CN108312872A - A kind of pure electric automobile power supply system - Google Patents

A kind of pure electric automobile power supply system Download PDF

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Publication number
CN108312872A
CN108312872A CN201810109939.XA CN201810109939A CN108312872A CN 108312872 A CN108312872 A CN 108312872A CN 201810109939 A CN201810109939 A CN 201810109939A CN 108312872 A CN108312872 A CN 108312872A
Authority
CN
China
Prior art keywords
connection
fan
vane
rail
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Withdrawn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
CN201810109939.XA
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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 CN201810109939.XA priority Critical patent/CN108312872A/en
Publication of CN108312872A publication Critical patent/CN108312872A/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Withdrawn legal-status Critical Current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
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—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
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • 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
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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

Abstract

The invention belongs to electric vehicle charging fields, more particularly to a kind of pure electric automobile power supply system, include multiple electric poles being equidistantly vertically installed among road among two-way lane, 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 carrying terminal pad movement.The present invention is arranged by road, can in time charge 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 with power transmission line by trolley component and is powered to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered.

Description

A kind of pure electric automobile power supply system
Technical field
The invention belongs to electric vehicle charging fields, and in particular to a kind of pure electric automobile power supply 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 problem to be solved by the present invention is to：In view of the deficienciess of the prior art, providing a kind of pure electric automobile Power supply system.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of pure electric automobile power supply system, packet Multiple electric poles being equidistantly vertically installed among road among two-way lane are included, is fixedly mounted on electric pole and is located at road The guide rail of road side and multiple trolley components being slidably connected on guide rail；Each electric pole includes vertical direction setting Upright bar；The upright bar upper end is fixedly connected with that there are two towards the horizontally disposed cross bar of road direction；The crossbar end and institute Guide rail is stated to be fixedly connected；The guide rail includes two vertical rails arranged in parallel, and to be fixedly connected on two vertical rails same The connection rail of the arc for trolley component turning commutation at end；The vertical rail and the connection rail upper end form top Rail；The vertical rail and the connection rail lower end form bottom rail；The head track end forms the overhead gage being directed downward；It is described Bottom rail end forms the lower baffle plate of direction upward；The vertical rail and the connection rail lateral surface are installed with transmission guide rail； The trolley component includes two moving assemblies being slidably connected on guide rail and is rotatablely connected with two moving assemblies Feeding pannel；The moving assembly is connect with the feeding pannel by pin rotation；The moving assembly includes being supplied for installing The supporting plate of electroplax；The supporting plate lower end forms the tilt prop for being used to support trolley component；The tilt prop end is equipped with more A the first roller that connection is rolled with the lower baffle plate lateral surface；The supporting plate upper surface forms riser；The riser upper end Form upper shifting board；The supporting plate and the upper shifting board are located in guide rail be respectively equipped with for making trolley component advance before Into wheel；The feeder wheel being installed on upper shifting board is connect with side roll in the overhead gage, is installed on described on supporting plate Feeder wheel is rolled with the vertical rail and is connected；The upper shifting board upper surface is equipped with multiple rolled with the overhead gage lower end and connects Third roller；The supporting plate lower face is equipped with multiple the second rollers that connection is rolled with the lower baffle plate upper end；The support Advance turbin generator for driving the feeder wheel rotation is installed at the plate feeder wheel corresponding with the upper shifting board；It is described Riser, which is located in the guide rail, is equipped with the contact slipper being slidably connected with the transmission guide rail；The supporting plate is far from the guide rail One end is equipped with the first connection electrode for being connect with the feeding pannel；It is logical that first connection electrode center forms first Hole；The feeding pannel upper surface is fixedly connected with the second electromagnet；The current electrode of annular is installed on second electromagnet； The feeding pannel corresponds to molding at the first through hole of two moving assemblies, and there are two the second through-holes；The feeding pannel lower end pair Answer the second connection electrode there are two being installed at the first connection electrode of two moving assemblies；Be equipped at the top of Rechargeable vehicle around Drum；It is pierced by the charging wire for being useful for charging to electric vehicle on rear side of the wire spool；The charging wire other end is connected with Connect disk；The wire spool upper end, which is fixedly connected with, parks disk；The terminal pad parks disk or described small described in being mobily connected in On vehicle component；Further include multiple aircraft for carrying terminal pad movement.
Preferably：Feeding pannel upper surface center is painted with for the first positioning for the Aerial vehicle position Label；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, every group of iron block slot are four circular grooves for being equipped with iron block；The terminal pad lower end is equipped with the annular iron of annular Block；The annular iron block lower end is equipped with the first receiving electrode for being electrically connected with the feeding pannel；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 of four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion, and be 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 It is connected with lower bracket, lower driving fan is installed on the lower bracket；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, and the fan blade diameter of upper driving fan is more than the fan blade diameter of lower driving fan, is located in the fan mounting portion Wind pressure superatmospheric between upper driving fan and lower driving fan so that go out and form wind pressure in vane；It is described go out vane packet The vane upper shell and vane lower housing of sealed connection are included, the vane lower housing inner circumferential upper end forms interior curved wall, described There are one air outlet guard board, air outlet guard board upper end and vane upper shell inner circumferential lower ends by the connection of multiple dowels for the inner circumferential of interior curved wall It is tightly connected；Outlet air gap wide at the top and narrow at the bottom, the lower end width in outlet air gap are formed between the interior curved wall and air outlet guard board For 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is training wall wide at the top and narrow at the bottom, the water conservancy diversion The cone angle size of taper surface residing for 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 The water that the wind for going out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and 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 Going out the adjusting part of vane outlet air speed, the adjusting part includes motor, the coaxially connected screw rod with motor output shaft, with And the valve plate being connect with screw flight；The valve plate upper periphery close to connection inside pipe wall, valve plate lower end be located at connecting tube it is interior on The medium position in lower direction；The connecting tube internal upper part forms to install the motor mounting plate of the motor, the motor Mounting plate is connected with the valve plate guide rod being slidably connected with the valve plate towards the side for going out vane；Lower part connects in the connecting tube There are one upper ends towards the inclined baffle in vane direction is gone out, and the conducting adjustable ventilation of area is formed between the baffle and valve plate Road；The upper driving fan, lower driving fan and each motor are electrically connected with control circuit board respectively；The main part upper end The air intake cover there are one semiellipse spherical shape is connected, the air inlet of strip is uniformly formed on air intake cover；The main part is Upper shell and lower housing, which are tightly connected, to be constituted；The lower, outer perimeter of the fan mounting portion is battery installation section, in battery installation section It is connected with the accumulator being electrically connected with control circuit board；The top for being located at battery installation section on the fan mounting portion is an electricity Road plate installation cavity, the control circuit board are mounted in circuit board installation cavity, and there are one the connections of circuit board installation cavity lower end The cover board of annular；The upper surface of the circuit board installation cavity uniformly forms the air inlet hole being connected to in fan mounting portion, described The lateral wall of circuit board installation cavity uniformly forms vent；The lower driving fan lower end is equipped with to be electrically connected with control circuit board The camera connect；Go out position of the vane inner circumferential far from connecting tube described in each and forms Holder joint of rising and falling, each undercarriage Respectively there are one undercarriages for connection on connector；The undercarriage includes the supporting rod being fixedly connected with the Holder joint of rising and falling and company It is connected on the first electromagnet far from Holder joint one end of rising and falling on supporting rod, the supporting rod is downwards；First electromagnet Lower section is equipped with the second receiving electrode for charging to aircraft.
Preferably：Go out position of the vane inner circumferential far from connecting tube described in each and forms 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 includes to be fixedly connected and pass through with Holder joint of rising and falling Holder joint of rising and falling with go 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 connecting rod with rotation connection in the middle part of sliding tube middle part, supporting rod respectively；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 sliding 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：It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction of vane The horizontal wind-force and upper drive that the wind for forming the angle of 5-20 degree between horizontal direction, and going out the outlet air gap blowout of vane generates The rotation direction of the fan blade of dynamic 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 include respectively two annular electros being arranged concentrically Polar ring.
Preferably：Speed limit 40km/h when the electric vehicle charging.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention installs by road, is carried by aircraft Terminal pad moves, and to make to establish connection between transmission guide rail and electric vehicle, and then charges to electric vehicle.When not carrying out When 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 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 of the direction front end in no charging tasks, 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 mounted on lower section 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 are disconnected 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 controlling aircraft carrying terminal pad and being 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, to make electronic vapour Vehicle charges；The advance turbin generator work that trolley component is controlled in charging process, makes trolley component be moved with electric automobile during traveling； Carry-on first electromagnet power-off is then controlled, aircraft disengages with terminal pad and carries out other tasks.When electric vehicle fills It controls after electricity after aircraft is moved to above trolley component and is connected with terminal pad, the second electromagnet in trolley component is disconnected Electricity, terminal pad and charging board disconnect, and subsequent aircraft carries terminal pad and parks to parking on disk.When the trolley in charging tasks When the trolley component for not carrying out charging tasks is parked in front of component, feeding back to server and sending move makes not charge Trolley component move forward, until charging in trolley component complete charging tasks.
The present invention is arranged by road, can in time charge to electric vehicle on road, not by time restriction, and drive Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；It is led by trolley and transmission of electricity Rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft, which carries, to be connected It connects disk to charge to electric vehicle, security risk when can avoid manual powered；When Rechargeable vehicle starts to charge up, aircraft with Terminal pad disconnects, compared to can more rationally be utilized in the case of aircraft and terminal pad one aircraft and save at This；The connection rail being connect with two vertical rail the same end ends makes trolley component complete charging tasks arrival side road pair It can be moved to above reversed track along connection rail after the end of rail should be found；The disk of parking is fixedly connected on electric vehicle, To store the terminal pad under non-charged state；The trolley under charged state is not carried out under off working state to electric vehicle Aircraft charging, and to aircraft offer store place.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention.
Fig. 2 is the structural schematic diagram of electric pole and guide rail.
Fig. 3 is the structural schematic diagram of electric vehicle charged state.
Fig. 4 is the structural schematic diagram of the non-charged state of electric vehicle.
Fig. 5 is the structural schematic diagram of trolley component.
Fig. 6 is the structural schematic diagram of feeding pannel.
Fig. 7, Fig. 8 are the structural scheme of mechanism of moving assembly.
Fig. 9, Figure 10 are the structural schematic diagrams of terminal pad.
Structural schematic diagram when Figure 11 is aircraft grounding state or carrying terminal pad.
Figure 12 is the structural schematic diagram under aircraft free flight state.
Figure 13 is the schematic cross-sectional view of aircraft.
Figure 14 is the portions the A schematic enlarged-scale view of Figure 13.
Figure 15 is the portions the B schematic enlarged-scale view of Figure 13.
The structural schematic diagram of each component that Figure 16 is upper shell and is connect with upper shell.
Figure 17 is the structural schematic diagram of lower housing section.
Figure 18 is the schematic cross-sectional view of lower housing section.
Figure 19 is the schematic cross-sectional view of undercarriage part.
Figure 20 is the decomposition texture schematic diagram of undercarriage part.
1, electric pole；11, mobile jib；12, cross bar；2, trolley component；21, moving assembly；211, supporting plate；2111, first is logical Hole；2112, the first connection electrode；212, riser；213, tilt prop；214, feeder wheel；215, advance turbin generator；216a, first Roller；216b, the second roller；216c, third roller；217, contact slipper；218, upper shifting board；22, feeding pannel；221, second Electromagnet；222, current electrode；223, the second through-hole；224, the second connection electrode；225, the first telltale mark；31, wire spool； 311, charging wire；32, disk is parked；321, ring electromagnet；322, insulation tank；323, the second telltale mark；4, terminal pad；41、 Iron block slot；42, annular iron block；43, the first receiving electrode；5, aircraft；51, main part；51a, upper shell；51b, lower housing； 510, fan mounting portion；5101, upper bracket；5102, lower bracket；5103, battery installation section；5104, circuit board installation cavity； 5105, air inlet hole；5106, vent；5107, camera；511, go out vane；5110, it rises and falls Holder joint；5111, vane upper casing Body；5112, vane lower housing；51121, interior curved wall；51122, dowel；51123, air outlet guard board；51124, training wall；512、 Connecting tube；5121, motor mounting plate；5122, valve plate guide rod；5123, baffle；513, cover board；52, accumulator；53, undercarriage； 531, connection pipe body；5311, hinged seat；5312, strip shape gob；532, sliding tube；5321, piston；5322, articulated joint；533, it seals Mouth cap；5331, spring positioning bar；534, connecting rod；535, supporting rod；5351, connecting rod tank；536, the first electromagnet；5361, Two receiving electrodes；537, spring；54, air intake cover；551, upper driving fan；552, lower driving fan；56, adjusting part；561、 Motor；562, screw rod；563, valve plate；57, control circuit board；6, guide rail；61, rail is found；62, bottom rail；63, head track；64, upper gear Plate；65, lower baffle plate；66, transmission guide rail；67, rail is connected.
Specific implementation mode
Embodiment 1
According to Fig. 1 to Figure 18, the present embodiment is a kind of pure electric automobile power supply system, includes multiple among the road etc. Away from the electric pole 1 being vertically installed among two-way lane, it is fixedly mounted on the guide rail 6 and more being located on electric pole above road A trolley component 2 being slidably connected on guide rail.
The trolley component include two moving assemblies being slidably connected on guide rail 21 and with two described mobile group The feeding pannel 22 of part rotation connection.
Wire spool 31 is installed at the top of Rechargeable vehicle；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 carrying terminal pad movement.
Each electric pole includes the upright bar 11 of vertical direction setting；The upright bar upper end is fixedly connected there are two direction The horizontally disposed cross bar in both sides of the road 12；The crossbar end is fixedly connected with the guide rail.
The guide rail includes two vertical rails 61 arranged in parallel, and is fixedly connected on the use of two vertical rail the same ends In the connection rail 67 of the arc of trolley component turning commutation；The vertical rail and the connection rail upper end form head track 63； The vertical rail and the connection rail lower end form bottom rail 62；The head track end forms the overhead gage 64 being directed downward；Institute It states bottom rail end and forms the lower baffle plate 65 of direction upward；The vertical rail and the connection rail lateral surface are installed with transmission of electricity and lead Rail 66.
The moving assembly is connect with the feeding pannel by pin rotation；The moving assembly includes for installing power supply The supporting plate 211 of disk；The supporting plate lower end forms the tilt prop 213 for being used to support trolley component；The tilt prop end installation There are multiple the first roller 216a that connection is rolled with the lower baffle plate lateral surface；The supporting plate upper surface forms riser 212；Institute It states riser upper end and forms upper shifting board 218；The supporting plate be located in guide rail with the upper shifting board be respectively equipped with it is small for making The feeder wheel 214 that vehicle component advances；The feeder wheel being installed on upper shifting board is connect with side roll in the overhead gage, peace It rolls and connects with the vertical rail loaded on the feeder wheel on supporting plate；The upper shifting board upper surface is equipped on multiple and described Baffle lower end rolls the third roller 216c of connection；The supporting plate lower face is equipped with multiple rolled with the lower baffle plate upper end and connects The the second roller 216b connect；It is equipped at the supporting plate feeder wheel corresponding with the upper shifting board for driving the advance Take turns the advance turbin generator 215 of rotation；The riser is located to be equipped in the guide rail to be connect with what the transmission guide rail was slidably connected Touch sliding block 217；The supporting plate is equipped with the first connection electrode for being connect with the feeding pannel far from described guide rail one end 2112；First connection electrode center forms first through hole 2111；The feeding pannel upper surface is fixedly connected with the second electricity Magnet 221；The current electrode 222 of annular is installed on second electromagnet；The feeding pannel corresponds to two described mobile group There are two the second through-holes 223 for molding at the first through hole of part；The feeding pannel lower end corresponds to the first of two moving assemblies There are two the second connection electrodes 224 for installation at connection electrode；Feeding pannel upper surface center is painted with for supplying the flight First telltale mark 225 of device positioning.The feeder wheel positioned at guide rail interior makes the trolley component be slided along the guide rail, Mutually being butted on respectively by the feeder wheel on the inside of vertical trackside face and overhead gage prevents the moving assembly from rolling；Two moving assemblies On the feeder wheel and charging board on second through-hole junction between form quadrilateral structure, by connect rail when The trolley component can be enable to pass through by the deformation of quadrangle, be limited by trolley entire length small.
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 slipper is transferred to feeding pannel by the first connection electrode and the second connection electrode, charging wire is transferred to through terminal pad after It charges afterwards to electric vehicle.
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 of 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 bracket 5102, is installed on the lower bracket 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 form wind pressure in vane.
It is described go out vane include sealed connection vane upper shell 5111 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 The lower end width in narrow outlet air gap under width, 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 horizontal wind-force and the fan blade of upper driving fan that the wind for forming the angle of 5-20 degree, and going out the outlet air gap blowout of vane generates 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 with control circuit board 57 respectively.
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 upper shell 51a and lower housing 51b is tightly connected and constitutes.
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, to realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only play tune The effect of whole attitude of flight vehicle goes out when vane generates touching with foreign object without the fan for being provided with power 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, it is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction and water of vane The horizontal wind-force and upper driving wind that the wind for forming the angle of 5-20 degree square between, and going out the outlet air gap blowout of vane generates The rotation direction of the fan blade of fan is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset The reaction force that driving fan and lower driving fan generate when rotating；Also, change by adjusting each adjusting part simultaneously Vane go out wind velocity, it can be achieved that aircraft whole forward or reverse.Make one by adjusting one or two adjusting part It is a or two go out vane go out wind velocity, it can be achieved that aircraft is generally in heeling condition, can be driven aircraft in this way in water Square to flight.
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 connection of circuit board installation cavity lower end Cover board 513；The upper surface of the circuit board installation cavity uniformly forms the air inlet hole 5105 being connected to 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 forms 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 it is connected to the first electromagnet 536 far from Holder joint one end of rising and falling on supporting rod, 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, is risen to the control circuit board 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, the first connection electrode, the second connection electrode include respectively two concentric The annular electro polar ring of setting.
Speed limit 40km/h when the electric vehicle charging.
The present invention installs by road, terminal pad movement is carried by aircraft, 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 disk is parked, 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 that aircraft and feeding pannel is made to connect 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 feeds back electric vehicle and open to trolley component of the direction of traffic front end in no charging tasks Side, at the same by server to rest in the trolley component or the aircraft nearest apart from the trolley component send instruction, The terminal pad upper end that aircraft is artificially controlled by the camera mounted on lower section and the electric vehicle that flies to is connected, it is described to fly 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 makes charging wire extend, while controlling aircraft and carrying terminal pad shifting 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, to make electric vehicle 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 power-off is then controlled, Aircraft disengages with terminal pad and carries out other tasks.Aircraft is controlled after electric vehicle charges to be moved in trolley component 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 trolley group for not carrying out charging tasks is parked in front of the trolley component in charging tasks When part, feeds back to server and sending move makes the trolley component not charged move forward, until small in charging Vehicle component completes charging tasks.
The present invention is arranged by road, can in time charge to electric vehicle on road, not by time restriction, and drive Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；It is led by trolley and transmission of electricity Rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft, which carries, to be connected It connects disk to charge to electric vehicle, security risk when can avoid manual powered；When Rechargeable vehicle starts to charge up, aircraft with Terminal pad disconnects, compared to can more rationally be utilized in the case of aircraft and terminal pad one aircraft and save at This；The connection rail being connect with two vertical rail the same end ends makes trolley component complete charging tasks arrival side road pair It can be moved to above reversed track along connection rail after the end of rail should be found；The disk of parking is fixedly connected on electric vehicle, To store the terminal pad under non-charged state；The trolley under charged state is not carried out under off working state to electric vehicle Aircraft charging, and to aircraft offer store place.
Embodiment 2
According to Figure 19 to Figure 20, 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 include be fixedly connected with Holder joint of rising and falling and by rise and fall Holder joint with go 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 is connected on supporting rod far from first electromagnet 536 of Holder joint one end of rising and falling, and respectively with sliding The connecting rod 534 being rotatablely connected in the middle part of pipe, in the middle part of supporting rod；It is equipped with below first electromagnet for charging to aircraft 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, sliding pipe outer wall middle part position close to Holder joint one end of rising and falling It sets 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 It is connected to sealing cap 533, 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 when state.
The spring is in supporting rod when extended configuration and is in unfolded state, 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 with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, go out Wind pressure in vane makes piston be moved to sealing cap one end together with sliding tube, to make sliding tube drive connecting rod one end to sealing cap Direction is moved, to make supporting rod lower end also be rotated to sealing cap one end, to make undercarriage be in collapsed state.Work as aircraft When landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved toward hinged seat direction together with piston, to make sliding tube Connecting rod one end is driven to be moved to hinged seat direction, to make supporting rod lower end turn to extreme position to hinged seat one end, to Undercarriage is set 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 makes spring 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 carries 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 (4)

1. a kind of pure electric automobile power supply system, it is characterised in that：Include it is multiple be equidistantly vertically installed among the road it is double To the electric pole among track, it is fixedly mounted on electric pole and is located at the guide rail above road and multiple is slidably connected at guide rail On trolley component；
Each electric pole includes the upright bar of vertical direction setting；The upright bar upper end is fixedly connected with that there are two towards road two The horizontally disposed cross bar in side；The crossbar end is fixedly connected with the guide rail；
The guide rail includes two vertical rails arranged in parallel, and be fixedly connected on two vertical rail the same ends for described The connection rail of the arc of trolley component turning commutation；The vertical rail and the connection rail upper end form head track；The vertical rail and The connection rail lower end forms bottom rail；The head track end forms the overhead gage being directed downward；The bottom rail end molding There is the lower baffle plate of direction upward；The vertical rail and the connection rail lateral surface are installed with transmission guide rail；
The trolley component includes two moving assemblies being slidably connected on guide rail and is rotated with two moving assemblies The feeding pannel of connection；The moving assembly is connect with the feeding pannel by pin rotation；The moving assembly includes for pacifying Fill the supporting plate of feeding pannel；The supporting plate lower end forms the tilt prop for being used to support trolley component；The tilt prop end installation There are multiple the first rollers that connection is rolled with the lower baffle plate lateral surface；The supporting plate upper surface forms riser；The riser Upper end forms upper shifting board；The supporting plate, which is located at the upper shifting board in guide rail, to be respectively equipped with for making trolley component advance Feeder wheel；The feeder wheel being installed on upper shifting board is connect with side roll in the overhead gage, is installed on supporting plate The feeder wheel is rolled with the vertical rail and is connected；The upper shifting board upper surface is equipped with the multiple and overhead gage lower end and rolls The third roller of connection；The supporting plate lower face is equipped with multiple the second rollers that connection is rolled with the lower baffle plate upper end；Institute State the advance turbin generator being equipped at the supporting plate feeder wheel corresponding with the upper shifting board for driving the feeder wheel rotation； The riser, which is located in the guide rail, is equipped with the contact slipper being slidably connected with the transmission guide rail；The supporting plate is far from described Guide rail one end is equipped with the first connection electrode for being connect with the feeding pannel；First connection electrode center forms One through-hole；The feeding pannel upper surface is fixedly connected with the second electromagnet；The power supply of annular is installed on second electromagnet Electrode；The feeding pannel corresponds to molding at the first through hole of two moving assemblies, and there are two the second through-holes；The feeding pannel Lower end corresponds to installation at the first connection electrode of two moving assemblies, and there are two the second connection electrodes；
Wire spool is installed at the top of Rechargeable vehicle；It is pierced by the charging wire for being useful for charging to electric vehicle on 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 is removable It is connected to described park in disk or the trolley component；Further include multiple aircraft for carrying 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 of 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 bracket, lower driving fan is installed on the lower bracket； 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 sealed connection vane upper shell and vane lower housing, the vane lower housing inner circumferential upper end at 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 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 go out the rotation of the horizontal wind-force and the fan blade of upper driving fan of the wind generation of the outlet air gap blowout of vane 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, the coaxially connected screw rod with motor output shaft, and the valve plate being connect with screw flight；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 at Type has to install the motor mounting plate of 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；There are one upper end directions to go out the inclined baffle in vane direction for lower part connection 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 with control circuit board respectively；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly formed on air intake cover strip into Air port；
The main part is that upper shell and lower housing are tightly connected and constitute；
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；The top for being located at battery installation section on the fan mounting portion is a circuit board installation cavity, the control circuit Plate is mounted in circuit board installation cavity, and there are one the cover boards of annular for the connection of circuit board installation cavity lower end；The circuit board peace The upper surface behaveing affectedly uniformly forms the air inlet hole being connected to 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；Installation below first electromagnet It is useful for the second receiving electrode to charge to aircraft.
2. a kind of pure electric automobile power supply system as described in claim 1, it is characterised in that：Feeding pannel upper surface center It 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 pure electric automobile power supply system as claimed in claim 2, it is characterised in that：The current electrode, first connect It includes two annular electro polar rings being arranged concentrically to receive electrode, the first connection electrode, the second connection electrode respectively.
4. a kind of pure electric automobile power supply system as claimed in claim 2, it is characterised in that：The electric vehicle charges the time limit Fast 40km/h.
CN201810109939.XA 2017-06-23 2017-06-23 A kind of pure electric automobile power supply system Withdrawn CN108312872A (en)

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