CN107264317A - A kind of electric power system for being available for charging electric vehicle - Google Patents

A kind of electric power system for being available for charging electric vehicle Download PDF

Info

Publication number
CN107264317A
CN107264317A CN201710489015.2A CN201710489015A CN107264317A CN 107264317 A CN107264317 A CN 107264317A CN 201710489015 A CN201710489015 A CN 201710489015A CN 107264317 A CN107264317 A CN 107264317A
Authority
CN
China
Prior art keywords
plate
charging
fan
vane
frame body
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.)
Granted
Application number
CN201710489015.2A
Other languages
Chinese (zh)
Other versions
CN107264317B (en
Inventor
虞丽丽
江佳辉
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.)
Yu Qing
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 CN201710489015.2A priority Critical patent/CN107264317B/en
Priority to CN201810112318.7A priority patent/CN108263236A/en
Priority to CN201810112319.1A priority patent/CN108556649A/en
Publication of CN107264317A publication Critical patent/CN107264317A/en
Application granted granted Critical
Publication of CN107264317B publication Critical patent/CN107264317B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 charging electric vehicle field, specifically related to a kind of electric power system for being available for charging electric vehicle, 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 connected with each trolley component, is movably connected in the aircraft above terminal pad, and electric automobile of the traveling on road.The present invention is arranged on by road, can be on road to the timely charging of electric automobile, not by time restriction, and driver can save the time of driver's charging waiting while driving to charging electric vehicle；It is connected by trolley component with power transmission line and electric automobile is powered, flexibility is had more compared to charging pile, the place of charging is unfettered.

Description

A kind of electric power system for being available for charging electric vehicle
Technical field
The invention belongs to charging electric vehicle field, and in particular to a kind of electric power system for being available for charging electric vehicle.
Background technology
Electric automobile has the advantages that prominent while the problem of there is charging aspect as energy-saving and environment-friendly automobile.It is existing Charging modes are mainly charging pile, but charging pile is fixed due to installation site, and charging can only be rested in during charging electric vehicle Stake is nearby charged；And the time that charging pile needs when charging is long, can not be moved during charging electric vehicle.
The content of the invention
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, providing one kind is available for electronic vapour The electric power system of car charging.
To realize the purpose of the present invention, it is achieved using following technical scheme：A kind of confession for being available for charging electric vehicle 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 Guide rail and multiple trolley components being slidably connected on guide rail above road；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, and the wire-winding unit in upper frame body is sliding The dynamic sliding arc plate being connected in lower frame body, be fixedly connected on upper frame body upper end and with connecing that the transmission guide rail is slidably connected Touch sliding plate and the charging wire being wrapped on the wire-winding unit；
The charging wire end is fixedly connected with for the terminal pad to charging electric vehicle；Also include multiple for carrying connection The aircraft of disk movement.
Preferably：Each electric pole includes the vertical rod that vertical direction is set；The upper part of telegraph pole is fixed It is connected with and parks disk towards what road direction was set；The vertical rod upper end is fixedly connected with towards the horizontally disposed horizontal stroke of road direction Bar；The crossbar end is fixedly connected with the guide rail；
The guide rail includes the upper connection rail for being fixedly connected on each cross bar lower end；The upper connection rail two ends form perpendicular Straight downward two sides connection rail；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail, the traveling Rail is connected rail with the side in T fonts；The transmission guide rail is fixedly connected on the traveling connected positioned at the side on the inside of rail Rail upper end；
Upper frame body both sides symmetrical molding has two side plates；Two side plate inside middle portions are integrally formed with connecting plate；Two Multiple feeder wheels being equally spaced are rotatably connected on the inside of the individual side plate upper end；Each described advance of correspondence on the outside of the side plate Multiple the first motors for being used to drive the feeder wheel to rotate are fixedly connected with wheel；The trolley component passes through the feeder wheel 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 is located at forms upper frame body end plate between the connecting plate and two side plates；It is molded on the upper frame body end plate There is the first mounting hole for installing the wire-winding unit；The upper frame body forms installing plate close to the other end；The peace Second mounting hole coaxial with first mounting hole is formed on dress plate；Two side plate interior sides bottoms are close to middle part and position Two electrode slices are fixedly connected near the installing plate；
The installing plate is fixedly connected with the second motor away from the upper frame body end plate side；On the output shaft of second motor Installation axle is fixedly connected with, the installation axle is rotatably connected in first mounting hole and second mounting hole；Institute State to be fixedly connected with the middle part of installation axle and form externally threaded screw thread disk；The screw thread disk is close away from the 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 described install Plate side is fixedly connected with incoming panel；The incoming panel outer circumferential is provided with two annular slot electrodes being parallel to each other；Two The individual electrode slice is plugged in two slot electrodes respectively；The screw thread disk diameter is more than the incoming panel；The charging Line winding is located in the installation axle between the screw thread disk and the incoming panel；
The lower frame body and the upper frame body are isometric and are arc；Lower frame body one end corresponding with the upper frame body end plate into 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 Symmetrical molding has the sliding groove that two confessions sliding arc plate is slidably connected along its length；
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inwall form with it is described The internal thread of screw thread disk threaded connection；The sliding arc plate forms pressing end plate close to described lower frame body end plate one end；It is described Sliding arc plate forms smooth plate away from described pressing end plate one end；At the sliding arc plate lateral wall correspondence sliding groove into Type has slider bar；The wire hole for being passed through for the charging wire is formed on the smooth plate；
Form and passed through for the charging wire passed from the wire hole along its length at the lower frame body correspondence wire hole Bar hole；Bar shaped hole width is more than or equal to wire 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 wire hole and Bar hole is passed；
Agv controller for controlling first motor and second motor to rotate 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 automobile upper end is provided with charging board；The charging board upper end is provided with the first receiving electrode；The charging board Upper end be located at first receiving electrode on the outside of be fixedly connected with circumferentially be equally spaced have multiple second electromagnet；
It is described to park the insulation tank that disk upper end forms annular；The disk upper end of parking is fixedly connected on the outside of the insulation tank There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through hole；The first confession is installed at the terminal pad lower end correspondence first receiving electrode Electrode；The take-up reel lower end is provided with the iron block corresponding with the second electromagnet position each described；In the terminal pad End periphery is fixedly connected with the annular iron block for being connected for aircraft with terminal pad；Be provided with the annular iron block with it is described Corresponding second current electrode of second receiving electrode；
The aircraft, trolley component, electric automobile are connected by wireless signal and the server communication of system.
Preferably：The aircraft includes main part, and the fan that the main part includes tubular is installed Portion, is connected to the connecting tube of fan installation portion periphery and four equidistant arrangements being connected with fan installation portion, and is connected to Each connecting tube outer end and with correspondence position connecting tube is connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed； It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior Footpath is more than the internal diameter that lower driving fan section is installed in fan installation portion, and the fan blade diameter of upper driving fan is more than lower driving wind Blast superatmospheric in the fan blade diameter of fan, the fan installation portion between upper driving fan and lower driving fan, Blast is formed in vane so that going out；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out 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 installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction formed The angle of 5-20 degree, and go out the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced In the opposite direction；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube Part includes motor, the coaxially connected screw rod with motor output shaft, and the valve plate being connected with screw flight；The valve plate top Periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube internal upper part into Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane The valve plate guide rod that plate is slidably connected；Bottom is connected with upper end towards going out the inclined baffle plate in vane direction in the connecting tube, The conducting adjustable airway of area is formed between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected with control board respectively；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip Air port；
The main part is that upper shell and lower house are tightly connected composition；
The lower, outer perimeter of the fan installation portion is to be connected with to electrically connect with control board in battery installation section, battery installation section Battery；It is a circuit board installation cavity, the control circuit to be located at the top of battery installation section on the fan installation portion Plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular cover plate；The circuit board peace The upper surface behaveing affectedly uniformly forms the fresh air inlet connected with fan installation portion, and the lateral wall of the circuit board installation cavity is uniform Form vent；The lower driving fan lower end is provided with the camera electrically connected with control board；
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, it is each in Holder joint of rising and falling described in each It is connected with a undercarriage；The undercarriage includes the support bar being fixedly connected with the Holder joint of rising and falling and is connected to support The first electromagnet away from Holder joint one end of rising and falling on bar, the support bar is downwards；Installed below first electromagnet There is the second receiving electrode for being charged to aircraft.
Preferably：Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, each A undercarriage is respectively connected with the Holder joint of rising and falling；The undercarriage, which includes, to be fixedly connected and passes through with Holder joint of rising and falling The connection pipe body that Holder joint of rising and falling is connected with going out inside vane, is slidably mounted on the sliding tube in connection pipe body, with connecting tube Body rotates the support bar of connection close to Holder joint one end of rising and falling, and is connected to the first electricity away from Holder joint one end of rising and falling on support bar Magnet, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar；Use is installed below first electromagnet In the second receiving electrode charged to aircraft；
The connection pipe body forms hinged seat close to Holder joint one end side wall that rises and falls, and described support bar one end is rotated with hinged seat Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position, which is connected with, to be hinged Head, described connecting rod one end rotates with articulated joint and is connected, and side wall of the connection pipe body away from Holder joint one end of rising and falling forms confession The strip shape gob that articulated joint is passed through；The one end of the connection pipe body away from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap The inner is connected with spring locating rod, the spring locating rod and is arranged with spring, and the both ends of the spring is against piston respectively And between sealing cap is inner；The connecting rod tank that the connecting rod is accommodated in support bar collapsed state is formed on the support bar.
Preferably：The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out the axial direction of vane with The angle of 5-20 degree is formed between horizontal direction, and goes out horizontal wind-force and upper driving that the wind of the air-out gap blowout of vane is produced The rotation direction of the fan blade of fan is opposite.
Preferably：Diameter of a circle where the annular iron block center line is corresponding with after aircraft support bar expansion 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 Respectively include two annular electro polar rings being arranged concentrically.Two are provided with the brush on the position of correspondence brush to set with one heart The annular electro polar ring put.
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 during the charging electric vehicle.
Preferably：The through-hole diameter is more than the battery external diameter.
Preferably：The 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 is installed along by road, is carried by aircraft Terminal pad is moved, so that connection is set up between power transmission line and electric automobile, and then to charging electric vehicle.Filled when no During electric task, terminal pad, which is parked in, parks on disk, terminal pad is connected with parking disk 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 offseted with the second limit switch Place, the charging wire is 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 connected with terminal pad, and the second current electrode is connected to carry out aircraft with the second receiving electrode Charging.When electric automobile not enough power supply, below electric automobile during traveling to guide rail, and the letter of charge request is sent to server Number, server is received after charge request signal, according to the location of electric automobile, and is fed back electric automobile and opened to driving side Below to the trolley component that remains static foremost, while being adjusted the distance the nearest aircraft of the trolley component by server Instruction is sent, aircraft installed in the camera manual control of lower section by flying in the terminal pad that the trolley component connected End, the second electromagnet power-off during the aircraft declines on the electric automobile, 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 Two motor reversals, the extension elongation increase of charging wire is moved to above electric automobile while controlling aircraft to carry terminal pad, this When electric automobile on the second electromagnet be powered, control aircraft decline the first current electrode is connected with the first receiving electrode, So that charging electric vehicle, then control aircraft, which drives, connects on disc spins, the iron block and charging board for making terminal pad lower end The second electromagnet it is attracting so that terminal pad is 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 is then controlled to power off, aircraft disengages with terminal pad and carries out other tasks.When electronic Control aircraft is connected after being moved to above electric automobile with terminal pad after automobile charging is finished, the second electricity on electric automobile Magnet is powered off, and terminal pad and charging board disconnect, subsequent aircraft carry terminal pad be connected on follow-up electric automobile charging or Person parks terminal pad to parking on disk；Charging electric vehicle is finished and during 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 dolly control Device processed controls the first motor to be moved near the nearest electric pole parked where disk, and the second motor is rotated forward, and charging wire is twined Around on reel, stopping finally being touched to the second limit switch.When aircraft charges, pass through the shooting below aircraft Head judges to be parked in the terminal pad parked on disk, and control aircraft is moved to above the terminal pad, then drop to the terminal pad On make the first electromagnet attracting so as to be attached to aircraft with annular iron block, while the second current electrode receives electric with second Pole is electrically connected, so as to be charged to aircraft.
The present invention is arranged on by road, not by time restriction, and can be driven on road to the timely charging of electric automobile The time of driver's charging waiting can be saved while driving to charging electric vehicle by sailing people；By trolley component with it is defeated Conductance rail is connected powers to electric automobile, 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, so as to reduce the friction of charging wire outer layer；Aircraft carries terminal pad to charging electric vehicle, energy Potential safety hazard when enough avoiding manual powered；When Rechargeable vehicle is started to charge up, aircraft is disconnected with terminal pad, compared to Aircraft can be more rationally utilized in the case of aircraft and terminal pad one and cost-effective；The disk of parking is fixedly connected On utility poles, make that storage need not be fixed to the terminal pad of charging electric vehicle, cause generation hidden in the air without being suspended from Suffer from；Terminal pad, which is fixed, to be stored in when parking on disk, and the aircraft under off working state can be charged simultaneously, and to aircraft Offer storage place.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of electric pole and guide rail.
Fig. 3 is the structural representation of electric automobile.
Fig. 4 is the structural representation of trolley component.
Fig. 5 is the decomposition texture schematic diagram of trolley component.
Fig. 6 is the cross section structure diagram of upper frame body.
Fig. 7 is the structural representation of sliding arc plate.
Fig. 8 is the structural representation of lower frame body.
Fig. 9, Figure 10 are the structural representations of terminal pad.
Structural representation when Figure 11 is aircraft grounding state or carries terminal pad.
Figure 12 is the structural representation under aircraft free flight state.
Figure 13 is the cross section structure diagram of aircraft.
Figure 14 is Figure 13 A portions schematic enlarged-scale view.
Figure 15 is Figure 13 B portions schematic enlarged-scale view.
The structural representation of each part that Figure 16 is upper shell and is connected with upper shell.
Figure 17 is the structural representation of lower housing section.
Figure 18 is the cross section structure diagram of lower housing section.
Figure 19 is the cross section structure diagram of undercarriage part.
Figure 20 is the decomposition texture schematic diagram of undercarriage part.
1st, electric pole；11st, mobile jib；12nd, disk is parked；121st, permanent magnet；122nd, insulation tank；13rd, cross bar；2nd, trolley component； 21st, upper frame body；211st, side plate；2111st, electrode slice；212nd, connecting plate；213rd, feeder wheel；2131st, the first motor；214th, upper frame body End plate；2141st, the first mounting hole；215th, installing plate；2151st, the second mounting hole；22nd, wire-winding unit；221st, screw thread disk；2211、 First limit switch；222nd, the second motor；223rd, installation axle；224th, incoming panel；2241st, slot electrode；23rd, lower frame body；231st, under Framework end plate；2311st, the second limit switch；2312nd, sliding groove；2313rd, bar hole；24th, sliding plate is contacted；25th, sliding arc plate； 251st, internal thread；252nd, slider bar；253rd, smooth plate；2531st, wire hole；254th, end plate is pressed；26th, charging wire；31st, charge Disk；32nd, the first receiving electrode；33rd, the second electromagnet；4th, terminal pad；41st, annular iron block；42nd, the first current electrode；43rd, iron Block；44th, the second current electrode；45th, through hole；5th, aircraft；51st, main part；51a, upper shell；51b, lower house；510th, fan Installation portion；5101st, upper bracket；5102nd, lower carriage；5103rd, battery installation section；5104th, circuit board installation cavity；5105th, fresh air inlet； 5106th, vent；5107th, camera；511st, vane is gone out；5110th, rise and fall Holder joint；5111st, vane upper shell；5112nd, vane Lower house；51121st, interior curved wall；51122nd, dowel；51123rd, air outlet guard board；51124th, training wall；512nd, connecting tube；5121、 Motor mounting plate；5122nd, valve plate guide rod；5123rd, baffle plate；513rd, cover plate；52nd, battery；53rd, undercarriage；531st, connection pipe body； 5311st, hinged seat；5312nd, strip shape gob；532nd, sliding tube；5321st, piston；5322nd, articulated joint；533rd, sealing cap；5331st, spring Locating rod；534th, connecting rod；535th, support bar；5351st, connecting rod tank；536th, the first electromagnet；5361st, the second receiving electrode； 537th, spring；54th, air intake cover；551st, upper driving fan；552nd, lower driving fan；56th, adjusting part；561st, motor；562nd, spiral shell Bar；563rd, valve plate；57th, control board；6th, guide rail；61st, upper connection rail；62nd, side connection rail；63rd, traveling rail；64th, transmission of electricity is led Rail.
Embodiment
Embodiment 1
According to Fig. 1 to Figure 20, the present embodiment is a kind of electric power system for being available for charging electric vehicle, is included 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 It is slidably connected at the trolley component 2 on guide rail；Transmission guide rail 64 is installed in the guide rail.
The trolley component includes the upper frame body 21 and lower frame body 23 being fixedly connected up and down, the coiling in upper frame body Component 22, is slidably connected at the sliding arc plate 25 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 for the terminal pad 4 to charging electric vehicle；Present invention additionally comprises multiple Aircraft 5 for carrying terminal pad movement.
Each electric pole includes the vertical rod 11 that vertical direction is set；The upper part of telegraph pole is fixedly connected with towards road What direction was set parks disk 12；The vertical rod upper end is fixedly connected with towards the horizontally disposed cross bar 13 of road direction；The horizontal stroke 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；It is described it is upper connection rail two ends into Type has two sides connection rail 62 straight down；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail 63, the traveling rail is connected rail with the side in T fonts；The transmission guide rail is fixedly connected on the inside of side connection rail The traveling rail upper end.The transmission guide rail is arranged on the guide rail interior, prevents human or animal from directly being connect with transmission guide rail Touch and occur electric shock accidents.
Upper frame body both sides symmetrical molding has two side plates 21；Two side plate inside middle portions are integrally formed with connection Plate 212, the connecting plate is the circular arc arched 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 with the outside of the side plate at each described feeder wheel of correspondence multiple for driving the rotation of advancing The first dynamic 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 installing plate 215 close to the other end；Formed on the installing plate and the described first peace Fill the second coaxial mounting hole 2151 of hole；Two side plate interior sides bottoms are close to middle part and fixed near the installing plate It is connected with two electrode slices 2111.
The installing plate is fixedly connected with the second motor 222 away from the upper frame body end plate side；Second motor Installation axle 223 is fixedly connected with output shaft, the installation axle is rotatably connected on first mounting hole and described second In mounting hole；It is fixedly connected with the middle part of the installation axle and forms externally threaded screw thread disk 221；The screw thread disk is away from described Two motor sides are provided with multiple first limit switches 2211 at screw thread plate edge along the installation axle is circumferentially equidistant；It is described Installation axle is fixedly connected with incoming panel 224 positioned at the installing plate side；The incoming panel outer circumferential is provided with two mutually Parallel annular slot electrode 2241；Two electrode slices are plugged in two slot electrodes respectively；The screw thread disk is straight Footpath is more than the incoming panel；The pitch of the screw thread disk is equal with the line footpath of the charging wire；The charging wire winding is located at institute State in the installation axle between screw thread disk and the incoming panel.
The lower frame body and the upper frame body are isometric and are 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 Symmetrical molding has the sliding groove 2312 that two confessions sliding arc plate is slidably connected to framework madial wall along its length.
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inwall form with The internal thread 251 of the screw thread disk threaded connection；The sliding arc plate forms press-side close to described lower frame body end plate one end Plate 254；The sliding arc plate forms smooth plate 253 away from described pressing end plate one end；The sliding arc plate lateral wall correspondence Slider bar 252 is formed at the sliding groove；The wire hole for being passed through for the charging wire is formed on the smooth plate 2531。
The charging wire for being passed from the wire hole is formed at the lower frame body correspondence wire hole along its length The bar hole 2313 passed through；Bar shaped hole width is more than or equal to wire 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 bar hole are passed.
Agv controller for controlling first motor and second motor to rotate is installed in the upper frame body； First motor, the second motor, the first limit switch, the second limit switch are electrically connected with agv controller.
The pitch of the screw thread disk is equal with the line footpath of the charging wire.When second motor is rotated forward, the charging Line is wrapped between the screw thread disk and the incoming panel, because the threaded connection between the screw thread disk and the internal thread makes The sliding arc plate is slided along the sliding groove, the direction of rotation of the charging wire winding and the thread rotary orientation phase of the screw thread disk Together, and the pitch due to screw thread disk is equal with the diameter in the section of charging wire, the charging wire winds around the coiling On cylinder, pressing end plate lateral surface is touched and presses the second limit switch, agv controller described in the sliding arc plate sliding process Second motor is controlled to be stopped；When second motor reversal, charging wire rotation unwrapping wire and from the outlet Passed in hole and the bar hole, it is described to fill because the pitch of the screw thread disk is equal with the diameter in the section of the charging wire The point departed from during wire releasing at winding synchronizing moving with the slip of sliding arc plate, all the time above the wire hole, Press end plate medial surface in sliding arc plate slipping to touch and press first limit switch, agv controller control is described Second motor is stopped.Sliding arc plate is set to be slided while wire-winding unit is rotated by the threaded connection of screw thread disk and internal thread It is dynamic, and due to the setting of pitch makes to be closely wound in charging wire winding process and prevent mixed and disorderly, and charging wire depart from around Passed during the defence line of spool from wire hole, and bar shaped hole width is more than wire hole aperture, therefore, it is possible to reduce even The friction between charging wire and wire hole is avoided to protect charging wire.
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 aircraft includes main part 51, and the main part includes the fan installation portion 510 of tubular, is connected to Fan installation portion periphery and the connecting tube 512 for four equidistant arrangements being connected with fan installation portion, and it is connected to each company That takes over outer end and be connected with correspondence position connecting tube goes out vane 511.
It is located to be connected with upper bracket 5101, the upper bracket above connecting tube in the fan installation portion and is provided with Drive fan 551；It is located to be connected with lower carriage 5102, the lower carriage below connecting tube in the fan installation portion and installs There is lower driving fan 552；The upper driving fan is with the lower steering for driving fan on the contrary, and being installed in the fan installation portion The internal diameter of fan section is driven to be more than the internal diameter for installing lower driving fan section in fan installation portion, and the fan blade of upper driving fan Diameter is more than in the fan blade diameter of lower driving fan, the fan installation portion and is located between upper driving fan and lower driving fan Blast superatmospheric so that go out and blast is formed in vane.
It is described go out vane include the vane upper shell 5111 and vane lower house 5112 being tightly connected, the vane lower casing Internal Zhou Shangduan forms interior curved wall 51121, and the inner circumferential of the interior curved wall is connected with an air outlet guard board by multiple dowels 51123, air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；On being formed between the interior curved wall and air outlet guard board Narrow air-out gap under width, the bottom width in air-out gap is 0.8-1.5mm；The inner circumferential of the vane lower house is located at air-out 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 installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction The angle of 5-20 degree is formed, and goes out horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced Rotation direction is opposite.
It is provided with to adjust the adjusting part 56 that correspondence position goes out vane air-out speed in each described 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 connected with screw flight 563；The valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；Institute State 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；Bottom is connected with a upper end court in the connecting tube To the inclined baffle plate 5123 in vane direction is gone out, the conducting adjustable airway of area is formed between the baffle plate and valve plate.
The upper driving fan, lower driving fan and each motor are electrically connected with control board 57 respectively.
The main part upper end is connected with the air intake cover 54 of a semiellipse spherical shape, air intake cover and uniformly forms bar The air inlet of shape.
The main part is that upper shell 51a and lower house 51b is tightly connected composition.
Aircraft provides driving force, upper driving fan production by the upper driving fan in fan installation portion, lower driving fan Raw fraction is blown out downwards from each air-out gap for going out vane, and combines the air-out that adjusting part adjustment each goes out vane Speed, so as to realize the horizontal flight or steering of aircraft, due to going out vane positioned at each of aircraft periphery and only play tune The effect of whole attitude of flight vehicle, without the fan for being provided with power, goes out when vane produces touching with foreign object and is not easily caused aircraft Out of control or produce injury to human or animal, security is good.
Further, it is described go out vane air-out 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 in the lump, so fly When the part in air-out gap is stopped in row device flight course, the overall airflow influence that air-out gap is formed is small, is conducive to flying The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out axial direction and the level of vane The angle of 5-20 degree is formed between direction, and goes out horizontal wind-force and upper driving fan that the wind of the air-out gap blowout of vane is produced Fan blade rotation direction it is opposite.Pass through such design so that the wind energy for going out the air-out gap blowout of vane enough offsets drive The reaction force produced when dynamic fan and the rotation of lower driving fan；Also, change air-out by adjusting each adjusting part simultaneously Ring goes out wind velocity, and the overall forward or reverse of aircraft can be achieved.Make one by adjusting one or two adjusting part Or two go out vane go out wind velocity, aircraft can be achieved generally in heeling condition, aircraft can be so driven in level Fly in direction.
The lower, outer perimeter of the fan installation portion is to be connected with battery installation section 5103, battery installation section and control circuit The battery 52 of plate electrical connection；It is a circuit board installation cavity to be located at the top of battery installation section on the fan installation portion 5104, the control board 57 is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular Cover plate 513；The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet 5105 connected with fan installation portion, institute The lateral wall for stating circuit board installation cavity uniformly forms vent 5106；The lower driving fan lower end is provided with and control circuit The camera 5107 of plate electrical connection.
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint 5110 of rising and falling, each described undercarriage A undercarriage 53 is respectively connected with joint；The undercarriage includes the support bar 535 being fixedly connected with the Holder joint of rising and falling And the first electromagnet 536 away from Holder joint one end of rising and falling on support bar is connected to, the support bar is downwards；Described The second receiving electrode 5361 for being charged to aircraft is installed below one electromagnet.
A small amount of air-flow of the fan installation portion enters from fresh air inlet and from vent discharge, the control board is risen To thermolysis.
The electric automobile upper end is provided with charging board 31；The charging board upper end is provided with the first receiving electrode 32；Institute State charging board upper end be fixedly connected with the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnetism Iron 33.
It is described to park the insulation tank 122 that disk upper end forms annular；The disk upper end of parking is 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 by the aircraft and moved to the charging electric vehicle.When the aircraft is carried During the terminal pad movement, the aircraft is connected with the terminal pad upper end；During the charging electric vehicle, the charging board It is connected with the terminal pad lower end.
The terminal pad intermediary form has through hole 45, and the through-hole diameter is more than the battery external diameter；The terminal pad The first current electrode 42 is installed at lower end correspondence first receiving electrode；The take-up reel lower end is provided with each institute of correspondence State the iron block 43 of the second electromagnet；Terminal pad upper end periphery is fixedly connected with the ring for being connected for aircraft with terminal pad Shape iron block 41, diameter of a circle where the annular iron block center line and corresponding first electromagnetism iron phase after aircraft support bar expansion Circumscribed circle diameter where the rectangle being linked to be is equal；The second confession is installed at the annular iron block correspondence second receiving electrode Electrode 44.
The aircraft, trolley component, electric automobile 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 respectively include two The annular electro polar ring being arranged concentrically.Two annular electrodes being arranged concentrically are installed on the position of correspondence brush in the brush Ring.
Speed limit 40km/h during the charging electric vehicle.
The present invention is installed along by road, and carrying terminal pad by aircraft moves so that power transmission line and electric automobile it Between set up connection, and then to charging electric vehicle.When no progress charging tasks, terminal pad, which is parked in, parks on disk, passes through Iron block and permanent magnet is attracting makes terminal pad be connected with parking disk, first current electrode is plugged in the insulation tank, is slided Arc plate is located at lower frame body end plate one end and offseted place with the second limit switch, and the charging wire is wound to most short extension elongation shape State, while the first electromagnet without the aircraft under aerial mission is with annular, iron block is attracting aircraft is connected with terminal pad, the Two current electrodes are connected to charge to aircraft with the second receiving electrode.When electric automobile not enough power supply, electronic vapour Car is travelled to guide rail, and the signal of charge request is sent to server, and server is received after charge request signal, root According to the location of electric automobile, and feed back electric automobile and open under the trolley component remained static foremost to direction of traffic Side, while sending and instructing by the server nearest aircraft of the trolley component of adjusting the distance, aircraft passes through installed in lower section Camera manual control flies to the terminal pad upper end that the trolley component is connected, the electronic vapour during the aircraft declines The second electromagnet power-off on car, each first electromagnet with annular iron block is attracting aircraft is connected with terminal pad；Simultaneously Server sends to agv controller and instructed, 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 automobile, now the second electromagnet on electric automobile is powered, control Aircraft, which declines, makes the first current electrode be connected with the first receiving electrode, so that charging electric vehicle, then controls aircraft Connection disc spins are driven, make the second electromagnet on the iron block and charging board of terminal pad lower end attracting, so that terminal pad is fixed On charging board；The first motor work of trolley component is controlled in charging process, trolley component is 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 is powered off, and aircraft disengages with terminal pad and carries out other tasks.Aircraft is controlled to be moved to electricity after charging electric vehicle is finished It is connected after above electrical automobile with terminal pad, the second electromagnet power-off on electric automobile, terminal pad disconnects with charging board, then Aircraft carries terminal pad and is connected on follow-up electric automobile charging or parks terminal pad to parking on disk；Electric automobile Charging is finished and during without charging tasks, and server is sent to trolley component and aircraft and instructed, and aircraft is judged by camera And carry terminal pad and park to nearest and park on disk, while agv controller, which controls the first motor to be moved to, nearest parks disk Near the electric pole at place, and the second motor is rotated forward, and charging wire is wound on reel, finally touched to the second limit switch After stop.When aircraft charges, judge to be parked in the terminal pad parked on disk by the camera below aircraft, control flies Row device is moved to above the terminal pad, and then droping in the terminal pad makes the first electromagnet attracting so as to flying with annular iron block Row device is attached, while the second current electrode is electrically connected with the second receiving electrode, so as to be charged to aircraft.
The present invention is arranged on by road, not by time restriction, and can be driven on road to the timely charging of electric automobile The time of driver's charging waiting can be saved while driving to charging electric vehicle by sailing people；By trolley component with it is defeated Conductance rail is connected powers to electric automobile, 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, so as to reduce the friction of charging wire outer layer；Aircraft carries terminal pad to charging electric vehicle, energy Potential safety hazard when enough avoiding manual powered；When Rechargeable vehicle is started to charge up, aircraft is disconnected with terminal pad, compared to Aircraft can be more rationally utilized in the case of aircraft and terminal pad one and cost-effective；The disk of parking is fixedly connected On utility poles, make that storage need not be fixed to the terminal pad of charging electric vehicle, cause generation hidden in the air without being suspended from Suffer from；Terminal pad, which is fixed, to be stored in when parking on disk, and the aircraft under off working state can be charged simultaneously, and to aircraft Offer storage place.
Embodiment 2
The present embodiment has done following improvement on the basis of embodiment 1：Go out position of the vane inner circumferential away from connecting tube described in each Holder joint 5110 of rising and falling is formed, a undercarriage 53 is respectively connected with Holder joint of rising and falling described in each；The undercarriage includes There is the connection pipe body 531 for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling, slide peace Sliding tube 532 in connection pipe body, rotates the support bar 535 being connected, even with connection pipe body close to Holder joint one end of rising and falling Be connected on support bar away from first electromagnet 536 of Holder joint one end of rising and falling, and respectively with the middle part of sliding tube, in the middle part of support bar Rotate the connecting rod 534 of connection；The second receiving electrode 5361 for being charged to aircraft is installed below first electromagnet.
The connection pipe body forms hinged seat 5311, described support bar one end and hinge close to Holder joint one end side wall that rises and falls Joint chair rotates connection；The sliding tube is connected with position in the middle part of piston 5321, the slip pipe outer wall close to Holder joint one end of rising and falling Put and be connected with articulated joint 5322, described connecting rod one end rotates with articulated joint and is connected, the connection pipe body is away 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 away from Holder joint of rising and falling, which is fixed, to be connected Sealing cap 533 is connected to, the inner of sealing cap, which is connected with spring locating rod 5331, the spring locating rod, is arranged with spring 537, the both ends of the spring is against between piston and sealing cap the inner respectively；Formed on the support bar and pack up shape in support bar The connecting rod tank 5351 of the connecting rod is accommodated during state.
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in work shape After state, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
The undercarriage is packed up or deployed as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out Blast in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drivening rod one end is to sealing cap Direction is moved, so that support bar lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft During landing, the blast gone out in vane reduces, and Spring driving sliding tube is moved together with piston toward hinged seat direction, so that sliding tube Drivening rod one end is moved to hinged seat direction, so that support bar lower end turns to extreme position to hinged seat one end, so that Undercarriage is set to be in deployed condition.
The strip shape gob plays a part of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch After length, support bar turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each support bar is equal In stable state.Aircraft is carried in the moving process of terminal pad, because the first electromagnet and annular iron block are attracting, but air-out The power that blast in ring is produced is insufficient to allow support bar to pack up.

Claims (10)

1. a kind of electric power system for being available for charging electric vehicle, 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, and the wire-winding unit in upper frame body is sliding The dynamic sliding arc plate being connected in lower frame body, be fixedly connected on upper frame body upper end and with connecing that the transmission guide rail is slidably connected Touch sliding plate and the charging wire being wrapped on the wire-winding unit；
The charging wire end is fixedly connected with for the terminal pad to charging electric vehicle；Also include multiple for carrying connection The aircraft of disk movement.
2. a kind of electric power system for being available for charging electric vehicle as claimed in claim 1, it is characterised in that：Each electric wire Bar includes the vertical rod that vertical direction is set；The upper part of telegraph pole is fixedly connected with and parks disk towards what road direction was set；It is described Vertical rod upper end is fixedly connected with towards the horizontally disposed cross bar of road direction；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 two ends form perpendicular Straight downward two sides connection rail；Two side connection rail lower ends are fixedly connected with horizontally disposed traveling rail, the traveling Rail is connected rail with the side in T fonts；The transmission guide rail is fixedly connected on the traveling connected positioned at the side on the inside of rail Rail upper end；
Upper frame body both sides symmetrical molding has two side plates；Two side plate inside middle portions are integrally formed with connecting plate；Two Multiple feeder wheels being equally spaced are rotatably connected on the inside of the individual side plate upper end；Each described advance of correspondence on the outside of the side plate Multiple the first motors for being used to drive the feeder wheel to rotate are fixedly connected with wheel；The trolley component passes through the feeder wheel 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 is located at forms upper frame body end plate between the connecting plate and two side plates；It is molded on the upper frame body end plate There is the first mounting hole for installing the wire-winding unit；The upper frame body forms installing plate close to the other end；The peace Second mounting hole coaxial with first mounting hole is formed on dress plate；Two side plate interior sides bottoms are close to middle part and position Two electrode slices are fixedly connected near the installing plate；
The installing plate is fixedly connected with the second motor away from the upper frame body end plate side；On the output shaft of second motor Installation axle is fixedly connected with, the installation axle is rotatably connected in first mounting hole and second mounting hole；Institute State to be fixedly connected with the middle part of installation axle and form externally threaded screw thread disk；The screw thread disk is close away from the 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 described install Plate side is fixedly connected with incoming panel；The incoming panel outer circumferential is provided with two annular slot electrodes being parallel to each other；Two The individual electrode slice is plugged in two slot electrodes respectively；The screw thread disk diameter is more than the incoming panel；The charging Line winding is located in the installation axle between the screw thread disk and the incoming panel；
The lower frame body and the upper frame body are isometric and are arc；Lower frame body one end corresponding with the upper frame body end plate into 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 Symmetrical molding has the sliding groove that two confessions sliding arc plate is slidably connected along its length；
The sliding arc plate is the arc that length is the upper ledge body length half；The sliding arc plate inwall form with it is described The internal thread of screw thread disk threaded connection；The sliding arc plate forms pressing end plate close to described lower frame body end plate one end；It is described Sliding arc plate forms smooth plate away from described pressing end plate one end；At the sliding arc plate lateral wall correspondence sliding groove into Type has slider bar；The wire hole for being passed through for the charging wire is formed on the smooth plate；
Form and passed through for the charging wire passed from the wire hole along its length at the lower frame body correspondence wire hole Bar hole；Bar shaped hole width is more than or equal to wire 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 wire hole and Bar hole is passed；
Agv controller for controlling first motor and second motor to rotate 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 automobile upper end is provided with charging board；The charging board upper end is provided with the first receiving electrode；The charging board Upper end be located at first receiving electrode on the outside of be fixedly connected with circumferentially be equally spaced have multiple second electromagnet；
It is described to park the insulation tank that disk upper end forms annular；The disk upper end of parking is fixedly connected on the outside of the insulation tank There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through hole；The first confession is installed at the terminal pad lower end correspondence first receiving electrode Electrode；The take-up reel lower end is provided with the iron block corresponding with the second electromagnet position each described；In the terminal pad End periphery is fixedly connected with the annular iron block for being connected for aircraft with terminal pad；Be provided with the annular iron block with it is described Corresponding second current electrode of second receiving electrode；
The aircraft, trolley component, electric automobile are connected by wireless signal and the server communication of system.
3. a kind of electric power system for being available for charging electric vehicle as claimed in claim 1, it is characterised in that：The aircraft bag Main part is included, the main part includes the fan installation portion of tubular, be connected to fan installation portion periphery and pacify with fan The connecting tube for four equidistant arrangements that dress portion is connected, and be connected to each connecting tube outer end and with correspondence position connecting tube phase What is connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed； It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior Footpath is more than the internal diameter that lower driving fan section is installed in fan installation portion, and the fan blade diameter of upper driving fan is more than lower driving wind Blast superatmospheric in the fan blade diameter of fan, the fan installation portion between upper driving fan and lower driving fan, Blast is formed in vane so that going out；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out 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 installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction formed The angle of 5-20 degree, and go out the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced In the opposite direction；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube Part includes motor, the coaxially connected screw rod with motor output shaft, and the valve plate being connected with screw flight；The valve plate top Periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube internal upper part into Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane The valve plate guide rod that plate is slidably connected；Bottom is connected with upper end towards going out the inclined baffle plate in vane direction in the connecting tube, The conducting adjustable airway of area is formed between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected with control board respectively；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip Air port；
The main part is that upper shell and lower house are tightly connected composition；
The lower, outer perimeter of the fan installation portion is to be connected with to electrically connect with control board in battery installation section, battery installation section Battery；It is a circuit board installation cavity, the control circuit to be located at the top of battery installation section on the fan installation portion Plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular cover plate；The circuit board peace The upper surface behaveing affectedly uniformly forms the fresh air inlet connected with fan installation portion, and the lateral wall of the circuit board installation cavity is uniform Form vent；The lower driving fan lower end is provided with the camera electrically connected with control board；
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, it is each in Holder joint of rising and falling described in each It is connected with a undercarriage；The undercarriage includes the support bar being fixedly connected with the Holder joint of rising and falling and is connected to support The first electromagnet away from Holder joint one end of rising and falling on bar, the support bar is downwards；Installed below first electromagnet There is the second receiving electrode for being charged to aircraft.
4. a kind of electric power system for being available for charging electric vehicle as claimed in claim 3, it is characterised in that：Each described air-out Position of the ring inner circumferential away from connecting tube forms Holder joint of rising and falling, and being respectively connected with one in Holder joint of rising and falling described in each rises and falls Frame；The undercarriage includes the company for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling Adapter body, is slidably mounted on the sliding tube in connection pipe body, and the branch being connected is rotated close to Holder joint one end of rising and falling with connection pipe body Strut, is connected on support bar away from first electromagnet of Holder joint one end of rising and falling, and respectively with the middle part of sliding tube, support bar Middle part rotates the connecting rod of connection；The second receiving electrode for being charged to aircraft is installed below first electromagnet；
The connection pipe body forms hinged seat close to Holder joint one end side wall that rises and falls, and described support bar one end is rotated with hinged seat Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position, which is connected with, to be hinged Head, described connecting rod one end rotates with articulated joint and is connected, and side wall of the connection pipe body away from Holder joint one end of rising and falling forms confession The strip shape gob that articulated joint is passed through；The one end of the connection pipe body away from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap The inner is connected with spring locating rod, the spring locating rod and is arranged with spring, and the both ends of the spring is against piston respectively And between sealing cap is inner；The connecting rod tank that the connecting rod is accommodated in support bar collapsed state is formed on the support bar.
5. a kind of electric power system for being available for charging electric vehicle as claimed in claim 3, it is characterised in that：The axle of the vane To perpendicular with the radial direction of fan installation portion, and go out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and go out The horizontal wind-force that the wind of the air-out gap blowout of vane is produced is opposite with the rotation direction of the fan blade of upper driving fan.
6. a kind of electric power system for being available for charging electric vehicle as claimed in claim 2, it is characterised in that：The annular iron block It is external where the rectangle that corresponding first electromagnet is connected to after diameter of a circle deploys with the aircraft support bar where center line Circular diameter is equal.
7. a kind of electric power system for being available for charging electric vehicle as claimed in claim 2, it is characterised in that：First power supply Electrode, the second current electrode, the first receiving electrode, the second receiving electrode respectively include two annular electrodes being arranged concentrically Ring；
Two annular electro being arranged concentrically polar rings are installed on the position of correspondence brush in the brush.
8. a kind of electric power system for being available for charging electric vehicle as claimed in claim 2, it is characterised in that：Described park is tried to get to the heart of a matter End terrain clearance is 3.5-4m.
9. a kind of electric power system for being available for charging electric vehicle as claimed in claim 2, it is characterised in that：The electric automobile Speed limit 40km/h during charging.
10. a kind of electric power system for being available for charging electric vehicle as claimed in claim 2, it is characterised in that：The through hole is straight Footpath is more than the battery external diameter.
CN201710489015.2A 2017-06-23 2017-06-23 A kind of electric power system for electric automobile charging Active CN107264317B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN201710489015.2A CN107264317B (en) 2017-06-23 2017-06-23 A kind of electric power system for electric automobile charging
CN201810112318.7A CN108263236A (en) 2017-06-23 2017-06-23 A kind of electric power system for electric vehicle charging
CN201810112319.1A CN108556649A (en) 2017-06-23 2017-06-23 A kind of power supply system for electric vehicle charging

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710489015.2A CN107264317B (en) 2017-06-23 2017-06-23 A kind of electric power system for electric automobile charging

Related Child Applications (2)

Application Number Title Priority Date Filing Date
CN201810112318.7A Division CN108263236A (en) 2017-06-23 2017-06-23 A kind of electric power system for electric vehicle charging
CN201810112319.1A Division CN108556649A (en) 2017-06-23 2017-06-23 A kind of power supply system for electric vehicle charging

Publications (2)

Publication Number Publication Date
CN107264317A true CN107264317A (en) 2017-10-20
CN107264317B CN107264317B (en) 2018-05-04

Family

ID=60069477

Family Applications (3)

Application Number Title Priority Date Filing Date
CN201810112318.7A Withdrawn CN108263236A (en) 2017-06-23 2017-06-23 A kind of electric power system for electric vehicle charging
CN201810112319.1A Withdrawn CN108556649A (en) 2017-06-23 2017-06-23 A kind of power supply system for electric vehicle charging
CN201710489015.2A Active CN107264317B (en) 2017-06-23 2017-06-23 A kind of electric power system for electric automobile charging

Family Applications Before (2)

Application Number Title Priority Date Filing Date
CN201810112318.7A Withdrawn CN108263236A (en) 2017-06-23 2017-06-23 A kind of electric power system for electric vehicle charging
CN201810112319.1A Withdrawn CN108556649A (en) 2017-06-23 2017-06-23 A kind of power supply system for electric vehicle charging

Country Status (1)

Country Link
CN (3) CN108263236A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572024A (en) * 2022-03-01 2022-06-03 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 delivery system for an aircraft

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110316009B (en) * 2019-07-17 2020-09-01 湖北文理学院 Electric automobile roadside charging system
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103935266A (en) * 2014-04-08 2014-07-23 杨有岳 Traveling vehicle power supply device
CN203787229U (en) * 2014-03-11 2014-08-20 重庆市南方阻燃电线电缆厂 Cable wrapping guider
DE102014217091A1 (en) * 2014-08-27 2016-03-03 Volkswagen Aktiengesellschaft Charging device and method for assisting a user to charge an electrically powered vehicle
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203787229U (en) * 2014-03-11 2014-08-20 重庆市南方阻燃电线电缆厂 Cable wrapping guider
CN103935266A (en) * 2014-04-08 2014-07-23 杨有岳 Traveling vehicle power supply device
DE102014217091A1 (en) * 2014-08-27 2016-03-03 Volkswagen Aktiengesellschaft Charging device and method for assisting a user to charge an electrically powered vehicle
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114572024A (en) * 2022-03-01 2022-06-03 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 delivery system for an aircraft
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

Also Published As

Publication number Publication date
CN107264317B (en) 2018-05-04
CN108263236A (en) 2018-07-10
CN108556649A (en) 2018-09-21

Similar Documents

Publication Publication Date Title
CN107244253B (en) Charging system for electric automobile
CN107264318B (en) A kind of charging system for electric automobile to be charged by transmission guide rail
CN107264317B (en) A kind of electric power system for electric automobile charging
CN107215231B (en) A kind of electric vehicle and charging system
CN107176052A (en) Electric car electric energy shared system and sharing method
CN107264316A (en) A kind of charging system for electric automobile of use guide rail transmission of electricity
CN107215232B (en) A kind of New-energy electric vehicle charging system
CN107215233B (en) A kind of pure electric automobile charging system
CN107472062B (en) A kind of charging pile system
CN107139767A (en) A kind of electric car electric energy shared system and sharing method
CN107310413B (en) A kind of pure electric automobile electric power system
CN107117301B (en) Charging system for electric automobile
CN206841203U (en) Electric car electric energy shared system
CN206812832U (en) A kind of electric car electric energy shared system

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20211118

Address after: No.3 Heze Road, Shinan District, Qingdao, Shandong 266071

Patentee after: Yu Qing

Address before: 325000 building 3, area a, 329 Jinhai Third Road, Wenzhou Economic and Technological Development Zone, Zhejiang Province

Patentee before: WENZHOU RUICHU TECHNOLOGY Co.,Ltd.