CN108556649A - A kind of power supply system for electric vehicle charging - Google Patents

A kind of power supply system for electric vehicle charging Download PDF

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Publication number
CN108556649A
CN108556649A CN201810112319.1A CN201810112319A CN108556649A CN 108556649 A CN108556649 A CN 108556649A CN 201810112319 A CN201810112319 A CN 201810112319A CN 108556649 A CN108556649 A CN 108556649A
Authority
CN
China
Prior art keywords
plate
fan
frame body
fixedly connected
vane
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Withdrawn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
CN201810112319.1A
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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 CN201810112319.1A priority Critical patent/CN108556649A/en
Publication of CN108556649A publication Critical patent/CN108556649A/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Withdrawn legal-status Critical Current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
    • B60L53/30—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
    • 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
    • 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
    • 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
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles
    • 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
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles
    • Y02T90/167—Systems integrating technologies related to power network operation and communication or information technologies for supporting the interoperability of electric or hybrid vehicles, i.e. smartgrids as interface for battery charging of electric vehicles [EV] or hybrid vehicles [HEV]
    • 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
    • Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
    • Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
    • Y04S30/00—Systems supporting specific end-user applications in the sector of transportation
    • Y04S30/10—Systems supporting the interoperability of electric or hybrid vehicles
    • Y04S30/12—Remote or cooperative charging

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention belongs to electric vehicle charging fields, more particularly to a kind of power supply system for electric vehicle charging, include multiple electric poles being equidistantly vertically installed at along road by road, it is fixedly mounted on the guide rail being located on electric pole above road, multiple trolley components being slidably connected on guide rail, the terminal pad being connect with each trolley component, the aircraft being movably connected in above terminal pad, and travel the electric vehicle on road.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 power supply system for electric vehicle charging
Technical field
The invention belongs to electric vehicle charging fields, and in particular to a kind of power supply system for electric vehicle charging.
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 one kind for electronic vapour The power supply system of vehicle charging.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of confession for electric vehicle charging Electric system includes multiple electric poles being equidistantly vertically installed at along road by road, 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；Transmission guide rail is installed in the guide rail；
The trolley component includes the upper frame body and lower frame body being fixedly connected up and down, the wire-winding unit being mounted in upper frame body, sliding The dynamic sliding arc plate being connected in lower frame body, is fixedly connected on upper frame body upper end and is connect with what the transmission guide rail was slidably connected The charging wire for touching sliding plate and being wrapped on the wire-winding unit；
The charging wire end is fixedly connected with the terminal pad for being useful for charging to electric vehicle；Further include it is multiple for carry connection The aircraft of disk movement.
Preferably：Each electric pole includes the upright bar of vertical direction setting；The upper part of telegraph pole is fixed It is connected with towards what road direction was arranged and parks disk；The upright bar upper end is fixedly connected with towards the horizontally disposed cross of road direction Bar；The crossbar end is fixedly connected with the guide rail；
The guide rail includes the upper connection rail for being fixedly connected on each cross bar lower end；The upper connection rail both ends form perpendicular Straight two downward sides connect rail；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail, the traveling It is in T fonts that rail, which connect rail with the side,；The transmission guide rail is fixedly connected on the traveling on the inside of side connection rail Rail upper end；
There are two side plates for upper frame body both sides symmetrical molding；Two side plate inside middle portions are integrally formed with connecting plate；Two It is rotatably connected to multiple feeder wheels being equally spaced on the inside of a side plate upper end；Corresponding each advance on the outside of the side plate Multiple first motors for driving the feeder wheel rotation are fixedly connected at wheel；The trolley component passes through the feeder wheel It is moved on the traveling rail on the outside of the side plate；The contact sliding plate is fixedly connected on upper end in the middle part of connecting plate；On described Framework one end forms upper frame body end plate between the connecting plate and two side plates；It is molded on the upper frame body end plate It is useful for that the first mounting hole of the wire-winding unit is installed；The upper frame body forms mounting plate close to the other end；The peace Second mounting hole coaxial with first mounting hole is formed in loading board；Two side plate interior sides lower parts are close to middle part and position Electrode slice there are two being nearby fixedly connected in the mounting plate；
The mounting plate is fixedly connected with the second motor far from upper frame body end plate side；On the output shaft of second motor It is fixedly connected with installation axle, the installation axle is rotatably connected in first mounting hole and second mounting hole；Institute It states to be fixedly connected in the middle part of installation axle and forms externally threaded screw thread disk；The screw thread disk is close far from second motor side Multiple first limit switches are installed along the installation axle is circumferentially equidistant at screw thread plate edge；The installation axle is located at the installation Plate side is fixedly connected with incoming panel；There are two the slot electrodes for the annular being mutually parallel for the incoming panel outer circumferential installation；Two A electrode slice is plugged on respectively in two slot electrodes；The screw thread disk diameter is more than the incoming panel；The charging Line winding is in the installation axle between the screw thread disk and the incoming panel；
The lower frame body is isometric with the upper frame body and is arc；Lower frame body one end corresponding with the upper frame body end plate at Type has lower frame body end plate；The second limit switch is installed on the inside of the lower frame body end plate marginal center；The lower frame body madial wall There are two the sliding grooves being slidably connected for the sliding arc plate for symmetrical molding along its length；
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inner wall form with it is described The internal thread that screw thread disk is threadedly coupled；The sliding arc plate forms pressing end plate close to lower frame body end plate one end；It is described Sliding arc plate forms smooth plate far from described pressing end plate one end；The sliding arc plate lateral wall correspond at the sliding groove at Type has slider bar；The outlet hole for being passed through for the charging wire is formed on the smooth plate；
The lower frame body is corresponded to form along its length at the outlet hole and be passed through for the charging wire being pierced by from the outlet hole Strip-shaped hole；Bar shaped hole width is more than or equal to outlet hole aperture；
Described charging wire one end is electrically connected with the slot electrode of the wire-winding unit, the charging wire other end through the outlet hole and Strip-shaped hole is pierced by；
Agv controller for controlling the first motor and second motor rotation is installed in the upper frame body；It is described First motor, the second motor, the first limit switch, the second limit switch are electrically connected with agv controller；
Electric current is exported from transmission guide rail, by contacting sliding plate, is transferred to after electrode slice and is transferred to charging wire by slot electrode, finally Reach terminal pad；
The electric vehicle upper end is equipped with charging board；The charging board upper end is equipped with the first receiving electrode；The charging board Upper end be located at be fixedly connected on the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnet；
The insulation tank parked disk upper end and form annular；It is described park disk upper end and be located on the outside of the insulation tank be fixedly connected There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through-hole；The terminal pad lower end corresponds to and is equipped with the first confession at first receiving electrode Electrode；The take-up reel lower end is equipped with iron block corresponding with each second electromagnet position；In the terminal pad End periphery is fixedly connected with the annular iron block for being useful for being connect with terminal pad for aircraft；It is described annular iron block on be equipped with it is described Corresponding second current electrode of second receiving electrode；
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；
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 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 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.
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 annular iron block center line is corresponding after being unfolded with the aircraft support bar Circumscribed circle diameter where the rectangle that first electromagnet is connected to is equal.
Preferably：First current electrode, the second current electrode, the first receiving electrode, the second receiving electrode Include respectively two annular electro polar rings being arranged concentrically.Installation on the position of brush is corresponded in the brush, and there are two set with one heart The annular electro polar ring set.
Preferably：The end terrain clearance of trying to get to the heart of a matter of parking is 3.5-4m.
Preferably：Speed limit 40km/h when the electric vehicle charging.
Preferably：The through-hole diameter is more than the accumulator outer diameter.
Preferably：The screw pitch of the screw thread disk is equal with the line footpath of the charging wire.
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 power transmission line and electric vehicle, and then charges to electric vehicle.When not filled When electric task, terminal pad, which is parked in, parks on disk, so that terminal pad is connect with disk is parked by the way that iron block and permanent magnet are attracting, and described One current electrode is plugged in the insulation tank, and sliding arc plate is located at lower frame body end plate one end and offsets with the second limit switch Place, the charging wire are wound to most short extension elongation state, while the first electromagnet and ring without the aircraft under aerial mission Shape iron block is attracting to make aircraft be connect with terminal pad, and the second current electrode connect to carry out aircraft with the second receiving electrode Charging.When electric vehicle not enough power supply, below electric automobile during traveling to guide rail, and the letter of charge request is sent to server Number, after server receives charge request signal, according to the location of electric vehicle, and feeds back electric vehicle and open to driving side Below the trolley component that remains static to front end, while being adjusted the distance the nearest aircraft of the trolley component by server Instruction is sent, aircraft is by the way that artificially control is flown in the terminal pad that the trolley component is connected mounted on the camera of lower section End, the second electromagnet power-off during the aircraft declines on the electric vehicle, each first electromagnet and annular iron Block is attracting to make aircraft be connected with terminal pad；Server gives agv controller to send instruction, agv controller control the simultaneously The extension elongation of two motor reversals, charging wire increases, while controlling aircraft carrying terminal pad and being moved to above electric vehicle, this When electric vehicle on the second electromagnet be powered, control aircraft decline so that the first current electrode is connect with the first receiving electrode, To make electric vehicle charge, then control aircraft, which drives, connects disc spins, on the iron block and charging board for making terminal pad lower end The second electromagnet it is attracting, to make terminal pad be fixed on charging board；The first motor of trolley component is controlled in charging process Work, makes trolley component be moved with electric automobile during traveling, the second motor stops after sliding arc plate is touched to the first limit switch Only work；Carry-on first electromagnet power-off is then controlled, aircraft disengages with terminal pad and carries out other tasks.When electronic Automobile controls after charging after aircraft is moved to above electric vehicle to be connected with terminal pad, the second electricity on electric vehicle Magnet powers off, and terminal pad and charging board disconnect, subsequent aircraft carry terminal pad be connected on subsequent electric vehicle charging or Person parks terminal pad to parking on disk；Electric vehicle charging finishes and when without charging tasks, and server is to trolley component and flies Row device sends instruction, and aircraft judges and carry terminal pad and park to nearest to park on disk by camera, while trolley control Device processed control first motor is moved near the nearest electric pole parked where disk, and the second motor rotates forward, and charging wire twines Around on reel, stop after finally touching to the second limit switch.When aircraft charges, pass through the camera shooting below aircraft Head judges to be parked in the terminal pad parked on disk, controls aircraft and be moved to above the terminal pad, then drop to the terminal pad On keep the first electromagnet attracting to be attached to aircraft with annular iron block, while the second current electrode received with second it is electric Pole is electrically connected, to charge to aircraft.
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；By trolley component with it is defeated Conductance rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Wire-winding unit The form being connected through a screw thread with sliding arc plate, make in charging wire winding process can close proper alignment, during unwrapping wire again It can be passed through from line outlet, to reduce the friction of charging wire outer layer；Aircraft carries terminal pad and charges to electric vehicle, energy Security risk when enough avoiding manual powered；When Rechargeable vehicle starts to charge up, aircraft is disconnected with terminal pad, compared to Aircraft and cost-effective can be more rationally utilized in the case of aircraft and terminal pad one；The disk of parking is fixedly connected On utility poles, make that storage need not be fixed to terminal pad that electric vehicle charges, without be suspended from it is aerial cause to generate it is hidden Suffer from；Terminal pad fixation is stored in when parking on disk, can be charged simultaneously to the aircraft under off working state, 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.
Fig. 4 is the structural schematic diagram of trolley component.
Fig. 5 is the decomposition texture schematic diagram of trolley component.
Fig. 6 is the schematic cross-sectional view of upper frame body.
Fig. 7 is the structural schematic diagram of sliding arc plate.
Fig. 8 is the structural schematic diagram of lower frame body.
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, disk is parked；121, permanent magnet；122, insulation tank；13, cross bar；2, trolley component； 21, upper frame body；211, side plate；2111, electrode slice；212, connecting plate；213, feeder wheel；2131, first motor；214, upper frame body End plate；2141, the first mounting hole；215, mounting plate；2151, the second mounting hole；22, wire-winding unit；221, screw thread disk；2211、 First limit switch；222, the second motor；223, installation axle；224, incoming panel；2241, slot electrode；23, lower frame body；231, under Framework end plate；2311, the second limit switch；2312, sliding groove；2313, strip-shaped hole；24, sliding plate is contacted；25, sliding arc plate； 251, internal thread；252, slider bar；253, smooth plate；2531, outlet hole；254, end plate is pressed；26, charging wire；31, it charges Disk；32, the first receiving electrode；33, the second electromagnet；4, terminal pad；41, annular iron block；42, the first current electrode；43, iron Block；44, the second current electrode；45, through-hole；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 shell；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, sealing cap；5331, spring Locating rod；534, connecting rod；535, supporting rod；5351, connecting rod tank；536, the first electromagnet；5361, the second receiving electrode； 537, spring；54, air intake cover；551, upper driving fan；552, lower driving fan；56, adjusting part；561, motor；562, spiral shell Bar；563, valve plate；57, control circuit board；6, guide rail；61, upper connection rail；62, side connects rail；63, traveling rail；64, transmission of electricity is led Rail.
Specific implementation mode
Embodiment 1
According to Fig. 1 to Figure 20, the present embodiment is a kind of power supply system for electric vehicle charging, includes multiple along road Road is equidistantly vertically installed at the electric pole 1 by road, is fixedly mounted on the guide rail 6 and multiple being located on electric pole above road The trolley component 2 being slidably connected on guide rail；Transmission guide rail 64 is installed in the guide rail.
The trolley component includes the upper frame body 21 being fixedly connected up and down and lower frame body 23, the coiling being mounted in upper frame body Component 22, the sliding arc plate 25 being slidably connected in lower frame body, be fixedly connected on upper frame body upper end and with the transmission guide rail The contact sliding plate 24 being slidably connected and the charging wire 26 being wrapped on the wire-winding unit.
The charging wire end is fixedly connected with the terminal pad 4 for being useful for charging to electric vehicle；The invention also includes multiple Aircraft 5 for carrying terminal pad movement.
Each electric pole includes the upright bar 11 of vertical direction setting；The upper part of telegraph pole is fixedly connected with towards road Disk 12 is parked in direction setting；The upright bar upper end is fixedly connected with towards the horizontally disposed cross bar of road direction 13；The cross Boom end is fixedly connected with the guide rail.
The guide rail includes the upper connection rail 61 for being fixedly connected on each cross bar lower end；The upper connection rail both ends at Type has two sides straight down to connect rail 62；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail 63, it is in T fonts that the traveling rail, which connect rail with the side,；The transmission guide rail is fixedly connected on the inside of side connection rail Traveling rail upper end.The transmission guide rail is arranged in the guide rail interior, prevents human or animal from directly being connect with transmission guide rail It touches and electric shock accidents occurs.
There are two side plates 21 for upper frame body both sides symmetrical molding；Two side plate inside middle portions are integrally formed with connection Plate 212, the connecting plate are the circular arc to arch upward upwards；Multiple be equally spaced is rotatably connected on the inside of two side plate upper ends Feeder wheel 213；It is fixedly connected at corresponding each feeder wheel on the outside of the side plate multiple for driving the advance to rotate Dynamic first motor 2131；The trolley component is moved by the feeder wheel on the traveling rail on the outside of the side plate； The contact sliding plate is fixedly connected on upper end in the middle part of connecting plate；Described upper frame body one end is located at the connecting plate and two sides Upper frame body end plate 214 is formed between plate；The first peace for installing the wire-winding unit is formed on the upper frame body end plate Fill hole 2141；The upper frame body forms mounting plate 215 close to the other end；It is formed on the mounting plate and first peace Fill the second coaxial mounting hole 2151 of hole；Two side plate interior sides lower parts are close to middle part and fixed nearby positioned at the mounting plate There are two electrode slices 2111 for connection.
The mounting plate is fixedly connected with the second motor 222 far from upper frame body end plate side；Second motor Installation axle 223 is fixedly connected on output shaft, the installation axle is rotatably connected on first mounting hole and described second In mounting hole；It is fixedly connected in the middle part of the installation axle and forms externally threaded screw thread disk 221；The screw thread disk is far from described Two motor sides are equipped with multiple first limit switches 2211 along the installation axle is circumferentially equidistant at screw thread plate edge；It is described Installation axle is located at the mounting plate side and is fixedly connected with incoming panel 224；There are two mutually for the incoming panel outer circumferential installation The slot electrode 2241 of parallel annular；Two electrode slices are plugged on respectively in two slot electrodes；The screw thread disk is straight Diameter is more than the incoming panel；The screw pitch of the screw thread disk is equal with the line footpath of the charging wire；The charging wire winding is located at institute It states in the installation axle between screw thread disk and the incoming panel.
The lower frame body is isometric with the upper frame body and is arc；The lower frame body and the upper frame body end plate corresponding one End forms lower frame body end plate 231；The second limit switch 2311 is installed on the inside of the lower frame body end plate marginal center；Under described There are two the sliding grooves 2312 being slidably connected for the sliding arc plate for symmetrical molding along its length for framework madial wall.
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inner wall form with The internal thread 251 that the screw thread disk is threadedly coupled；The sliding arc plate forms press-side close to lower frame body end plate one end Plate 254；The sliding arc plate forms smooth plate 253 far from described pressing end plate one end；The sliding arc plate lateral wall corresponds to Slider bar 252 is formed at the sliding groove；The outlet hole for being passed through for the charging wire is formed on the smooth plate 2531。
The lower frame body corresponds to the charging wire formed along its length at the outlet hole for being pierced by from the outlet hole The strip-shaped hole 2313 passed through；Bar shaped hole width is more than or equal to outlet hole aperture.
Described charging wire one end is electrically connected with the slot electrode of the wire-winding unit, and the charging wire other end is through the outlet Hole and strip-shaped hole are pierced by.
Agv controller for controlling the first motor and second motor rotation is installed in the upper frame body； The first motor, the second motor, the first limit switch, the second limit switch are electrically connected with agv controller.
The screw pitch of the screw thread disk is equal with the line footpath of the charging wire.When second motor rotates forward, the charging Line is wrapped between the screw thread disk and the incoming panel, since the threaded connection between the screw thread disk and the internal thread makes The sliding arc plate is slided along the sliding groove, the thread rotary orientation phase of the direction of rotation and the screw thread disk of the charging wire winding Together, and since the diameter in section of screw pitch and charging wire of screw thread disk is equal, the charging wire winds around the coiling On cylinder, the pressing end plate lateral surface described in the sliding arc plate sliding process is touched and presses the second limit switch, agv controller Second motor is controlled to be stopped；When second motor reversal, the charging wire rotates unwrapping wire and from the outlet It is pierced by hole and the strip-shaped hole, it is described to fill since the screw pitch of the screw thread disk is equal with the diameter in the section of the charging wire The point being detached from from winding place when wire releasing synchronizing moving with the sliding of sliding arc plate, is in above the outlet hole always, End plate medial surface is pressed in sliding arc plate slipping and touch and press first limit switch, described in agv controller controls Second motor is stopped.Sliding arc plate is set to be slided while wire-winding unit rotates by the threaded connection of screw thread disk and internal thread It is dynamic, and due to the setting of screw pitch makes can be closely wound in charging wire winding process and it is mixed and disorderly to prevent, and charging wire be detached from around It is pierced by, and bar shaped hole width is more than outlet hole aperture, therefore can reduce even from outlet hole during the defence line of spool Avoid the friction between charging wire and outlet hole to protect charging wire.
Electric current is exported from transmission guide rail, by contact sliding plate, is transferred to after electrode slice and is transferred to charging wire by slot electrode, Finally reach terminal pad.
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 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 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.
The electric vehicle upper end is equipped with charging board 31；The charging board upper end is equipped with the first receiving electrode 32；Institute State charging board upper end be located at be fixedly connected on the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnetism Iron 33.
The insulation tank 122 parked disk upper end and form annular；The disk upper end of parking is located on the outside of the insulation tank Be fixedly connected with circumferentially be equally spaced have multiple permanent magnets 121.
The terminal pad is carried and is moved by the aircraft and charged to the electric vehicle.When the aircraft carries When the terminal pad movement, the aircraft is connect with the terminal pad upper end；When the electric vehicle charging, the charging board It is connect with the terminal pad lower end.
The terminal pad intermediary form has through-hole 45, the through-hole diameter to be more than the accumulator outer diameter；The terminal pad Lower end, which corresponds to, is equipped with the first current electrode 42 at first receiving electrode；The take-up reel lower end is equipped with corresponding each institute State the iron block 43 of the second electromagnet；Terminal pad upper end periphery is fixedly connected with the ring for being useful for being connect with terminal pad for aircraft Shape iron block 41, corresponding first electromagnetism iron phase after diameter of a circle where the annular iron block center line is unfolded with the aircraft support bar Circumscribed circle diameter where the rectangle being linked to be is equal；The annular iron block corresponds to is equipped with the second confession at second receiving electrode Electrode 44.
The aircraft, trolley component, electric vehicle are connected by wireless signal and the server communication of system.
The end terrain clearance of trying to get to the heart of a matter of parking is 3.5-4m.
First current electrode, the second current electrode, the first receiving electrode, the second receiving electrode include respectively two The annular electro polar ring being arranged concentrically.Installation on the position of brush is corresponded in the brush, and there are two the annular electrodes being arranged concentrically Ring.
Speed limit 40km/h when the electric vehicle charging.
The present invention installs by the road, and terminal pad movement is carried by aircraft, to make power transmission line and electric vehicle it 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, passes through Iron block and permanent magnet is attracting that terminal pad is made to be connect with disk is parked, first current electrode is plugged in the insulation tank, sliding Arc plate is located at lower frame body end plate one end and offsets place with the second limit switch, and the charging wire is wound to most short extension elongation shape State, while iron block is attracting that aircraft is made to be connect with terminal pad with annular for the first electromagnet without the aircraft under aerial mission, the Two current electrodes 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 under the trolley component to remain static to direction of traffic front end Side, while instruction is sent by the server nearest aircraft of the trolley component of adjusting the distance, aircraft passes through mounted on lower section Camera artificially controls the terminal pad upper end that the trolley component of flying to is connected, the electronic vapour during the aircraft declines The second electromagnet power-off on vehicle, each first electromagnet with annular iron block is attracting that aircraft is made to be connected with terminal pad；Simultaneously Server sends to agv controller and instructs, and agv controller controls the second motor reversal, and the extension elongation of charging wire increases, together When control aircraft carry terminal pad and be moved to above electric vehicle, the second electromagnet on electric vehicle is powered at this time, control Aircraft decline makes the first current electrode be connect with the first receiving electrode, to make electric vehicle charge, then controls aircraft Connection disc spins are driven, keep the second electromagnet on the iron block and charging board of terminal pad lower end attracting, to make terminal pad fix On charging board；The first motor work that trolley component is controlled in charging process, makes trolley component be moved with electric automobile during traveling Dynamic, the second motor is stopped after sliding arc plate is touched to the first limit switch；Then control carry-on first electromagnetism Iron powers off, and aircraft disengages with terminal pad and carries out other tasks.Aircraft, which is controlled, after electric vehicle charges is moved to electricity It is connected with terminal pad after above electrical automobile, the second electromagnet power-off on electric vehicle, terminal pad is disconnected with charging board, then Aircraft carries terminal pad and is connected on subsequent electric vehicle charging or parks terminal pad to parking on disk；Electric vehicle Charging finishes and when without charging tasks, and server sends instruction to trolley component and aircraft, and aircraft is judged by camera And carry terminal pad and park to nearest and park on disk, while agv controller control first motor is moved to and nearest parks disk Near the electric pole at place, and the second motor rotates forward, and charging wire is wound on reel, finally touches to the second limit switch After stop.When aircraft charges, the terminal pad parked on disk is parked in by the camera judgement below aircraft, control flies Row device is moved to above the terminal pad, and then droping in the terminal pad keeps the first electromagnet attracting to flying with annular iron block Row device is attached, while the second current electrode is electrically connected with the second receiving electrode, to charge to aircraft.
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；By trolley component with it is defeated Conductance rail, which is connected, powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Wire-winding unit The form being connected through a screw thread with sliding arc plate, make in charging wire winding process can close proper alignment, during unwrapping wire again It can be passed through from line outlet, to reduce the friction of charging wire outer layer；Aircraft carries terminal pad and charges to electric vehicle, energy Security risk when enough avoiding manual powered；When Rechargeable vehicle starts to charge up, aircraft is disconnected with terminal pad, compared to Aircraft and cost-effective can be more rationally utilized in the case of aircraft and terminal pad one；The disk of parking is fixedly connected On utility poles, make that storage need not be fixed to terminal pad that electric vehicle charges, without be suspended from it is aerial cause to generate it is hidden Suffer from；Terminal pad fixation is stored in when parking on disk, can be charged simultaneously to the aircraft under off working state, and to aircraft Offer store place.
Embodiment 2
The present embodiment has done following improvement on the basis of embodiment 1：Go out position of the vane inner circumferential far from connecting tube described in each Form Holder joint 5110 of rising and falling, respectively there are one undercarriages 53 for connection in each Holder joint of rising and falling；The undercarriage includes Have and is fixedly connected with Holder joint of rising and falling and is pacified with the connection pipe body 531 being connected inside vane, sliding is gone out by rising and falling Holder joint Sliding tube 532 in connection pipe body, with connection pipe body close to the supporting rod 535 for Holder joint one end rotation connection of rising and falling, even Be connected on supporting rod far from first electromagnet 536 of Holder joint one end of rising and falling, and respectively in the middle part of sliding tube, in the middle part of supporting rod The connecting rod 534 of rotation connection；The second receiving electrode 5361 for charging to aircraft is installed below first electromagnet.
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 annular iron block are attracting, but outlet air The power that wind pressure in ring generates is insufficient to allow supporting rod to pack up.

Claims (3)

1. a kind of power supply system for electric vehicle charging, it is characterised in that：Include multiple equidistantly vertically-mounted along road Electric pole by road is fixedly mounted on electric pole and is located at the guide rail above road and multiple is slidably connected on guide rail Trolley component；Transmission guide rail is installed in the guide rail；
The trolley component includes the upper frame body and lower frame body being fixedly connected up and down, the wire-winding unit being mounted in upper frame body, sliding The dynamic sliding arc plate being connected in lower frame body, is fixedly connected on upper frame body upper end and is connect with what the transmission guide rail was slidably connected The charging wire for touching sliding plate and being wrapped on the wire-winding unit；
The charging wire end is fixedly connected with the terminal pad for being useful for charging to electric vehicle；Further include it is multiple for carry connection The aircraft of disk movement；
Each electric pole includes the upright bar of vertical direction setting；The upper part of telegraph pole, which is fixedly connected with towards road direction, to be set That sets parks disk；The upright bar upper end is fixedly connected with 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 the upper connection rail for being fixedly connected on each cross bar lower end；The upper connection rail both ends form perpendicular Straight two downward sides connect rail；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail, the traveling It is in T fonts that rail, which connect rail with the side,；The transmission guide rail is fixedly connected on the traveling on the inside of side connection rail Rail upper end；
There are two side plates for upper frame body both sides symmetrical molding；Two side plate inside middle portions are integrally formed with connecting plate；Two It is rotatably connected to multiple feeder wheels being equally spaced on the inside of a side plate upper end；Corresponding each advance on the outside of the side plate Multiple first motors for driving the feeder wheel rotation are fixedly connected at wheel；The trolley component passes through the feeder wheel It is moved on the traveling rail on the outside of the side plate；The contact sliding plate is fixedly connected on upper end in the middle part of connecting plate；On described Framework one end forms upper frame body end plate between the connecting plate and two side plates；It is molded on the upper frame body end plate It is useful for that the first mounting hole of the wire-winding unit is installed；The upper frame body forms mounting plate close to the other end；The peace Second mounting hole coaxial with first mounting hole is formed in loading board；Two side plate interior sides lower parts are close to middle part and position Electrode slice there are two being nearby fixedly connected in the mounting plate；
The mounting plate is fixedly connected with the second motor far from upper frame body end plate side；On the output shaft of second motor It is fixedly connected with installation axle, the installation axle is rotatably connected in first mounting hole and second mounting hole；Institute It states to be fixedly connected in the middle part of installation axle and forms externally threaded screw thread disk；The screw thread disk is close far from second motor side Multiple first limit switches are installed along the installation axle is circumferentially equidistant at screw thread plate edge；The installation axle is located at the installation Plate side is fixedly connected with incoming panel；There are two the slot electrodes for the annular being mutually parallel for the incoming panel outer circumferential installation；Two A electrode slice is plugged on respectively in two slot electrodes；The screw thread disk diameter is more than the incoming panel；The charging Line winding is in the installation axle between the screw thread disk and the incoming panel；
The lower frame body is isometric with the upper frame body and is arc；Lower frame body one end corresponding with the upper frame body end plate at Type has lower frame body end plate；The second limit switch is installed on the inside of the lower frame body end plate marginal center；The lower frame body madial wall There are two the sliding grooves being slidably connected for the sliding arc plate for symmetrical molding along its length；
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inner wall form with it is described The internal thread that screw thread disk is threadedly coupled；The sliding arc plate forms pressing end plate close to lower frame body end plate one end；It is described Sliding arc plate forms smooth plate far from described pressing end plate one end；The sliding arc plate lateral wall correspond at the sliding groove at Type has slider bar；The outlet hole for being passed through for the charging wire is formed on the smooth plate；
The lower frame body is corresponded to form along its length at the outlet hole and be passed through for the charging wire being pierced by from the outlet hole Strip-shaped hole；Bar shaped hole width is more than or equal to outlet hole aperture；
Described charging wire one end is electrically connected with the slot electrode of the wire-winding unit, the charging wire other end through the outlet hole and Strip-shaped hole is pierced by；
Agv controller for controlling the first motor and second motor rotation is installed in the upper frame body；It is described First motor, the second motor, the first limit switch, the second limit switch are electrically connected with agv controller；
Electric current is exported from transmission guide rail, by contacting sliding plate, is transferred to after electrode slice and is transferred to charging wire by slot electrode, finally Reach terminal pad；
The electric vehicle upper end is equipped with charging board；The charging board upper end is equipped with the first receiving electrode；The charging board Upper end be located at be fixedly connected on the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnet；
The insulation tank parked disk upper end and form annular；It is described park disk upper end and be located on the outside of the insulation tank be fixedly connected There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through-hole；The terminal pad lower end corresponds to and is equipped with the first confession at first receiving electrode Electrode；The take-up reel lower end is equipped with iron block corresponding with each second electromagnet position；In the terminal pad End periphery is fixedly connected with the annular iron block for being useful for being connect with terminal pad for aircraft；It is described annular iron block on be equipped with it is described Corresponding second current electrode of second receiving electrode；
The aircraft, trolley component, electric vehicle are connected by wireless signal and the server communication of system；
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 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 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 power supply system for electric vehicle charging as described in claim 1, it is characterised in that：Each outlet air Position of the ring inner circumferential far from connecting tube forms Holder joint of rising and falling, and respectively there are one rise and fall for connection in each Holder joint of rising and falling Frame；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, the sliding tube being slidably mounted in connection pipe body, with connection pipe body close to the branch for Holder joint one end rotation connection of rising and falling Strut is connected on supporting rod far from first electromagnet of Holder joint one end of rising and falling, and respectively in the middle part of sliding tube, supporting rod The connecting rod of middle part rotation connection；The second receiving electrode for charging to aircraft is installed below first electromagnet；
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.
3. a kind of power supply system for electric vehicle charging as described in claim 1, it is characterised in that：It is described go out vane It is axial perpendicular with the radial direction of fan mounting portion, and go out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and The horizontal wind-force for going out the wind generation of the outlet air gap blowout of vane is opposite with the rotation direction of the fan blade of upper driving fan.
CN201810112319.1A 2017-06-23 2017-06-23 A kind of power supply system for electric vehicle charging Withdrawn CN108556649A (en)

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CN112350263A (en) * 2019-08-07 2021-02-09 阿里巴巴集团控股有限公司 Power transmission cable storage structure, power supply system, data processing system and power supply method

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CN110316009B (en) * 2019-07-17 2020-09-01 湖北文理学院 Electric automobile roadside charging system
CN114572024B (en) * 2022-03-01 2024-06-04 中国商用飞机有限责任公司北京民用飞机技术研究中心 Energy transmission system of aircraft

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CN203787229U (en) * 2014-03-11 2014-08-20 重庆市南方阻燃电线电缆厂 Cable wrapping guider
CN103935266B (en) * 2014-04-08 2016-08-17 福州开发区和世林实业发展有限公司 Driving electric supply installation
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CN205944904U (en) * 2016-08-18 2017-02-08 国网湖南省电力公司带电作业中心 Cloth cable pulls component

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CN112350263A (en) * 2019-08-07 2021-02-09 阿里巴巴集团控股有限公司 Power transmission cable storage structure, power supply system, data processing system and power supply method
CN112350263B (en) * 2019-08-07 2022-08-19 阿里巴巴集团控股有限公司 Power transmission cable storage structure, power supply system, data processing system and power supply method

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