one the connections of lower part in the connecting tube,
The conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly form on air intake cover strip into
Air port；
The main part is tightly connected and forms for upper shell and lower housing；
The lower, outer perimeter of the fan mounting portion is battery installation section, is connected in battery installation section and is electrically connected with control circuit board
Accumulator；Positioned at the top of battery installation section for a circuit board installation cavity on the fan mounting portion, the control circuit
Plate is mounted in circuit board installation cavity, and there are one the cover boards of annular for the circuit board installation cavity lower end connection；The circuit board peace
The upper surface behaveing affectedly uniformly forms the air inlet hole connected in fan mounting portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is equipped with the camera being electrically connected with control circuit board；
It is each it is described go out position of the vane inner circumferential far from connecting tube form Holder joint of rising and falling, it is each in each Holder joint of rising and falling
There are one undercarriages for connection；The undercarriage includes the supporting rod being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet far from Holder joint one end of rising and falling on bar, the supporting rod is downwards；It is installed below first electromagnet
It is useful for the second receiving electrode to charge to aircraft.
Preferably：Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint of rising and falling, it is each
Respectively there are one undercarriages for connection in the Holder joint of rising and falling；The undercarriage, which includes, to be fixedly connected and passes through with Holder joint of rising and falling
Holder joint of rising and falling is with going out the connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connecting tube
Body is connected to the first electricity far from Holder joint one end of rising and falling on supporting rod close to the supporting rod for Holder joint one end rotation connection of rising and falling
Magnet and the respectively connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod；Installation is useful below first electromagnet
In the second receiving electrode to charge to aircraft；
The connection pipe body forms hinged seat close to the Holder joint one end wall that rises and falls, and described supporting rod one end is rotated with hinged seat
Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position is connected with hinged
Head, described connecting rod one end are rotatablely connected with articulated joint, and side wall of the connection pipe body far from Holder joint one end of rising and falling forms confession
The strip shape gob that articulated joint passes through；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap
Inner end is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against piston respectively
Between sealing cap inner end；The connecting rod tank that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod.
Preferably：The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out the axial direction of vane with
The angle of 5-20 degree is formed between horizontal direction, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and upper driving
The rotation direction of the fan blade of fan is opposite.
Preferably：Diameter of a circle where the center line of second electromagnet, ring electromagnet and annular iron block
Circumscribed circle diameter where the rectangle that corresponding first electromagnet is connected to after being unfolded with the aircraft support bar is equal.
Preferably：The current electrode, the first receiving electrode respectively include two annular electros being arranged concentrically
Polar ring.
Preferably：Speed limit 40km/h during the electric vehicle charging.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is installed along by road, is carried by aircraft
Terminal pad moves, and so as to make to establish connection between transmission guide rail and electric vehicle, and then charges to electric vehicle.When not carrying out
During charging tasks, terminal pad, which is parked in, parks on disk, makes terminal pad and to park disk by the way that annular iron block and ring electromagnet are attracting
Connection, first receiving electrode is plugged in the insulation tank, while the first electromagnet without the aircraft under aerial mission
With the second electromagnet is attracting that aircraft is made to be connect with feeding pannel, current electrode connect with the second receiving electrode so as to aircraft into
Row charging.When electric vehicle not enough power supply, below electric automobile during traveling to guide rail, and charge request is sent to server
Signal after server receives charge request signal, according to the location of electric vehicle, and feeds back electric vehicle and opens to driving
Below trolley component that direction front end remains static, at the same by server to rest in the trolley component or away from
The aircraft nearest from the trolley component sends instruction, and aircraft is artificially controlled by the camera below being mounted on and flies to this
The terminal pad upper end that electric vehicle is connected, the ring electromagnet during the aircraft declines on the electric vehicle break
Electricity, the aircraft is directed at the second telltale mark by camera, while aircraft rotates horizontally, and makes four the first electromagnet
With one group of iron block slot is attracting that aircraft is made to be connected with terminal pad；Wire spool work on server controls electric vehicle makes charging
Line extends, while aircraft is controlled to carry terminal pad and is moved to above trolley component, at this time the second electromagnet in trolley component
It is powered, control aircraft, which is directed at the decline of the first telltale mark, makes current electrode be connect with the first receiving electrode, so as to make electronic vapour
Vehicle charges；The advance turbin generator work of trolley component is controlled in charging process, trolley component is made to be moved with electric automobile during traveling；
Carry-on first electromagnet is then controlled to power off, aircraft disengages with terminal pad and carries out other tasks.When electric vehicle fills
Aircraft is controlled to be connected after being moved to above trolley component with terminal pad after electricity, the second electromagnet in trolley component breaks
Electricity, terminal pad and charging board disconnect, and subsequent aircraft carries terminal pad and parks to parking on disk.
The present invention is arranged on by road, can in time be charged to electric vehicle on road, not by time restriction, and be driven
Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；By trolley component with it is defeated
Conductance rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft is taken
Band connection disk charges to electric vehicle, security risk when can avoid manual powered；When electric vehicle starts to charge up, flight
Device is disconnected with terminal pad, can more rationally using aircraft and be saved compared in the case of aircraft and terminal pad one
About cost；The disk of parking is fixedly connected on electric vehicle, to store the terminal pad under non-charged state；Not to electronic
The trolley component that automobile is carried out under charged state charges to the aircraft under off working state, and is stored to the offer of aircraft
Place.
Description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is the structure diagram of electric pole and guide rail.
Fig. 3 is the structure diagram of electric vehicle charged state.
Fig. 4 is the structure diagram of the non-charged state of electric vehicle.
Fig. 5, Fig. 6 are the structure diagrams of trolley component.
Fig. 7, Fig. 8 are the structure diagrams of terminal pad.
Structure diagram when Fig. 9 is aircraft grounding state or carries terminal pad.
Figure 10 is the structure diagram under aircraft free flight state.
Figure 11 is the schematic cross-sectional view of aircraft.
Figure 12 is the A portions schematic enlarged-scale view of Figure 11.
Figure 13 is the B portions schematic enlarged-scale view of Figure 11.
The structure diagram of each component that Figure 14 is upper shell and is connect with upper shell.
Figure 15 is the structure diagram of lower housing section.
Figure 16 is the schematic cross-sectional view of lower housing section.
Figure 17 is the schematic cross-sectional view of undercarriage part.
Figure 18 is the decomposition texture schematic diagram of undercarriage part.
1st, electric pole；11st, mobile jib；12nd, cross bar；2nd, trolley component；21st, positioning mounting plate；211st, contact strip；22nd, it supplies
Electric installing plate；221st, the first telltale mark；23rd, feeding pannel；231st, the second electromagnet；232nd, current electrode；24th, feeder wheel；25、
Advance turbin generator；26th, motor mounting plate；27th, roller；28th, square hole；29th, traveling plate；31st, wire spool；311st, charging wire；32nd, stop
Sale at reduced prices；321st, ring electromagnet；322nd, insulation tank；323rd, the second telltale mark；4th, terminal pad；41st, iron block slot；42nd, annular iron
Block；43rd, the first receiving electrode；5th, aircraft；51st, main part；51a, upper shell；51b, lower housing；510th, fan mounting portion；
5101st, upper bracket；5102nd, lower carriage；5103rd, battery installation section；5104th, circuit board installation cavity；5105th, air inlet hole；5106th, it arranges
Air holes；5107th, camera；511st, go out vane；5110th, it rises and falls Holder joint；5111st, vane upper shell；5112nd, vane lower housing；
51121st, interior curved wall；51122nd, dowel；51123rd, air outlet guard board；51124th, training wall；512nd, connecting tube；5121st, motor is pacified
Loading board；5122nd, valve plate guide rod；5123rd, baffle；513rd, cover board；52nd, accumulator；53rd, undercarriage；531st, connection pipe body；5311、
Hinged seat；5312nd, strip shape gob；532nd, sliding tube；5321st, piston；5322nd, articulated joint；533rd, sealing cap；5331st, spring positioning
Bar；534th, connecting rod；535th, supporting rod；5351st, connecting rod tank；536th, the first electromagnet；5361st, the second receiving electrode；537th, bullet
Spring；54th, air intake cover；551st, upper driving fan；552nd, lower driving fan；56th, adjusting part；561st, motor；562nd, screw rod；563、
Valve plate；57th, control circuit board；6th, guide rail；61st, traveling rail；62nd, position-limited rail；63rd, transmission of electricity mounting rail；64th, transmission guide rail.
Specific embodiment
Embodiment 1
According to Fig. 1 to Figure 16, the present embodiment is a kind of charging system for electric automobile transmitted electricity using guide rail, is included multiple
The electric pole 1 being equidistantly vertically installed at along road by road, be fixedly mounted on electric pole be located at road above guide rail 6 and
Multiple trolley components 2 being slidably connected on guide rail.
The trolley component includes the positioning mounting plate 21 being slidably connected on the guide rail, is integrally formed is positioning respectively
Installing plate lower end both sides and horizontally disposed power supply installing plate 22 and traveling plate 29 and it is fixedly connected on the power supply installing plate
On feeding pannel 23.
Electromobile at top is equipped with wire spool 31；It is pierced by rear side of the wire spool and is useful for filling to what electric vehicle charged
Electric wire 311；The charging wire other end is connected with terminal pad 4；The wire spool upper end, which is fixedly connected with, parks disk 32；The company
It connects disk and is mobily connected in described park on disk or the trolley；Further include multiple aircraft 5 for being used to carry terminal pad movement.
Each electric pole includes the upright bar 11 of vertical direction setting；The upright bar upper end is fixedly connected with towards road
The horizontally disposed cross bar 12 in direction；The crossbar end is fixedly connected with the guide rail.
The guide rail includes horizontally disposed traveling rail 61；The traveling rail upper center forms described small for positioning
The transmission of electricity mounting rail 63 of vehicle component；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail 64 for being useful for power supply；The row
The position-limited rail 62 for preventing the trolley component from rolling is formed close to described electric pole one end into rail.
The positioning mounting plate inner wall upper end corresponds to and is installed at the transmission guide rail along trolley component length direction
Contact strip 211, the contact strip are slidably connected with the transmission guide rail；The traveling plate and the power supply installing plate upper end
Face is respectively fixedly connected with there are one motor mounting plate 26；The motor mounting plate side is equipped with multiple advance turbin generators 25；
The output shaft end of each advance turbin generator is fixedly connected with the feeder wheel 24 for being useful for that trolley component is made to advance；The traveling plate
It is corresponded to the power supply installing plate and multiple square holes 28 for being used to pass through for the feeder wheel is formed at each feeder wheel；Institute
It states power supply installing plate and is located remotely from the electric pole side；Trolley length direction described in the traveling plate upper edge be equipped with it is multiple with
Upper surface rolls the roller 27 of connection in the position-limited rail；The feeding pannel upper surface is fixedly connected with the second electromagnet 231；Institute
State the current electrode 232 that annular is equipped on the second electromagnet；Feeding pannel upper surface center is painted with being used to fly for described
First telltale mark 221 of row device positioning.The position-limited rail offsets with the roller slip, prevents trolley component because of feeding pannel one
Side preponderance and roll, and therefore can make between the contact strip and the transmission guide rail, the feeder wheel and institute
It states and effectively contacts between traveling rail；The advance turbin generator controls the feeder wheel rotation to make the trolley component along the guide rail
It is mobile.
When electric vehicle charges, the terminal pad is connect with the feeding pannel, and electric current is exported from transmission guide rail, is passed through successively
Contact strip is transferred to feeding pannel, charges after terminal pad is transferred to charging wire to electric vehicle after.
The aircraft includes main part 51, and the main part includes the fan mounting portion 510 of tubular, is connected to
Fan mounting portion periphery and the connecting tube 512 for four equidistant arrangements being connected with fan mounting portion and it is connected to each company
It takes over outer end and what is be connected with corresponding position connecting tube goes out vane 511.
It is located in the fan mounting portion above connecting tube and is connected with upper bracket 5101, is equipped on the upper bracket
Driving fan 551；It is located in the fan mounting portion below connecting tube and is connected with lower carriage 5102, is installed on the lower carriage
There is lower driving fan 552；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install
The internal diameter of driving fan part is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade of upper driving fan
Diameter is more than the fan blade diameter of lower driving fan, and the fan mounting portion is interior between upper driving fan and lower driving fan
Wind pressure superatmospheric so that go out and wind pressure is formed in vane.
It is described go out vane include the vane upper shell 5111 of sealed connection and vane lower housing 5112, the vane lower casing
Internal Zhou Shangduan forms interior curved wall 51121, and there are one air outlet guard boards by the connection of multiple dowels for the inner circumferential of the interior curved wall
51123, air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；On being formed between the interior curved wall and air outlet guard board
Narrow outlet air gap under width, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing is located at outlet air
The lower section in gap is training wall 51124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree.
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction
The angle of 5-20 degree is formed, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and the fan blade of upper driving fan
Rotation direction is opposite.
It is equipped with to adjust the adjusting part 56 that corresponding position goes out vane outlet air speed in each connecting tube, it is described
Adjusting part includes motor 561, the screw rod 562 coaxially connected with motor output shaft and the valve plate being connect with screw flight
563；For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；Institute
It states connecting tube internal upper part to form that the motor mounting plate 5121 of the motor is installed, the motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod 5122 being slidably connected with the valve plate；There are one upper end courts for lower part connection in the connecting tube
To the inclined baffle 5123 in vane direction is gone out, the conducting adjustable air passage of area is formed between the baffle and valve plate.
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board 57.
The main part upper end connects the air intake cover 54 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover
The air inlet of shape.
The main part is tightly connected for upper shell 51a and lower housing 51b and forms.
Aircraft provides driving force, upper driving fan production by upper driving fan, the lower driving fan in fan mounting portion
Raw fraction from it is each go out vane outlet air gap blow out downwards, and combine adjusting part adjustment each go out vane outlet air
Speed, so as to fulfill the horizontal flight or steering of aircraft, due to be located at aircraft periphery it is each go out vane only play tune
The effect of whole attitude of flight vehicle without the fan for being provided with power, goes out when vane generates touching with foreign object and does not easily lead to aircraft
Out of control or generate injury to human or animal, safety is good.
Further, it is described go out vane outlet air gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward together, flown in this way
When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out the axial direction and level of vane
The angle of 5-20 degree is formed between direction, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and upper driving fan
Fan blade rotation direction it is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane enough offsets drive
The reaction force that dynamic fan and lower driving fan generate when rotating；Also, change outlet air by adjusting each adjusting part simultaneously
Ring goes out wind velocity, it can be achieved that the whole forward or reverse of aircraft.Make one by adjusting one or two adjusting part
Or two go out vane go out wind velocity, it can be achieved that aircraft can drive aircraft in level in this way generally in heeling condition
It flies in direction.
The lower, outer perimeter of the fan mounting portion is battery installation section 5103, is connected in battery installation section and control circuit
The accumulator 52 of plate electrical connection；The top for being located at battery installation section on the fan mounting portion is a circuit board installation cavity
5104, the control circuit board 57 is mounted in circuit board installation cavity, and there are one annulars for the circuit board installation cavity lower end connection
Cover board 513；The upper surface of the circuit board installation cavity uniformly forms the air inlet hole 5105 connected in fan mounting portion, institute
The lateral wall for stating circuit board installation cavity uniformly forms vent 5106；The lower driving fan lower end is equipped with and control circuit
The camera 5107 of plate electrical connection.
Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint 5110 of rising and falling, each undercarriage
Respectively there are one undercarriages 53 for connection on connector；The undercarriage includes the supporting rod 535 being fixedly connected with the Holder joint of rising and falling
And the first electromagnet 536 far from Holder joint one end of rising and falling on supporting rod is connected to, the supporting rod is downwards；Described
The second receiving electrode 5361 for charging to aircraft is installed below one electromagnet.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, and the control circuit board is risen
To cooling effect.
Described park is fixedly connected with ring electromagnet 321 on disk；The insulation of annular is installed on the ring electromagnet
Slot 322；The disk upper surface center of parking is painted with for the second telltale mark 323 for the Aerial vehicle position；The ring
The controller of shape electromagnet is mounted on electric vehicle.
The terminal pad is carried by the aircraft and moves to connect with the feeding pannel and charged to electric vehicle.Work as institute
When stating aircraft and carrying terminal pad movement, the aircraft is connect with the terminal pad upper end；When electric vehicle charges, institute
Feeding pannel is stated to connect with the terminal pad lower end.
The terminal pad is annular；The terminal pad upper end, which corresponds to, is equipped with multigroup iron block slot at first electromagnet,
Every group of iron block slot is four circular grooves for being equipped with iron block, the circular groove be unfolded respectively with the aircraft after first electromagnet
It is corresponding；The terminal pad lower end is equipped with the annular iron block 42 of annular；The annular iron block lower end be equipped with for the confession
First receiving electrode 43 of electroplax electrical connection.
Diameter of a circle and the aircraft branch where the center line of second electromagnet, ring electromagnet and annular iron block
Circumscribed circle diameter where the rectangle that corresponding first electromagnet is connected to after strut expansion is equal.
The aircraft, trolley component, electric vehicle are connected by wireless signal and the server communication of system.
The current electrode, the first receiving electrode respectively include two annular electro polar rings being arranged concentrically.
Speed limit 40km/h during the electric vehicle charging.
The present invention is installed along by road, and carrying terminal pad by aircraft moves, so as to make transmission guide rail and electric vehicle
Between establish connection, and then to electric vehicle charge.When not having to carry out charging tasks, terminal pad, which is parked in, parks on disk, leads to
It crosses annular iron block and ring electromagnet is attracting that terminal pad is made to be connect with parking disk, first receiving electrode is plugged on the insulation
In slot, while the first electromagnet without the aircraft under aerial mission and the second electromagnet is attracting connects aircraft and feeding pannel
It connects, current electrode connect to charge to aircraft with the second receiving electrode.When electric vehicle not enough power supply, electronic vapour
Vehicle is travelled to guide rail, and the signal of charge request, after server receives charge request signal, root are sent to server
According to the location of electric vehicle, and feed back electric vehicle and open under the trolley component to remain static to direction of traffic front end
Side, at the same by server to rest in the trolley component or the aircraft nearest apart from the trolley component send instruction,
Aircraft is described to fly by being mounted on the terminal pad upper end that the camera of lower section artificially controls and the electric vehicle that flies to is connected
Ring electromagnet power-off during row device declines on the electric vehicle, the aircraft pass through the second positioning of camera alignment
Label, while aircraft rotates horizontally, and makes four the first electromagnet and one group of iron block slot is attracting makes aircraft and terminal pad phase
Connection；Wire spool work on server controls electric vehicle extends charging wire, while aircraft is controlled to carry terminal pad and is moved
It moves to above trolley component, the second electromagnet in trolley component is powered at this time, and control aircraft is aligned under the first telltale mark
Drop makes current electrode be connect with the first receiving electrode, so as to which electric vehicle be made to charge；Before trolley component being controlled in charging process
It works into turbin generator, trolley component is made to be moved with electric automobile during traveling；Carry-on first electromagnet is then controlled to power off,
Aircraft disengages with terminal pad and carries out other tasks.Aircraft is controlled to be moved in trolley component after electric vehicle charges
Fang Houyu terminal pads are connected, and the second electromagnet power-off in trolley component, terminal pad is disconnected with charging board, and subsequent aircraft is taken
Band connection disk is parked to parking on disk.
The present invention is arranged on by road, can in time be charged to electric vehicle on road, not by time restriction, and be driven
Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；By trolley component with it is defeated
Conductance rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft is taken
Band connection disk charges to electric vehicle, security risk when can avoid manual powered；When electric vehicle starts to charge up, flight
Device is disconnected with terminal pad, can more rationally using aircraft and be saved compared in the case of aircraft and terminal pad one
About cost；The disk of parking is fixedly connected on electric vehicle, to store the terminal pad under non-charged state；Not to electronic
The trolley component that automobile is carried out under charged state charges to the aircraft under off working state, and is stored to the offer of aircraft
Place.
Embodiment 2
According to Figure 17 to Figure 18, the present embodiment has done following improvement on the basis of embodiment 1：Go out in vane described in each
Week, the position far from connecting tube formed Holder joint 5110 of rising and falling, and respectively there are one undercarriages for connection in each Holder joint of rising and falling
53；The undercarriage, which includes, to be fixedly connected with Holder joint of rising and falling and by Holder joint of rising and falling with going out the company being connected inside vane
Take over body 531, the sliding tube 532 being slidably mounted in connection pipe body connect with connection pipe body close to Holder joint one end rotation of rising and falling
The supporting rod 535 connect, be connected on supporting rod far from rise and fall Holder joint one end the first electromagnet 536 and respectively with slip
The connecting rod 534 being rotatablely connected in the middle part of pipe, in the middle part of supporting rod；It is equipped with to charge to aircraft below first electromagnet
Second receiving electrode 5361.
The connection pipe body forms hinged seat 5311, described supporting rod one end and hinge close to the Holder joint one end wall that rises and falls
Joint chair is rotatablely connected；The sliding tube is connected with piston 5321, the slip pipe outer wall middle part position close to Holder joint one end of rising and falling
It puts and is connected with articulated joint 5322, described connecting rod one end is rotatablely connected with articulated joint, and the connection pipe body is far from Holder joint one of rising and falling
The side wall at end forms the strip shape gob 5312 passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling, which is fixed, to be connected
Sealing cap 533 is connected to, the inner end of sealing cap is connected with spring positioning bar 5331, spring is arranged on the spring positioning bar
537, the both ends of the spring is against respectively between piston and sealing cap inner end；It is formed on the supporting rod and packs up shape in supporting rod
The connecting rod tank 5351 of the connecting rod is accommodated during state.
The supporting rod is in unfolded state when the spring is in extended configuration, and the upper driving fan is in work shape
After state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The undercarriage is with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, goes out
Wind pressure in vane makes piston be moved together with sliding tube to sealing cap one end, so as to which sliding tube be made to drive connecting rod one end to sealing cap
Direction is moved, so as to which supporting rod lower end be made also to be rotated to sealing cap one end, so as to which undercarriage be made to be in collapsed state.Work as aircraft
During landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved together with piston toward hinged seat direction, so as to make sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, so as to which supporting rod lower end be made to turn to extreme position to hinged seat one end, so as to
Undercarriage is made to be in unfolded state.
The strip shape gob plays the role of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch
After length, supporting rod turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each supporting rod is equal
In stable state.Aircraft is carried in the moving process of terminal pad, since the first electromagnet and iron block slot are attracting, but goes out vane
The power that interior wind pressure generates is insufficient to allow supporting rod to pack up.
Claims (5)
1. a kind of charging system for electric automobile transmitted electricity using guide rail, it is characterised in that：It is multiple equidistantly vertical along road to include
Electric pole by road, is fixedly mounted on the guide rail being located on electric pole above road and multiple be slidably connected at is led
Trolley component on rail；
The guide rail includes horizontally disposed traveling rail；The traveling rail upper center forms to position the trolley component
Transmission of electricity mounting rail；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail for being useful for power supply；The traveling rail is close to institute
It states electric pole one end and forms position-limited rail for preventing the trolley component from rolling；
The trolley component includes the positioning mounting plate being slidably connected on the guide rail, is integrally formed respectively in positioning mounting plate
Lower end both sides and horizontally disposed power supply installing plate and traveling plate and the power supply being fixedly connected on the power supply installing plate
Disk；The positioning mounting plate inner wall upper end corresponds to and is installed with contact cunning along trolley component length direction at the transmission guide rail
Item, the contact strip are slidably connected with the transmission guide rail；The traveling plate and the power supply installing plate upper surface are respectively equal
Motor mounting plate there are one being fixedly connected；The motor mounting plate side is equipped with multiple advance turbin generators；Each advance
The output shaft end of turbin generator is fixedly connected with the feeder wheel for being useful for that trolley component is made to advance；The traveling plate and the power supply installation
Plate, which corresponds to, forms multiple square holes for being used to pass through for the feeder wheel at each feeder wheel；The power supply installing plate is located at
Far from the electric pole side；Trolley length direction described in the traveling plate upper edge is equipped with upper end in the multiple and position-limited rail
Face rolls the roller of connection；The feeding pannel upper surface is fixedly connected with the second electromagnet；It is equipped on second electromagnet
The current electrode of annular；
Electromobile at top is equipped with wire spool；The charging wire for being useful for charging to electric vehicle is pierced by rear side of the wire spool；
The charging wire other end is connected with terminal pad；The wire spool upper end, which is fixedly connected with, parks disk；The terminal pad moves
It is connected to described park in disk or the trolley component；Further include multiple aircraft for being used to carry terminal pad movement；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan installation
Portion periphery and the connecting tube for four equidistant arrangements being connected with fan mounting portion and be connected to each connecting tube outer end and with
What corresponding position connecting tube was connected goes out vane；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving wind is installed on the upper bracket
Fan；It is located in the fan mounting portion below connecting tube and is connected with lower carriage, lower driving fan is installed on the lower carriage；
The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion
Diameter is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade diameter of upper driving fan is more than lower driving wind
The fan blade diameter of fan, the interior wind pressure superatmospheric between upper driving fan and lower driving fan of the fan mounting portion,
Wind pressure is formed in vane so that going out；
It is described go out vane include the vane upper shell of sealed connection and vane lower housing, the vane lower housing inner circumferential upper end into
Type has interior curved wall, and there are one air outlet guard board, air outlet guard board upper end and wind by the connection of multiple dowels for the inner circumferential of the interior curved wall
Ring upper shell inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board
The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction and formed
The angle of 5-20 degree, and the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane generates
Direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting group in each connecting tube
Part includes motor, coaxially connected screw rod and the valve plate being connect with screw flight with motor output shaft；The valve plate top
Close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube for periphery；The connecting tube internal upper part into
Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane
The valve plate guide rod that plate is slidably connected；Upper end direction to go out the inclined baffle in vane direction there are one the connections of lower part in the connecting tube,
The conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly form on air intake cover strip into
Air port；
The main part is tightly connected and forms for upper shell and lower housing；
The lower, outer perimeter of the fan mounting portion is battery installation section, is connected in battery installation section and is electrically connected with control circuit board
Accumulator；Positioned at the top of battery installation section for a circuit board installation cavity on the fan mounting portion, the control circuit
Plate is mounted in circuit board installation cavity, and there are one the cover boards of annular for the circuit board installation cavity lower end connection；The circuit board peace
The upper surface behaveing affectedly uniformly forms the air inlet hole connected in fan mounting portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is equipped with the camera being electrically connected with control circuit board；
It is each it is described go out position of the vane inner circumferential far from connecting tube form Holder joint of rising and falling, it is each in each Holder joint of rising and falling
There are one undercarriages for connection；The undercarriage includes the supporting rod being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet far from Holder joint one end of rising and falling on bar, the supporting rod is downwards；It is installed below first electromagnet
It is useful for the second receiving electrode to charge to aircraft.
2. a kind of charging system for electric automobile transmitted electricity using guide rail as described in claim 1, it is characterised in that：It is each described
Electric pole includes the upright bar of vertical direction setting；The upright bar upper end is fixedly connected with towards the horizontally disposed horizontal stroke of road direction
Bar；The crossbar end is fixedly connected with the guide rail；
Feeding pannel upper surface center is painted with for the first telltale mark for the Aerial vehicle position；
Described park is fixedly connected with ring electromagnet on disk；The insulation tank of annular is installed on the ring electromagnet；It is described
The controller of ring electromagnet is mounted on electric vehicle；
The terminal pad is circular disk；The terminal pad upper end is equipped with multigroup iron block slot, and every group of iron block slot is four installations
There is the circular groove of iron block；The terminal pad lower end is equipped with the annular iron block of annular；The annular iron block lower end be equipped with for
First receiving electrode of the feeding pannel electrical connection；
The aircraft, trolley component, electric vehicle are connected by wireless signal and the server communication of system.
3. a kind of charging system for electric automobile transmitted electricity using guide rail as described in claim 1, it is characterised in that：Described second
Diameter of a circle where the center line of electromagnet, ring electromagnet and annular iron block corresponding with after aircraft support bar expansion the
Circumscribed circle diameter where the rectangle that one electromagnet is connected to is equal.
4. a kind of charging system for electric automobile transmitted electricity using guide rail as described in claim 1, it is characterised in that：The power supply
Electrode, the first receiving electrode respectively include two annular electro polar rings being arranged concentrically.
5. a kind of charging system for electric automobile transmitted electricity using guide rail as described in claim 1, it is characterised in that：It is described electronic
Speed limit 40km/h when automobile charges.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810112314.9A CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488123.8A CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
| CN201810112314.9A CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710488123.8A Division CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
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| Publication Number | Publication Date |
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| CN108263235A true CN108263235A (en) | 2018-07-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810112314.9A Withdrawn CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
| CN201710488123.8A Withdrawn CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
| CN201810112311.5A Withdrawn CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710488123.8A Withdrawn CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
| CN201810112311.5A Withdrawn CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110481354A (en) * | 2019-06-06 | 2019-11-22 | 上海荣灵电力科技有限公司 | Power supply system and its method of supplying power to based on electric pole charging unit |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106740212B (en) * | 2016-12-29 | 2023-10-24 | 重庆金澳机械制造有限公司 | Electric vehicle charging system |
| CN110667417A (en) * | 2019-09-23 | 2020-01-10 | 洛阳嘉盛电源科技有限公司 | Integrated pantograph charging system |
| CN110937126B (en) * | 2019-12-20 | 2021-02-02 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
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| FR2863958B1 (en) * | 2003-12-18 | 2006-03-17 | Hubert Laridant | DEVICE FOR GUIDING AND ELECTRICALLY POWERING THE GROUND OF A VEHICLE BY A CHUTE |
| CN201102628Y (en) * | 2007-09-10 | 2008-08-20 | 新疆生产建设兵团建筑工程科学技术研究院有限责任公司 | Connecting line power aerial vehicle |
| US8978905B2 (en) * | 2010-07-02 | 2015-03-17 | Liko Research & Development Ab | Lift systems with continuous in-rail charging |
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| DE102012013238A1 (en) * | 2012-06-21 | 2013-03-21 | Daimler Ag | Charging station for use in parking and charging device for electrically charging rechargeable battery of hybrid vehicle, has charging unit electrically connected with power transmission unit formed for connecting to rechargeable battery |
| CN103935266B (en) * | 2014-04-08 | 2016-08-17 | 福州开发区和世林实业发展有限公司 | Driving electric supply installation |
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| CN106335400B (en) * | 2016-09-22 | 2018-08-03 | 提前 | A kind of charging system for electric automobile |
| CN106515495B (en) * | 2016-12-03 | 2019-05-10 | 宝鸡中高创新研究院有限公司 | A kind of electric automobile charging pile and charging system |
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2017
- 2017-06-23 CN CN201810112314.9A patent/CN108263235A/en not_active Withdrawn
- 2017-06-23 CN CN201710488123.8A patent/CN107264316A/en not_active Withdrawn
- 2017-06-23 CN CN201810112311.5A patent/CN108237922A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481354A (en) * | 2019-06-06 | 2019-11-22 | 上海荣灵电力科技有限公司 | Power supply system and its method of supplying power to based on electric pole charging unit |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108237922A (en) | 2018-07-03 |
| CN107264316A (en) | 2017-10-20 |
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Application publication date: 20180710 |