CN108189687A - A kind of electric vehicle - Google Patents

A kind of electric vehicle Download PDF

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Publication number
CN108189687A
CN108189687A CN201711448505.4A CN201711448505A CN108189687A CN 108189687 A CN108189687 A CN 108189687A CN 201711448505 A CN201711448505 A CN 201711448505A CN 108189687 A CN108189687 A CN 108189687A
Authority
CN
China
Prior art keywords
vane
fan
mounting portion
aircraft
guide rail
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN201711448505.4A
Other languages
Chinese (zh)
Inventor
虞丽丽
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wenzhou Rui Chu Technology Co Ltd
Original Assignee
Wenzhou Rui Chu Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wenzhou Rui Chu Technology Co Ltd filed Critical Wenzhou Rui Chu Technology Co Ltd
Priority to CN201711448505.4A priority Critical patent/CN108189687A/en
Publication of CN108189687A publication Critical patent/CN108189687A/en
Withdrawn legal-status Critical Current

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Classifications

    • 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
    • B60L53/60—Monitoring or controlling 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
    • B60L53/30—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
    • 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
    • B60L53/32—Constructional details of charging stations by charging in short intervals along the itinerary, e.g. during short stops
    • 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
    • B61—RAILWAYS
    • B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
    • B61B13/00—Other railway systems
    • 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
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/62—Spring shock-absorbers; Springs
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • 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)
  • Transportation (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

The invention discloses a kind of electric vehicles, include car body and the aircraft being connect by conducting wire with car body；Car body top installation is there are one wire-winding unit, and wire-winding unit includes Wiinding cartridge, the box cover of the wire spool being rotatably installed in Wiinding cartridge and the magnetic material for being connected to Wiinding cartridge upper end；There are one coiling electric motors for installation in Wiinding cartridge；For the installation of Wiinding cartridge bottom there are two the annular electrode a that is arranged concentrically, the lower face of wire spool is equipped with the annular electrode b electrically connected with two annular electrode a slips, and the accumulator of annular electrode a and electric vehicle electrically connects, and conducting wire is electrically connected with annular electrode b；The present invention realizes electric vehicle without stopping the function that can be charged, and electric vehicle can be detached from fully charged or other aircraft with guide rail car at any time, and freely travelling for electric vehicle will not be caused to limit.

Description

A kind of electric vehicle
Technical field
The invention belongs to electric vehicle corollary system fields, and in particular to a kind of electric vehicle.
Background technology
Universal with electric vehicle, the problem of electric vehicle charging is inconvenient, also increasingly highlights；Purchase electric vehicle at present User be typically limited to only city use on and off duty, need for a long time at a distance outgoing user then still tend to use fuel oil Vehicle.And even city short distance traveling, user are also required to pay attention to very much the remaining capacity of electric vehicle, are otherwise susceptible on the way Situation about casting anchor without electricity.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric vehicle Speech is not just most suitable, and the floor space of one side electric vehicle is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills Electricity may cause traffic congestion, and on the other hand, electric vehicle power consumption also many bigger than the battery truck of two-wheeled charges in current battery In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
Invention content
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, provide a kind of charging conveniently, and The charging system for electric automobile of user hours underway is not delayed.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of charging system for electric automobile, including There are the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail between each power transmission rod of road homonymy, rolling Guide rail car that is dynamic or being slidably mounted on the transmission guide rail and be electrically connected with transmission guide rail, can rest on guide rail car and with Guide rail car electrical connection aircraft and be connected between electric vehicle and aircraft to by electric energy from transmission guide rail transmit Conducting wire on to electric vehicle；The transmission guide rail by two symmetrical, opening is spliced towards opposite U-shaped rail, Spliced transmission guide rail radial section is in I-shaped, is connected between two U-shaped rail by insulating materials；Under the guide rail car Side is set there are one stopping platform, and the stopping platform front and back ends respectively pass through the equal first connecting rod of effective length and second The front and back ends of connecting rod and guide rail car connect；The first connecting rod, second connecting rod are arranged in parallel, first connecting rod, second connecting rod two End is rotatablely connected respectively with guide rail car, stopping platform；One end that the first connecting rod is connect with guide rail car forms driven gear Portion is equipped with the platform driving motor of driving first connecting rod rotation on the guide rail car, connects on the output shaft of platform driving motor It is connected to the drive gear being connected by meshing transmission with driven tooth wheel portion；During aircraft flies to guide rail car, platform driving motor First connecting rod rotation is driven forward, stopping platform is driven to turn to guide rail car towards road side；Stop in aircraft flat to stopping After on platform, platform driving motor is driven reverse first connecting rod rotation, and then stopping platform is driven to turn to below guide rail car；Institute It states stopping platform upper end centre position and the wireless charging transmitting module powered by transmission guide rail, the aircraft lower end peace is installed Equipped with the wireless charging receiving module electrically connected with conducting wire.
Preferably：The guide rail car includes the whole vehicle frame in opening up U-shaped, the vehicle frame top two Side is two symmetrically arranged vehicle frame plates, is rotatablely equipped with 2 groups or more of driving wheel on the inside of two vehicle frame plates respectively, described The axis of driving wheel is horizontally disposed, and the position of corresponding each driving wheel is equipped with to band on the outside of two vehicle frame plates The driving motor of dynamic driving wheel rotation；The U-shaped of idler wheel, the idler wheel and homonymy is also separately installed on the inside of two vehicle frame plates Rail contact electrically connects；The idler wheel is rotatably installed in the roller mount of U-shaped, is connected in the roller mount along frame width The sliding bar of direction setting, is equipped with sliding seat be slidably connected with sliding bar on the vehicle frame plate, the sliding bar and The spring being against to pushing rolling wheels on U-shaped rail is installed between sliding seat；It is connected between the roller mount of homonymy Bar；The vehicle frame lower end is fixedly connected there are one mounting base, and the platform courses motor is mounted in mounting base, and described first connects Bar, second connecting rod one end be rotatably connected in mounting base；Roller mount or connecting rod positioned at vehicle frame both sides is by electric wire and wirelessly Charging transmitting module electrically connects so that transmission guide rail is electrically connected with the formation of wireless charging transmitting module.
Preferably：There are one wire-winding unit, the wire-winding unit includes one for the electromobile at top installation The Wiinding cartridge of a upper end opening, the wire spool being rotatably installed in Wiinding cartridge and the magnetic material for being connected to Wiinding cartridge upper end Box cover；There are one coiling electric motors for centre position installation in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electricity The rotor of machine is fixedly connected with wire spool；There are two the annular electrode a being arranged concentrically, the coilings for the Wiinding cartridge bottom installation The lower face of disk be equipped with the annular electrode b, the annular electrode a that two annular electrode a slips electrically connect with it is electronic The accumulator of automobile electrically connects, and the conducting wire is electrically connected with annular electrode b；The Wiinding cartridge side offers what is passed through for conducting wire Cross line mouth.
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；Positioned at the upper of connecting tube in the fan mounting portion Side is connected with upper bracket, and driving fan is equipped on the upper bracket；It is located at the lower section of connecting tube in the fan mounting portion Lower carriage is connected with, lower driving fan is installed on the lower carriage；The steering phase of the upper driving fan and lower driving fan Instead, and in the fan mounting portion internal diameter for installing driving fan part is more than the lower driving fan portion of installation in fan mounting portion The internal diameter divided, the interior wind pressure superatmospheric between upper driving fan and lower driving fan of the fan mounting portion so that Go out and wind pressure is formed in vane；It is described go out vane include the vane upper shell of sealed connection and vane lower housing, under the vane Housing inner circumferential upper end forms interior curved wall, and there are one air outlet guard boards by the connection of multiple dowels for the inner circumferential of the interior curved wall, go out Windshield plate upper end is tightly connected with vane upper shell inner circumferential lower end；It is formed between the interior curved wall and air outlet guard board wide at the top and narrow at the bottom Outlet air gap, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing is located under outlet air gap Side is training wall wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree；The axial direction of the vane and fan mounting portion Radial direction it is perpendicular, and go out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and go out the outlet air gap of vane The horizontal wind-force that the wind of blowout generates is opposite with the rotation direction of the fan blade of upper driving fan；It is equipped in each connecting tube To adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting part includes third motor, with third electricity The coaxially connected screw rod of machine output shaft and the valve plate being connect with screw flight；The valve plate upper periphery is close in connecting tube Wall, valve plate lower end are located at the medium position of upper and lower directions in connecting tube；The connecting tube internal upper part forms to install described The third motor mounting plate of third motor, the third motor mounting plate are connected with towards the side for going out vane and are slided with the valve plate The valve plate guide rod of dynamic connection；Upper end direction to go out the inclined baffle in vane direction there are one the connections of lower part in the connecting tube, described The conducting adjustable air passage of area is formed between baffle and valve plate；The upper driving fan, lower driving fan and each third Motor is electrically connected respectively with control circuit board；The main part is tightly connected and forms for upper shell and lower housing；The main part Upper end connects the air intake cover there are one semiellipse spherical shape, and the air inlet of strip is uniformly formed on air intake cover.
Preferably：The lower, outer perimeter of the fan mounting portion is accumulator mounting portion, is connected on accumulator mounting portion It is connected to the accumulator being electrically connected with control circuit board；The whole wireless charging receiving module in a ring is connected to accumulator Lower end, the lower end of the aircraft are equipped with camera, and the camera is electrically connected with control circuit board.
Preferably：The stopping platform upper end be located at wireless charging transmitting module periphery installation there are one annular Magnet；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 described to rise and fall in Holder joint There are one undercarriages for each connection；The undercarriage, which includes, to be fixedly connected with Holder joint of rising and falling and by Holder joint and the outlet air of rising and falling The connection pipe body being connected inside ring, the sliding tube being slidably mounted in connection pipe body, with connection pipe body close to Holder joint of rising and falling The supporting rod of one end rotation connection is connected on supporting rod far from Holder joint one end of rising and falling sucking in annular magnet upper end Or the second electromagnet and the connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod respectively of automobile top；The connection Tube body forms hinged seat close to the Holder joint one end wall that rises and falls, and described supporting rod one end is rotatablely connected with hinged seat；The cunning Dynamic pipe 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 articulated joint, the connecting rod One end is rotatablely connected with articulated joint, and side wall of the connection pipe body far from Holder joint one end of rising and falling forms what is passed through for articulated joint Strip shape gob；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, the inner end integrally connected of sealing cap There is spring positioning bar, spring is arranged on the spring positioning bar, the both ends of the spring is against piston and sealing cap inner end respectively Between；The connecting rod tank that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod；The spring is in The supporting rod is in unfolded state during extended configuration, after the upper driving fan is in running order, goes out the air pressure in vane Driving piston makes supporting rod be in collapsed state together with sliding tube movement.
The present invention also provides a kind of charging system for electric automobile, include the multiple transmissions of electricity for being fixedly mounted on both sides of the road Bar, the transmission guide rail between each power transmission rod of road homonymy, roll or be slidably mounted on the transmission guide rail and The guide rail car being electrically connected with transmission guide rail, the aircraft that can be rested on guide rail car and be electrically connected with guide rail car and connection Between electric vehicle and aircraft electric energy to be transferred to the conducting wire on electric vehicle from transmission guide rail；The transmission of electricity is led For rail by two symmetrical, opening is spliced towards opposite U-shaped rail, spliced transmission guide rail radial section is in I-shaped Type is connected by insulating materials between two U-shaped rail；It is set below the guide rail car there are one stopping platform, described stop is put down Platform front and back ends are respectively connected by the equal first connecting rod of effective length and the front and back ends of second connecting rod and guide rail car；It is described First connecting rod, second connecting rod are arranged in parallel, first connecting rod, second connecting rod both ends respectively with guide rail car, stopping platform rotation connect It connects；One end that the first connecting rod is connect with guide rail car forms driven tooth wheel portion, and driving first is equipped on the guide rail car The platform driving motor of link rotatable is connected with what is be connected by meshing transmission with driven tooth wheel portion on the output shaft of platform driving motor Drive gear；During aircraft flies to guide rail car, platform driving motor is driven forward first connecting rod rotation, drives to stop and put down Platform turns to guide rail car towards road side；After aircraft stops onto stopping platform, platform driving motor is driven reverse the One link rotatable, and then stopping platform is driven to turn to below guide rail car；Stopping platform upper end centre position be equipped with by The wireless charging transmitting module of transmission guide rail power supply, the aircraft lower end are equipped with the wireless charging electrically connected with conducting wire and receive Module；The guide rail car includes the whole vehicle frame in opening up U-shaped, and vehicle frame top both sides are symmetrical arranged for two Vehicle frame plate, be rotatablely equipped with 2 groups or more of driving wheel on the inside of two vehicle frame plates respectively, the axis of the driving wheel is along water Square to setting, the position of corresponding each driving wheels is equipped with the drive that driving wheel is driven to rotate on the outside of two vehicle frame plates Dynamic motor；The U-shaped rail contact Electricity Federation of idler wheel, the idler wheel and homonymy is also separately installed on the inside of two vehicle frame plates It connects；The idler wheel is rotatably installed in the roller mount of U-shaped, and the slip set along frame width direction is connected in the roller mount Bar is equipped with the sliding seat being slidably connected with sliding bar on the vehicle frame plate, is installed between the sliding bar and sliding seat There is the spring being against to pushing rolling wheels on U-shaped rail；Connecting rod is connected between the roller mount of homonymy；The vehicle frame lower end Be fixedly connected there are one mounting base, the platform courses motor is mounted in mounting base, the first connecting rod, second connecting rod one End is rotatably connected in mounting base；Roller mount or connecting rod positioned at vehicle frame both sides pass through electric wire and wireless charging transmitting module Electricity Federation It connects so that transmission guide rail is electrically connected with the formation of wireless charging transmitting module；There are one coiling groups for the electromobile at top installation Part, the wire-winding unit include the Wiinding cartridge there are one upper end opening, the wire spool being rotatably installed in Wiinding cartridge and connection In the box cover of the magnetic material of Wiinding cartridge upper end；There are one coiling electric motor, coiling electric motors for centre position installation in the Wiinding cartridge For external rotor electric machine, the rotor of the coiling electric motor is fixedly connected with wire spool；There are two with one heart for the Wiinding cartridge bottom installation The annular electrode a of setting, the lower face of the wire spool are equipped with the annular electro electrically connected with two annular electrode a slips The accumulator of pole b, the annular electrode a and electric vehicle electrically connects, and the conducting wire is electrically connected with annular electrode b；The coiling Box side is offered crosses line mouth for what conducting wire passed through；The aircraft includes main part, and the main part includes tubular Fan mounting portion, be connected to fan mounting portion periphery and the connecting tube of four equidistant arrangements being connected with fan mounting portion, And it is connected to each connecting tube outer end and goes out vane with what corresponding position connecting tube was connected；It is located in the fan mounting portion Upper bracket is connected with above connecting tube, driving fan is installed on the upper bracket；It is located in the fan mounting portion and connects The lower section taken over is connected with lower carriage, and lower driving fan is equipped on the lower carriage；The upper driving fan and lower driving wind The steering of fan is on the contrary, and install the internal diameter of driving fan part more than under installation in fan mounting portion in the fan mounting portion The internal diameter of driving fan part, the interior wind pressure between upper driving fan and lower driving fan of the fan mounting portion is higher than big Air pressure so that go out and wind pressure is formed in vane；It is described go out vane include the vane upper shell of sealed connection and vane lower housing, institute It states vane lower housing inner circumferential upper end and forms interior curved wall, there are one outlet air by the connection of multiple dowels for the inner circumferential of the interior curved wall Baffle, air outlet guard board upper end are 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 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree；The axial direction and wind of the vane The radial direction for fanning mounting portion is perpendicular, and goes out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and go out vane The horizontal wind-force that the wind of outlet air gap blowout generates is opposite with the rotation direction of the fan blade of upper driving fan；Each connecting tube It being inside equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting part includes third motor, Coaxially connected screw rod and the valve plate being connect with screw flight with third motor output shaft；The valve plate upper periphery close to Inside pipe wall is connected, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；The connecting tube internal upper part form to The third motor mounting plate of the third motor is installed, the third motor mounting plate is connected with towards the side for going out vane and institute State the valve plate guide rod that valve plate is slidably connected；Upper end direction to go out the inclined gear in vane direction there are one the connections of lower part in the connecting tube Plate forms the conducting adjustable air passage of area between the baffle and valve plate；The upper driving fan, lower driving fan and each A third motor is electrically connected respectively with control circuit board；The main part is tightly connected and forms for upper shell and lower housing；It is described Main part upper end connects the air intake cover there are one semiellipse spherical shape, and the air inlet of strip is uniformly formed on air intake cover；Institute The lower, outer perimeter for stating fan mounting portion is accumulator mounting portion, is connected with what is be electrically connected with control circuit board on accumulator mounting portion Accumulator；The whole wireless charging receiving module in a ring is connected to the lower end of accumulator, the lower end peace of the aircraft Equipped with camera, the camera is electrically connected with control circuit board；The stopping platform upper end is located at wireless charging transmitting module Periphery installation there are one annular magnet；Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint of rising and falling, Respectively there are one undercarriages for connection in each Holder joint of rising and falling；The undercarriage include be fixedly connected with Holder joint of rising and falling and By Holder joint of rising and falling with going out the connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connecting Take over body is connected to the use 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 With suck the second electromagnet in annular magnet upper end or electromobile at top and respectively in the middle part of sliding tube, in supporting rod The connecting rod of portion's rotation connection；The connection pipe body forms hinged seat, the supporting rod one close to the Holder joint one end wall that rises and falls End is rotatablely connected with hinged seat；The sliding tube is connected with piston, the slip pipe outer wall middle part close to Holder joint one end of rising and falling Position is connected with articulated joint, and described connecting rod one end is rotatablely connected with articulated joint, and the connection pipe body is far from Holder joint one end of rising and falling Side wall form the strip shape gob passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with envelope Mouth cap, the inner end of sealing cap is connected with spring positioning bar, spring, the both ends of the spring is arranged on the spring positioning bar It is against respectively between piston and sealing cap inner end；It is formed on the supporting rod and accommodates the connecting rod in supporting rod collapsed state Connecting rod tank；The supporting rod is in unfolded state when the spring is in extended configuration, and the upper driving fan is in work After making state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The present invention also provides a kind of electric vehicles, include car body and the aircraft being connect by conducting wire with car body；Institute Car body top installation is stated there are one wire-winding unit, the wire-winding unit includes the Wiinding cartridge there are one upper end opening, rotational installation Wire spool in Wiinding cartridge and be connected to Wiinding cartridge upper end magnetic material box cover；
There are one coiling electric motors for centre position installation in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；There are two the annular electrode a being arranged concentrically, the wire spools for the Wiinding cartridge bottom installation Lower face the annular electrode b, the annular electrode a that are electrically connected with two annular electrode a slips and electronic vapour are installed The accumulator of vehicle electrically connects, and the conducting wire is electrically connected with annular electrode b；The Wiinding cartridge side offers the mistake passed through for conducting wire Line mouth；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, institute It states and driving fan is installed on upper bracket；It is located in the fan mounting portion below connecting tube and is connected with lower carriage, it is described Lower driving fan is installed on lower carriage；The steering of the upper driving fan and lower driving fan is on the contrary, and fan installation The internal diameter that driving fan part is installed in portion is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, the fan Wind pressure superatmospheric in mounting portion between upper driving fan and lower driving fan so that go out and wind pressure is formed in vane； 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 forms Interior curved wall, the inner circumferential of the interior curved wall by the connection of multiple dowels there are one air outlet guard board, air outlet guard board upper end on vane Housing inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air gap are formed between the interior curved wall and air outlet guard board Lower end width be 0.8-1.5mm；It is led to be wide at the top and narrow at the bottom the lower section that the inner circumferential of the vane lower housing is located at outlet air gap Wall is flowed, the cone angle size of the taper surface is 20-30 degree；The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and Go out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and the water that the wind for going out the outlet air gap blowout of vane generates Flat wind-force is opposite with the rotation direction of the fan blade of upper driving fan；It is equipped with to adjust corresponding position in each connecting tube Go out the adjusting part of vane outlet air speed, the adjusting part includes third motor, coaxially connected with third motor output shaft Screw rod and the valve plate that is connect with screw flight；Close to connection inside pipe wall, valve plate lower end is located to be connected the valve plate upper periphery Take over the medium position of interior upper and lower directions；The connecting tube internal upper part forms to install the third motor of the third motor Installing plate, the third motor mounting plate are connected with the valve plate guide rod being slidably connected with the valve plate towards the side for going out vane； Lower part connection is formed there are one upper end towards the inclined baffle in vane direction is gone out between the baffle and valve plate in the connecting tube The adjustable air passage of area is connected；The upper driving fan, lower driving fan and each third motor respectively with control circuit Plate is electrically connected；The main part is tightly connected and forms for upper shell and lower housing；The main part upper end connection is ellipse there are one half The air intake cover of Surface of Sphere shape uniformly forms the air inlet of strip on air intake cover.
Preferably：The lower, outer perimeter of the fan mounting portion is accumulator mounting portion, is connected on accumulator mounting portion It is connected to the accumulator being electrically connected with control circuit board；The lower end of accumulator is connected with whole wireless charging in a ring and receives mould Block；The lower end of the aircraft is equipped with camera, and the camera is electrically connected with control circuit board.
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 on supporting rod far from Holder joint one end of rising and falling close to the supporting rod for Holder joint one end rotation connection of rising and falling inhaling The tightly connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod in the second electromagnet of electromobile at top and respectively；Institute It states connection pipe body and forms hinged seat close to the Holder joint one end wall that rises and falls, described supporting rod one end is rotatablely connected with hinged seat； 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 articulated joint, institute It states connecting rod one end to be rotatablely connected with articulated joint, side wall of the connection pipe body far from Holder joint one end of rising and falling is formed for articulated joint The strip shape gob passed through；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, the inner end one of sealing cap Body 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 and sealing respectively Between cap inner end；The connecting rod tank that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod；The bullet The supporting rod is in unfolded state when spring is in extended configuration, after the upper driving fan is in running order, goes out in vane Air pressure driving piston together with sliding tube movement supporting rod is made to be in collapsed state.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention on transmission guide rail by travelling and keeping The guide rail car of the travel speed identical with electric vehicle coordinates and passes through the aircraft that conducting wire is connect and guide rail car electricity with electric vehicle Connection charges for the electric vehicle in traveling, realizes electric vehicle without stopping the function that can be charged, and electricity Electrical automobile can be detached from fully charged or other aircraft with guide rail car at any time, will not be to the free walker of electric vehicle It sails and causes to limit.
When aircraft does not work, the aircraft passes through the second electromagnet（Iron core）It sucks in electromobile at top coiling The upper end of the box cover of component, when aircraft works, the energization of the second electromagnet, which generates the magnetic field reversed with the box cover of magnetic material, to be made Aircraft is detached from electric vehicle.
When electric vehicle needs charging, the control system of electric vehicle sends signal, clothes to the server of charging system The guide rail car of business device control nearby keeps travelling with electric vehicle uniform velocity, while the controller control platform of guide rail car drives electricity Machine rotation makes stopping platform turn to guide rail car towards the side among road, and then the control system of electric vehicle is to aircraft Signal is sent, aircraft is made to fly to corresponding guide rail car and is rested on the stopping platform of guide rail car, stopping platform and aircraft Between electric energy transmitted by wireless charging transmitting module and wireless charging receiving module, electric vehicle is made to form electricity with transmission guide rail Connection；During aircraft flies away from electric vehicle, control system controls the coiling electric motor of wire-winding unit to rotate simultaneously to be made to lead Line is released from wire spool；After electric vehicle charges, aircraft flies back to electromobile at top, while coiling electric motor is reversed Rotation makes on conducting wire wraparound wire spool.
The aircraft provides driving force, the part that upper driving fan generates by the upper driving fan in fan mounting portion Air-flow from it is each go out vane outlet air gap downwards blow out, and combine adjusting part adjustment and each go out vane and go out wind velocity, from And realize the horizontal flight or steering of aircraft, due to be located at aircraft periphery it is each go out vane only play adjustment aircraft The effect of posture, without the fan for being provided with power, go out not easily leading to when vane generates touching with foreign object aircraft it is out of control or Injury is generated to human or animal, safety is good.Similar to four-axle aircraft, four go out vane and only play adjusting appearance the aircraft appearance The function of state, therefore the present invention substantially should be uniaxial aircraft.
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 or upper driving fan and lower driving fan generate when rotating；Also, by adjusting each adjusting simultaneously Component change vane go out wind velocity, it can be achieved that the whole forward or reverse of aircraft.It is adjusted by adjusting one or two Section component makes what one or two went out vane to go out wind velocity, it can be achieved that aircraft can drive in this way generally in heeling condition Aircraft flies in the horizontal direction.
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.
Description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is structure diagram when aircraft is rested on electric vehicle.
Fig. 3 is the decomposition texture schematic diagram of wire-winding unit.
Fig. 4 is configuration state schematic diagram when aircraft is accommodated on guide rail car.
Fig. 5 is the configuration state schematic diagram after aircraft is accommodated on guide rail car.
Fig. 6 is the structure diagram of aircraft shutdown status.
Fig. 7 is the structure diagram of aircraft flight state.
Fig. 8 is the schematic cross-sectional view of aircraft.
Fig. 9 is the A portions schematic enlarged-scale view of Fig. 8.
Figure 10 is the B portions schematic enlarged-scale view of Fig. 8.
The structure diagram of each component that Figure 11 is upper shell and is connect with upper shell.
Figure 12 is the structure diagram of lower housing section.
Figure 13 is the schematic cross-sectional view of lower housing section.
Figure 14 is the decomposition texture schematic diagram of undercarriage part.
Figure 15 is the schematic cross-sectional view of undercarriage part.
1st, power transmission rod；2nd, transmission guide rail；3rd, commutate guide rail；4th, guide rail car；40th, vehicle frame；401st, mounting base；41st, it drives Wheel；411st, driving motor；42nd, idler wheel；421st, roller mount；422nd, sliding bar；423rd, sliding seat；424th, connecting rod；43rd, platform courses Motor；44th, first connecting rod；441st, driven tooth wheel portion；45th, second connecting rod；46th, stopping platform；461st, annular magnet；462nd, it is wireless Charge transmitting module；5th, electric vehicle；5a, wire-winding unit；51st, Wiinding cartridge；511st, line mouth is crossed；52nd, coiling electric motor；53rd, coiling Disk；54th, box cover；6th, conducting wire；9th, aircraft；91st, main part；91a, upper shell；91b, lower housing；910th, fan mounting portion； 9101st, upper bracket；9102nd, lower carriage；9103rd, accumulator mounting portion；9104th, circuit board installation cavity；9105th, air inlet hole；9106、 Vent；9107th, camera；911st, go out vane；9110th, it rises and falls Holder joint；9111st, vane upper shell；9112nd, vane lower casing Body；91121st, interior curved wall；91122nd, dowel；91123rd, air outlet guard board；91124th, training wall；912nd, connecting tube；9121st, third Motor mounting plate；9122nd, valve plate guide rod；9123rd, baffle；913rd, the first cover board；92nd, accumulator；93rd, undercarriage；931st, it connects Tube body；9311st, hinged seat；9312nd, strip shape gob；932nd, sliding tube；9321st, piston；9322nd, articulated joint；933rd, sealing cap； 9331st, spring positioning bar；934th, connecting rod；935th, supporting rod；9351st, connecting rod tank；936th, the second electromagnet；937th, spring；94、 Air intake cover；951st, upper driving fan；952nd, lower driving fan；96th, adjusting part；961st, third motor；962nd, screw rod；963rd, valve Plate；97th, control circuit board.
Specific embodiment
Embodiment 1
According to Fig. 1 to 5, the present embodiment is a kind of charging system for electric automobile, includes and is fixedly mounted on both sides of the road Multiple power transmission rods 1, the transmission guide rail 2 between each power transmission rod of road homonymy are rolled or are slidably mounted on and is described defeated The guide rail car 4 being electrically connected on conductance rail and with transmission guide rail, the flight that can be rested on guide rail car and be electrically connected with guide rail car Device 9 and be connected between electric vehicle and aircraft electric energy is transferred to leading on electric vehicle from transmission guide rail Line 6.The conducting wire refers to whole line, and 2 electric wires are included in conducting wire.The transmission guide rail is by two symmetrical, opening courts It is spliced to opposite U-shaped rail, spliced transmission guide rail radial section is in I-shaped, is passed through between two U-shaped rail Insulating materials connects.Between the end of the transmission guide rail of both sides of the road connection there are two commutation guide rail 3, commutation guide rail 3 to Few is being arc-shaped with transmission guide rail junction, and commutation guide rail is spliced as transmission guide rail by two U-shaped rail.By In the quantity and travel direction of the electric vehicle to charge on each section of road be random, therefore need in road At least two groups of commutation guide rails are connected between two transmission guide rails of both sides, in order to which guide rail car is moved from the transmission guide rail of road side It moves on the transmission guide rail of opposite side.Further, due to existing in commutation guide rail with transmission guide rail junction and transmission guide rail There are corners to certainly exist non-directional track for road（It is general as arc-shaped in being designed as in Fig. 1）, therefore the idler wheel on guide rail car It is designed to move along guide rail car left and right directions so that guide rail car can make the idler wheel of both sides when driving into arc-shaped track It keeps offseting with the holding of both sides U-shaped rail.Stopping platform 46 there are one being set below the guide rail car, the stopping platform are forward and backward End is respectively connect by the equal first connecting rod 66 of effective length and second connecting rod 45 with the front and back ends of guide rail car；Described One connecting rod, second connecting rod are arranged in parallel, first connecting rod, second connecting rod both ends respectively with guide rail car, stopping platform be rotatablely connected； One end that the first connecting rod is connect with guide rail car forms driven tooth wheel portion 441, and driving first is equipped on the guide rail car The platform driving motor 43 of link rotatable is connected on the output shaft of platform driving motor and is connected by meshing transmission with driven tooth wheel portion Drive gear.During aircraft flies to guide rail car, platform driving motor is driven forward first connecting rod rotation, drives and stops Platform turns to guide rail car towards road side；After aircraft stops onto stopping platform, platform driving motor is driven reverse First connecting rod rotates, and then stopping platform is driven to turn to below guide rail car.Stopping platform upper end centre position is equipped with The wireless charging transmitting module 462 powered by transmission guide rail, the aircraft lower end is equipped with the wireless charging electrically connected with conducting wire Electric receiving module.The guide rail car includes the whole vehicle frame 40 in opening up U-shaped, and vehicle frame top both sides are two Symmetrically arranged vehicle frame plate, two vehicle frame plates insides are rotatablely equipped with 2 groups or more of driving wheel 41, the driving wheel respectively Axis it is horizontally disposed, the position of corresponding each driving wheels is equipped with to drive driving on the outside of two vehicle frame plates Take turns the driving motor 411 of rotation.The U-shaped of idler wheel 42, the idler wheel and homonymy is also separately installed on the inside of two vehicle frame plates Rail contact electrically connects；The idler wheel is rotatably installed in the roller mount 421 of U-shaped, is connected in the roller mount along vehicle frame The sliding bar 422 of width direction setting, is equipped with the sliding seat 423 being slidably connected with sliding bar, institute on the vehicle frame plate State the spring for being equipped with and being against to pushing rolling wheels on U-shaped rail between sliding bar and sliding seat；Positioned at homonymy roller mount it Between be connected with connecting rod 424.
The vehicle frame lower end is fixedly connected there are one mounting base 401, and the platform courses motor is mounted in mounting base, institute State first connecting rod, one end of second connecting rod is rotatably connected in mounting base.Roller mount or connecting rod positioned at vehicle frame both sides pass through electricity Line is electrically connected with wireless charging transmitting module so that transmission guide rail is electrically connected with the formation of wireless charging transmitting module.The vehicle frame On the controller for controlling driving motor rotation direction and rotating speed and control platform driving motor rotating is installed.Institute It states and pressure sensor is installed on stopping platform, pressure sensor detects signal when aircraft is dropped on stopping platform, The rotation of controller control platform driving motor makes stopping platform turn to below guide rail car, to ensure that guide rail car left and right sides weight is put down Weighing apparatus.
Can be connected between the idler wheel and roller mount by bearing, then metal material inner ring, outer ring and the ball of bearing it Between also formed and electrically connect, and larger resistance may be caused between ball and inner ring, outer ring there are lubricant medium, therefore guide rail car is every Side is rolled by 2-3 idler wheel and transmission guide rail and connected, and can ensure the continuity transmitted electricity between guide rail car and transmission guide rail, is protected Demonstrate,prove stable voltage, electric current.
There are one wire-winding unit 5a for the electromobile at top installation, and the wire-winding unit is including there are one upper end openings The box cover 54 of Wiinding cartridge 51, the wire spool 53 being rotatably installed in Wiinding cartridge and the magnetic material for being connected to Wiinding cartridge upper end. There are one coiling electric motors 52 for centre position installation in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor is fixedly connected with wire spool.The annular electrode a that there are two the Wiinding cartridge bottom installations is arranged concentrically, the wire spool Lower face is equipped with the annular electrode b, the annular electrode a and electric vehicle electrically connected with two annular electrode a slips Accumulator or charge controller electrically connect, the conducting wire is electrically connected with annular electrode b.The Wiinding cartridge side offers confession What conducting wire passed through crosses line mouth 511.In addition, the aircraft is also powered by transmission guide rail.
The present invention passes through the guide rail car of travel speed travelled on transmission guide rail and holding is identical with electric vehicle, cooperation It electrically connects to charge for the electric vehicle in traveling with guide rail car with the aircraft that electric vehicle is connect by conducting wire, realizes electricity Electrical automobile is without stopping the function that can be charged, and electric vehicle is in fully charged or other aircraft It is detached from any time with guide rail car, freely travelling for electric vehicle will not be caused to limit.
When aircraft does not work, the aircraft passes through the second electromagnet（Iron core）It sucks in electromobile at top coiling The upper end of the box cover of component, when aircraft works, the energization of the second electromagnet, which generates the magnetic field reversed with the box cover of magnetic material, to be made Aircraft is detached from electric vehicle.
When electric vehicle needs charging, the control system of electric vehicle sends signal, clothes to the server of charging system The guide rail car of business device control nearby keeps travelling with electric vehicle uniform velocity, while the controller control platform of guide rail car drives electricity Machine rotation makes stopping platform turn to guide rail car towards the side among road, and then the control system of electric vehicle is to aircraft Signal is sent, aircraft is made to fly to corresponding guide rail car and is rested on the stopping platform of guide rail car, stopping platform and aircraft Between electric energy transmitted by wireless charging transmitting module and wireless charging receiving module, electric vehicle is made to form electricity with transmission guide rail Connection；During aircraft flies away from electric vehicle, control system controls the coiling electric motor of wire-winding unit to rotate simultaneously to be made to lead Line is released from wire spool；After electric vehicle charges, aircraft flies back to electromobile at top, while coiling electric motor is reversed Rotation makes on conducting wire wraparound wire spool.
Embodiment 2
With reference to shown in Fig. 6 to Figure 13, the present embodiment makes following improvement on the basis of embodiment 1：The aircraft includes Main part 91, the main part include the fan mounting portion 910 of tubular, are connected to fan mounting portion periphery and pacify with fan The connecting tube for four equidistant arrangements that dress portion is connected and be connected to each connecting tube outer end and with corresponding position connecting tube phase Connection goes out vane 911.
It is located in the fan mounting portion above connecting tube and is connected with upper bracket 9101, is equipped on the upper bracket Driving fan 951；It is located in the fan mounting portion below connecting tube and is connected with lower carriage 9102, is installed on the lower carriage There is lower driving fan 952；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, position in the fan mounting portion Wind pressure superatmospheric between upper driving fan and lower driving fan so that go out and wind pressure is formed in vane.
It is described go out vane include the vane upper shell 9111 of sealed connection and vane lower housing 9112, the vane lower casing Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected by multiple dowels 91122 there are one air outlet guard board, Air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；Shape between the interior curved wall 91121 and air outlet guard board 91123 Into outlet air gap wide at the top and narrow at the bottom, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing is located at The lower section in outlet air gap is training wall 91124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree.
The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out shape between the axial direction of vane and horizontal direction Into the angle of 5-20 degree, and turn 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 Dynamic direction is opposite.
It is equipped with to adjust the adjusting part 96 that corresponding position goes out vane outlet air speed in each connecting tube, it is described Adjusting part includes third motor 961, the screw rod 962 coaxially connected with third motor output shaft and with screw flight connect The valve plate 963 connect；For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the middle part of upper and lower directions in connecting tube Position；The connecting tube internal upper part forms to install the third motor mounting plate of the third motor, the third motor Installing plate 9121 is connected with the valve plate guide rod 9122 being slidably connected with the valve plate towards the side for going out vane；In the connecting tube Lower part connection, towards the inclined baffle 9123 in vane direction is gone out, forms conducting area there are one upper end between the baffle and valve plate Adjustable air passage.
The upper driving fan, lower driving fan and each third motor are electrically connected respectively with control circuit board 97.Institute It states main part and is tightly connected composition for upper shell 91a and lower housing 91b.
The main part upper end connects the air intake cover 94 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover The air inlet of shape.
The lower, outer perimeter of the fan mounting portion is accumulator mounting portion 9103, is connected with and controls on accumulator mounting portion The accumulator 92 of circuit board electrical connection；The whole wireless charging receiving module in a ring is connected to the lower end of accumulator.
The lower end of the aircraft is equipped with camera 9107, and the camera is electrically connected with control circuit board.
The camera shooting obtains the position of aircraft opposite rail vehicle or electric vehicle, can remotely be grasped by manual operation Vertical aircraft is accommodated to by the second electromagnet on corresponding guide rail car or electric vehicle, can also be allowed by machine vision technique Aircraft is accommodated to automatically on corresponding guide rail car or electric vehicle.
Positioned at the top of accumulator mounting portion for a circuit board installation cavity 9104 on the fan mounting portion, the control Circuit board is mounted in circuit board installation cavity, and there are one the first cover boards 913 of annular for the circuit board installation cavity lower end connection；Institute The upper surface for stating circuit board installation cavity uniformly forms the air inlet hole 9105 connected in fan mounting portion, the circuit board installation The lateral wall of chamber uniformly forms vent 9106.
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.The aircraft appearance is similar to four-axle aircraft, therefore with four-axle aircraft It is named, four go out vane i.e. so-called " four axis " and only play the function of adjusting posture, therefore this aircraft substantially should be uniaxial Aircraft.
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.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, control circuit board is played scattered Heat effect.
Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint 9110 of rising and falling, each undercarriage Respectively there are one undercarriages 93 for connection on connector；The undercarriage is equipped with to suck the second electromagnet in electromobile at top 936。
When aircraft does not work, aircraft is sucked by the second electromagnet of undercarriage lower end in electromobile at top On box cover.
Embodiment 3
With reference to Figure 14 to Figure 15, the present embodiment also makes following improvement on the basis of embodiment 2：The stopping platform upper end position In the installation of the periphery of wireless charging transmitting module, there are one annular magnets 461.
Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint 9110 of rising and falling, each undercarriage Respectively there are one undercarriages 93 for connection on connector；The undercarriage, which includes, to be fixedly connected with Holder joint of rising and falling and by the bridge joint that rises and falls Head is with going out the connection pipe body 931 being connected inside vane, the sliding tube 932 being slidably mounted in connection pipe body, with connection pipe body Close to rise and fall Holder joint one end rotation connection supporting rod 935, be connected on supporting rod far from rise and fall Holder joint one end to Suck the second electromagnet 936 in annular magnet upper end or automobile top and respectively with turning in the middle part of sliding tube, in the middle part of supporting rod The connecting rod 934 of dynamic connection.
The connection pipe body forms hinged seat 9311, 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 9321, 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 9322, 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 9312 passed through for articulated joint；The one end of 912 body of connecting tube far from Holder joint of rising and falling is consolidated Surely sealing cap 933 is connected with, the inner end of sealing cap is connected with spring positioning bar 9331, is arranged on the spring positioning bar Spring 937, the both ends of the spring are against respectively between piston and sealing cap inner end；It forms on the supporting rod and is received in supporting rod The connecting rod tank 9351 of the connecting rod is accommodated during the state of rising.
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.
Embodiment 4
The present embodiment is a kind of electric vehicle, includes car body and the aircraft being connect by conducting wire with car body.
There are one wire-winding unit, the wire-winding unit includes the coiling there are one upper end opening for the car body top installation Box, the wire spool being rotatably installed in Wiinding cartridge and be connected to Wiinding cartridge upper end magnetic material box cover.
There are one coiling electric motors for centre position installation in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling The rotor of motor is fixedly connected with wire spool.
There are two the annular electrode a being arranged concentrically, the lower face of the wire spool is equipped with for the Wiinding cartridge bottom installation The annular electrode b, the annular electrode a that are electrically connected with two annular electrode a slips and the accumulator Electricity Federation of electric vehicle It connects, the conducting wire is electrically connected with annular electrode b.
The Wiinding cartridge side is offered crosses line mouth for what conducting wire passed through.
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan Mounting portion periphery and the connecting tube for four equidistant arrangements being connected with fan mounting portion and it 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 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 wind is installed on the lower carriage Fan；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install driving fan part Internal diameter be more than the internal diameter of the lower driving fan part of installation in fan mounting portion, be located at upper driving fan in the fan mounting portion Wind pressure superatmospheric between lower driving fan so that go out and wind pressure is formed in vane.
It is described go out vane include the vane upper shell of sealed connection and vane lower housing, in the vane lower housing inner circumferential End forms interior curved wall, and there are one air outlet guard board, air outlet guard board upper ends by the connection of multiple dowels for the inner circumferential of the interior curved wall It is tightly connected with vane upper shell inner circumferential lower end；Outlet air gap wide at the top and narrow at the bottom is formed between the interior curved wall and air outlet guard board, The lower end width in outlet air 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 upper width Under narrow training wall, the cone angle size of the taper surface is 20-30 degree.
The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out shape between the axial direction of vane and horizontal direction Into the angle of 5-20 degree, and turn 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 Dynamic direction is opposite.
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the tune in each connecting tube Section component includes third motor, coaxially connected screw rod and the valve plate being connect with screw flight with third motor output shaft； 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；The company Take over internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out The side of vane is connected with the valve plate guide rod 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 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 third motor are electrically connected respectively with control circuit board.
The main part is tightly connected and forms for upper shell and lower housing.
The main part upper end connects the air intake cover there are one semiellipse spherical shape, and strip is uniformly formed on air intake cover Air inlet.
The lower, outer perimeter of the fan mounting portion is accumulator mounting portion, is connected on accumulator mounting portion and control circuit The accumulator of plate electrical connection；The lower end of accumulator is connected with whole wireless charging receiving module in a ring；The aircraft Lower end is equipped with camera, and the camera is electrically connected with control circuit board.
Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint of rising and falling, each Holder joint of rising and falling There are one undercarriages for upper each connection；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 connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connection pipe body close to the bridge joint that rises and falls The supporting rod of first end rotation connection is connected on supporting rod far from Holder joint one end of rising and falling sucking on electric vehicle top Second electromagnet in portion and the respectively connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod.
The connection pipe body forms hinged seat, described supporting rod one end and hinged seat close to the Holder joint one end wall that rises and falls Rotation 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 Articulated joint, described connecting rod one end are rotatablely connected with articulated joint, side wall molding of the connection pipe body far from Holder joint one end of rising and falling There is the strip shape gob passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, seals The inner end of cap is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against respectively Between piston and sealing cap inner end；The connecting rod appearance that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod Slot.
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.

Claims (2)

1. a kind of electric vehicle, it is characterised in that：Include car body and the aircraft being connect by conducting wire with car body；
There are one wire-winding unit, the wire-winding unit includes the Wiinding cartridge there are one upper end opening, turns for the car body top installation The box cover of dynamic wire spool and the magnetic material for being connected to Wiinding cartridge upper end in Wiinding cartridge；
There are one coiling electric motors for centre position installation in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；
The annular electrode a that there are two the Wiinding cartridge bottom installations is arranged concentrically, the lower face of the wire spool to be equipped with and two The annular electrode b, the annular electrode a and the accumulator of electric vehicle that a annular electrode a slips electrically connect are electrically connected, institute Conducting wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side is offered crosses line mouth for what conducting wire passed through；
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 the interior installation of fan mounting portion, is located at upper driving fan under in the fan mounting portion Wind pressure superatmospheric between driving fan so that go out and wind pressure is formed in vane；
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 third motor, coaxially connected screw rod and the valve plate being connect with screw flight with third motor output shaft；It is described For 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；The connecting tube Internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；Upper end direction to go out there are one the connections of lower part in the connecting tube The inclined baffle in vane direction forms the conducting adjustable air passage of area between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected respectively with control circuit board；
The main part is tightly connected and forms for upper shell and lower housing；
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.
2. a kind of electric vehicle as described in claim 1, it is characterised in that：The lower, outer perimeter of the fan mounting portion is electric power storage Pond mounting portion is connected with the accumulator being electrically connected with control circuit board on accumulator mounting portion；The lower end of accumulator is connected with whole The wireless charging receiving module of body in a ring；
The lower end of the aircraft is equipped with camera, and the camera is electrically connected with control circuit board.
CN201711448505.4A 2017-06-23 2017-06-23 A kind of electric vehicle Withdrawn CN108189687A (en)

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CN201710488460.7A CN107215231B (en) 2017-06-23 2017-06-23 A kind of electric vehicle and charging system

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CN201711448518.1A Withdrawn CN108177537A (en) 2017-06-23 2017-06-23 A kind of charging system of electric vehicle
CN201710488460.7A Active CN107215231B (en) 2017-06-23 2017-06-23 A kind of electric vehicle and charging system
CN201711446108.3A Withdrawn CN108001235A (en) 2017-06-23 2017-06-23 A kind of charging system of electric automobile
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CN201711446108.3A Withdrawn CN108001235A (en) 2017-06-23 2017-06-23 A kind of charging system of electric automobile
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CN107813723A (en) * 2017-11-01 2018-03-20 安徽易威斯新能源科技股份有限公司 A kind of energy storage charging pile using clean energy resource
CN109398010A (en) * 2018-12-11 2019-03-01 华东交通大学 A kind of car assisted device for crossing highway
DE102019131194A1 (en) * 2019-11-19 2021-05-20 Bayerische Motoren Werke Aktiengesellschaft Method for charging an accumulator of a motor vehicle
US20210253241A1 (en) * 2020-02-19 2021-08-19 Gad HARAN Electric vehicle with an airborne link device for connecting to a power line and an airborne link device thereof
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KR20130050003A (en) * 2011-11-07 2013-05-15 현대자동차주식회사 Vehicle charging system for complex building
CN102490619A (en) * 2011-12-14 2012-06-13 西南交通大学 Charging system in driving state of electric cars
CN202737496U (en) * 2012-06-11 2013-02-13 叶明旭 Automatic charging system for electric automobile
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
CN105244971A (en) * 2015-11-10 2016-01-13 蔡淑彬 Electric vehicle automatic charging system
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CN107215231A (en) 2017-09-29

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