CN107310413A - A kind of pure electric automobile electric power system - Google Patents
A kind of pure electric automobile electric power system Download PDFInfo
- Publication number
- CN107310413A CN107310413A CN201710488025.4A CN201710488025A CN107310413A CN 107310413 A CN107310413 A CN 107310413A CN 201710488025 A CN201710488025 A CN 201710488025A CN 107310413 A CN107310413 A CN 107310413A
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- Prior art keywords
- fan
- vane
- connection
- rising
- electromagnet
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- 230000000630 rising effect Effects 0.000 claims description 39
- 229910052742 iron Inorganic materials 0.000 claims description 26
- 238000007789 sealing Methods 0.000 claims description 12
- 230000000712 assembly Effects 0.000 claims description 10
- 238000000429 assembly Methods 0.000 claims description 10
- 238000009413 insulation Methods 0.000 claims description 6
- 238000005096 rolling process Methods 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 230000005611 electricity Effects 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000003860 storage Methods 0.000 description 2
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- 238000000354 decomposition reaction Methods 0.000 description 1
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- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- 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
- B60L53/60—Monitoring or controlling charging stations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/32—Constructional details of charging stations by charging in short intervals along the itinerary, e.g. during short stops
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60M—POWER SUPPLY LINES, AND DEVICES ALONG RAILS, FOR ELECTRICALLY- PROPELLED VEHICLES
- B60M7/00—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway
- B60M7/003—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway for vehicles using stored power (e.g. charging stations)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H12/00—Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The invention belongs to charging electric vehicle field, specifically related to a kind of pure electric automobile electric power system, include multiple along the equidistant electric pole being vertically installed in the middle of two-way lane in the middle of road, it is fixedly mounted on the guide rail and multiple trolley components being slidably connected on guide rail being located on electric pole above road, the terminal pad being connected with electric automobile, and multiple aircraft for being used to carry terminal pad movement.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
Technical field
The invention belongs to charging electric vehicle field, and in particular to a kind of pure electric automobile electric power system.
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 a kind of pure electric automobile
Electric power system.
To realize the purpose of the present invention, it is achieved using following technical scheme：A kind of pure electric automobile electric power system, bag
Include multiple along the equidistant electric pole being vertically installed in the middle of two-way lane in the middle of road, be fixedly mounted on electric pole and be located at road
Guide rail and multiple trolley components being slidably connected on guide rail above road；Each electric pole is set including vertical direction
Vertical rod；The vertical rod upper end is fixedly connected with two towards the horizontally disposed cross bar of road direction；The crossbar end and institute
Guide rail is stated to be fixedly connected；The guide rail includes two vertical rails arranged in parallel, and to be fixedly connected on two vertical rails same
The connection rail of the arc for being used for trolley component turning commutation at end；The vertical rail of connection and the connection rail upper end are formed
Head track；The vertical rail of connection and the connection rail lower end form bottom rail；The head track end forms the upper gear being directed downward
Plate；The bottom rail end forms the lower baffle plate of direction upward；The vertical rail of connection and the connection rail lateral surface are fixedly mounted
There is transmission guide rail；The trolley component include two moving assemblies for being slidably connected on guide rail and with two described mobile group
Part rotates the feeding pannel of connection；The moving assembly is connected with the feeding pannel by pin rotation；The moving assembly includes
Supporting plate for installing feeding pannel；The supporting plate lower end forms the tilt prop for supporting trolley component；The tilt prop end
Portion is provided with multiple the first rollers being connected with lower baffle plate lateral surface rolling；The supporting plate is located at the overhead gage and lower block
Riser is formed between plate；The riser upper end forms upper shifting board；The supporting plate is located in guide rail with the upper shifting board
Feeder wheel for making trolley component advance respectively is installed；It is installed in the feeder wheel on upper shifting board and the overhead gage
Side roll is connected, and the feeder wheel being installed on supporting plate is rolled with the vertical rail and is connected；Install the upper shifting board upper surface
There are multiple three rollers being connected with overhead gage lower end rolling；The supporting plate lower surface is provided with the multiple and lower baffle plate
Upper end rolls the second roller of connection；It is provided with the supporting plate feeder wheel corresponding with the upper shifting board for driving institute
State the advance turbin generator of feeder wheel rotation；The riser, which is located in the guide rail, is provided with what is be slidably connected with the transmission guide rail
Contact slipper；The upper shifting board upper end is fixedly connected with towards the inside support block on the inside of the overhead gage；The internal branch
Bracer is provided with the branch fastener offseted with the overhead gage medial surface towards overhead gage inner side；The supporting plate is led away from described
Rail one end is provided with the first connection electrode for being connected with the feeding pannel；The first connection electrode center forms first
Through hole；The feeding pannel upper surface is fixedly connected with the second electromagnet；The power supply electricity of annular is installed on second electromagnet
Pole；Two the second through holes are formed at the first through hole of two moving assemblies of the feeding pannel correspondence；Under the feeding pannel
Two the second connection electrodes are installed at first connection electrode of end two moving assemblies of correspondence；Installed at the top of Rechargeable vehicle
There is wire spool；Passed on rear side of the wire spool for the charging wire to charging electric vehicle；The charging wire other end connection
There is terminal pad；The wire spool upper end, which is fixedly connected with, parks disk；The terminal pad parks disk or institute described in being mobily connected in
State in trolley component；Also include multiple aircraft for being used to carry terminal pad movement.
Preferably：Feeding pannel upper surface center is painted with for the first positioning for the Aerial vehicle position
Mark；Described park is fixedly connected with ring electromagnet on disk；The insulation tank of annular is installed on the ring electromagnet；It is described
The controller of ring electromagnet is arranged on electric automobile；The terminal pad is circular disk；The terminal pad upper end is provided with
Multigroup iron block groove, every group of iron block groove is four circular grooves for being provided with iron block；The terminal pad lower end is provided with the annular iron of annular
Block；The annular iron block lower end is provided with the first receiving electrode for being electrically connected with the feeding pannel；The aircraft, dolly
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；Positioned at the upper of connecting tube in the fan installation portion
Side, which is connected with upper bracket, the upper bracket, is provided with driving fan；It is located at the lower section of connecting tube in the fan installation portion
It is connected with lower carriage, the lower carriage and lower driving fan is installed；The steering phase of the upper driving fan and lower driving fan
Instead, and in the fan installation portion internal diameter for installing driving fan section is more than the lower driving fan portion of installation in fan installation portion
It is located in the internal diameter divided, and fan blade diameter of the fan blade diameter more than lower driving fan of upper driving fan, the fan installation portion
Blast superatmospheric between upper driving fan and lower driving fan so that go out and blast is formed in vane；It is described go out vane bag
The vane upper shell and vane lower house being tightly connected are included, the vane lower house inner circumferential upper end forms interior curved wall, described
The inner circumferential of interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and vane upper shell inner circumferential lower end by multiple dowels
It is tightly connected；Air-out gap wide at the top and narrow at the bottom, the bottom width in air-out gap are formed between the interior curved wall and air outlet guard board
For 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is training wall wide at the top and narrow at the bottom, the taper
The cone angle size in face 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 the axial direction of vane
The angle of 5-20 degree is formed between horizontal direction, and goes out horizontal wind-force and upper drive that the wind of the air-out gap blowout of vane is produced
The rotation direction of the fan blade of dynamic fan is opposite；It is provided with to adjust correspondence position in each described connecting tube and goes out vane air-out speed
The adjusting part of degree, the adjusting part includes motor, the coaxially connected screw rod with motor output shaft, and and screw flight
The valve plate of connection；The valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the middle part of above-below direction in connecting tube
Position；The connecting tube internal upper part forms to install the motor mounting plate of the motor, and the motor mounting plate direction goes out
The side of vane is connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with a upper end court in the connecting tube
To the inclined baffle plate 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 respectively；The main part upper end is connected with one and half
The uniform air inlet for forming strip on the air intake cover of ellipsoidal surface shape, air intake cover；The main part is upper shell and lower casing
Body is tightly connected composition；The lower, outer perimeter of the fan installation portion is to be connected with and control in battery installation section, battery installation section
The battery of circuit board electrical connection；It is a circuit board installation cavity to be located at the top of battery installation section on the fan installation portion,
The control board is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular cover plate；
The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet connected with fan installation portion, the circuit board installation cavity
Lateral wall uniformly 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, respectively connected in Holder joint of rising and falling described in each
There is a undercarriage；The undercarriage includes the support bar being fixedly connected with the Holder joint of rising and falling and is connected on support bar
The first electromagnet away from Holder joint one end of rising and falling, the support bar is downwards；Use is installed below first electromagnet
In the second receiving electrode 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 center line of second electromagnet, ring electromagnet and annular iron block
Circumscribed circle diameter where the rectangle that corresponding first electromagnet is connected to after deploying with the aircraft support bar is equal.
Preferably：The current electrode, the first receiving electrode respectively include two annular electros being arranged concentrically
Polar ring.
Preferably：Speed limit 40km/h during the charging electric vehicle.
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 transmission guide rail and electric automobile, and then to charging electric vehicle.When not carrying out
During charging tasks, terminal pad, which is parked in, parks on disk, makes terminal pad and to park disk by the way that annular iron block and ring electromagnet are attracting
Connection, first receiving electrode is plugged in the insulation tank, while the first electromagnet without the aircraft under aerial mission
With the second electromagnet is attracting aircraft is connected with feeding pannel, current electrode is connected to enter aircraft with the second receiving electrode
Row charging.When electric automobile not enough power supply, below electric automobile during traveling to guide rail, and charge request is sent to server
Signal, server is received after charge request signal, according to the location of electric automobile, and is fed back electric automobile and opened to driving
Direction front end is in below trolley component without charging tasks, at the same by server to rest in the trolley component or away from
The aircraft nearest from the trolley component sends instruction, and aircraft is by the camera manual control installed in lower section and flies to this
The terminal pad upper end that electric automobile is connected, the ring electromagnet during the aircraft declines on the electric automobile breaks
Electricity, the aircraft is directed at the second telltale mark by camera, while aircraft is horizontally rotated, makes four the first electromagnet
With one group of iron block groove is attracting aircraft is connected with terminal pad；Wire spool work on server controls electric automobile makes charging
Line extends, and is moved to while controlling aircraft to carry terminal pad above trolley component, now the second electromagnet in trolley component
It is powered, control aircraft, which is directed at the decline of the first telltale mark, makes current electrode be connected with the first receiving electrode, so that electronic vapour
Car charges；The advance turbin generator work of trolley component is controlled in charging process, trolley component is moved with electric automobile during traveling；
Carry-on first electromagnet is then controlled to power off, aircraft disengages with terminal pad and carries out other tasks.When electric automobile fills
Control aircraft is connected after being moved to above trolley component with terminal pad after electricity is finished, and the second electromagnet in trolley component breaks
Electricity, terminal pad and charging board disconnect, and subsequent aircraft carries terminal pad and parked to parking on disk.When the dolly in charging tasks
When the trolley component for not carrying out charging tasks is parked in front of component, feeding back to server and sending move makes not charged
Trolley component move forward, until charging in trolley component complete charging tasks.
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；Led by dolly with transmission of electricity
Rail is connected powers to electric automobile, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft, which is carried, to be connected
Disk is connect to charging electric vehicle, potential safety hazard when can avoid manual powered；When Rechargeable vehicle is started to charge up, aircraft with
Terminal pad is disconnected, compared to aircraft with more rationally using aircraft and can be saved into the case of terminal pad one
This；Trolley component is set to complete charging tasks arrival side road pair with the connection rail that one end end is connected with two vertical rails
Should stand can be moved to above reverse track after the end of rail along connection rail；The disk of parking is fixedly connected on electric automobile,
To deposit the terminal pad under non-charged state；The dolly under charged state is not carried out to electric automobile under off working state
Aircraft charging, 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 charging electric vehicle state.
Fig. 4 is the structural representation of the non-charged state of electric automobile.
Fig. 5 is the structural representation of trolley component.
Fig. 6 is the structural representation of feeding pannel.
Fig. 7, Fig. 8 are the structural scheme of mechanism of moving assembly.
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, cross bar；2nd, trolley component；21st, moving assembly；211st, supporting plate；2111st, first leads to
Hole；2112nd, the first connection electrode；212nd, riser；213rd, tilt prop；214th, feeder wheel；215th, advance turbin generator；216a, first
Roller；216b, the second roller；216c, three rollers；217th, contact slipper；218th, upper shifting board；22nd, feeding pannel；221st, second
Electromagnet；222nd, current electrode；223rd, the second through hole；224th, the second connection electrode；225th, the first telltale mark；31st, wire spool；
311st, charging wire；32nd, disk is parked；321st, ring electromagnet；322nd, insulation tank；323rd, the second telltale mark；4th, terminal pad；41、
Iron block groove；42nd, annular iron block；43rd, the first receiving electrode；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 casing
Body；5112nd, vane lower house；51121st, interior curved wall；51122nd, dowel；51123rd, air outlet guard board；51124th, training wall；512、
Connecting tube；5121st, 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, seal
Mouth cap；5331st, spring locating rod；534th, connecting rod；535th, support bar；5351st, connecting rod tank；536th, the first electromagnet；5361st,
Two receiving electrodes；537th, spring；54th, air intake cover；551st, upper driving fan；552nd, lower driving fan；56th, adjusting part；561、
Motor；562nd, screw rod；563rd, valve plate；57th, control board；6th, guide rail；61st, rail is found；62nd, bottom rail；63rd, head track；64th, upper gear
Plate；65th, lower baffle plate；66th, transmission guide rail；67th, rail is connected；.
Embodiment
Embodiment 1
According to Fig. 1 to Figure 18, the present embodiment is a kind of pure electric automobile electric power system, is included multiple along road centre etc.
Away from the electric pole 1 being vertically installed in the middle of two-way lane, the guide rail 6 that is located on electric pole above road is fixedly mounted on and many
The individual trolley component 2 being slidably connected on guide rail.
The trolley component include two moving assemblies 21 for being slidably connected on guide rail and with two described mobile group
Part rotates the feeding pannel 22 of connection.
Wire spool 31 is installed at the top of Rechargeable vehicle；Passed on rear side of the wire spool for filling to charging electric vehicle
Electric wire 311；The charging wire other end is connected with terminal pad 4；The wire spool upper end, which is fixedly connected with, parks disk 32；The company
Connect disk and be mobily connected in described park on disk or the dolly；Also include multiple aircraft 5 for being used to carry terminal pad movement.
Each electric pole includes the vertical rod 11 that vertical direction is set；The vertical rod upper end is fixedly connected with two directions
The horizontally disposed cross bar 12 in both sides of the road；The crossbar end is fixedly connected with the guide rail.
The guide rail includes two vertical rails 61 arranged in parallel, and is fixedly connected on use of two vertical rails with one end
In the connection rail 67 of the arc of trolley component turning commutation；The vertical rail of connection and the connection rail upper end form head track
63；The vertical rail of connection and the connection rail lower end form bottom rail 62；The head track end forms the upper gear being directed downward
Plate 64；The bottom rail end forms the lower baffle plate 65 of direction upward；The vertical rail of connection and the connection rail lateral surface are fixed
Transmission guide rail 66 is installed.
The moving assembly is connected with the feeding pannel by pin rotation；The moving assembly includes being used to install power supply
The supporting plate 211 of disk；The supporting plate lower end forms the tilt prop 213 for supporting trolley component；Install the tilt prop end
There are multiple the first roller 216a being connected with lower baffle plate lateral surface rolling；The supporting plate is located at the overhead gage and lower baffle plate
Between form riser 212；The riser upper end forms upper shifting board 218；The supporting plate is located at the upper shifting board leads
Feeder wheel 214 for making trolley component advance respectively is installed in rail；Be installed on the feeder wheel on upper shifting board with it is described
Side roll is connected in overhead gage, and the feeder wheel being installed on supporting plate is rolled with the vertical rail and is connected；On the upper shifting board
End face is provided with multiple three rollers 216c being connected with overhead gage lower end rolling；The supporting plate lower surface is provided with multiple
The second roller 216b being connected is rolled with the lower baffle plate upper end；At the supporting plate feeder wheel corresponding with the upper shifting board
Advance turbin generator 215 for driving the feeder wheel to rotate is installed；The riser, which is located in the guide rail, to be provided with and institute
State the contact slipper 217 that transmission guide rail is slidably connected；The supporting plate is provided with away from described guide rail one end to be used for and the power supply
First connection electrode 2112 of disk connection；The first connection electrode center forms first through hole 2111；On the feeding pannel
End face is fixedly connected with the second electromagnet 221；The current electrode 222 of annular is installed on second electromagnet；The power supply
Two the second through holes 223 are formed at the first through hole of disk two moving assemblies of correspondence；The feeding pannel lower end correspondence two
Two the second connection electrodes 224 are installed at first connection electrode of the individual moving assembly；Feeding pannel upper surface center
It is painted with for the first telltale mark 225 for the Aerial vehicle position.Make positioned at the feeder wheel of guide rail interior described small
Car component is slided along the guide rail, and being mutually butted on respectively by the feeder wheel on the inside of vertical trackside face and overhead gage prevents the movement
Component is rolled；Four are formed between the junction of second through hole on the feeder wheel and charging board on two moving assemblies
Side shape structure, can enable the trolley component pass through by connecting during rail by the deformation of quadrangle, whole by dolly
The limitation of body length is small.
During charging electric vehicle, the terminal pad is connected with the feeding pannel, and electric current is exported from transmission guide rail, is sequentially passed through
Contact slipper, is transferred to feeding pannel by the first connection electrode and the second connection electrode, charging wire is transferred to through terminal pad after
Charging electric vehicle is given afterwards.
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.
Described park is fixedly connected with ring electromagnet 321 on disk；The insulation of annular is installed on the ring electromagnet
Groove 322；The disk upper surface center of parking is painted with for the second telltale mark 323 for the Aerial vehicle position；The ring
The controller of shape electromagnet is arranged on electric automobile.
The terminal pad is carried and moved by the aircraft and is connected with the feeding pannel to charging electric vehicle.Work as institute
When stating aircraft and carrying terminal pad movement, the aircraft is connected with the terminal pad upper end；During charging electric vehicle, institute
Feeding pannel is stated to be connected with the terminal pad lower end.
The terminal pad is annular；Multigroup iron block groove is installed at the terminal pad upper end correspondence first electromagnet,
Every group of iron block groove is four circular grooves for being provided with iron block, the circular groove deploy respectively with the aircraft after first electromagnet
Correspondence；The terminal pad lower end is provided with the annular iron block 42 of annular；The annular iron block lower end is provided with for being supplied with described
First receiving electrode 43 of electroplax electrical connection.
Diameter of a circle and the aircraft branch where the center line of second electromagnet, ring electromagnet and annular iron block
Circumscribed circle diameter where the rectangle that the first electromagnet of correspondence is connected to after strut expansion is equal.
The aircraft, trolley component, electric automobile are connected by wireless signal and the server communication of system.
The current electrode, the first receiving electrode, the first connection electrode, the second connection electrode respectively include two with one heart
The annular electro polar ring of setting.
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 transmission guide rail and electric automobile
Between set up connection, and then to charging electric vehicle.When no progress charging tasks, terminal pad, which is parked in, parks on disk, leads to
Cross annular iron block and ring electromagnet is attracting terminal pad is connected with parking disk, first receiving electrode is plugged on the insulation
In groove, aircraft is set to connect with feeding pannel while the first electromagnet and the second electromagnet without the aircraft under aerial mission are attracting
Connect, current electrode is 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 open to direction of traffic front end be in the trolley component without charging tasks under
Side, at the same by server to rest in the trolley component or the aircraft nearest apart from the trolley component send instruct,
The terminal pad upper end that aircraft is connected by the camera manual control installed in lower section and the electric automobile that flies to, it is described to fly
Ring electromagnet power-off during row device declines on the electric automobile, the aircraft is positioned by camera alignment second
Mark, while aircraft is horizontally rotated, makes four the first electromagnet and one group of iron block groove is attracting makes aircraft and terminal pad phase
Connection；Wire spool work on server controls electric automobile extends charging wire, is moved while controlling aircraft to carry terminal pad
Move to above trolley component, now the second electromagnet in trolley component is powered, control aircraft is aligned under the first telltale mark
Drop makes current electrode be connected with the first receiving electrode, so that charging electric vehicle；Controlled in charging process before trolley component
Enter turbin generator work, trolley component is moved with electric automobile during traveling；Carry-on first electromagnet is then controlled to power off,
Aircraft disengages with terminal pad and carries out other tasks.Aircraft is controlled to be moved in trolley component after charging electric vehicle is finished
Fang Houyu terminal pads are connected, and the second electromagnet power-off in trolley component, terminal pad disconnects with charging board, and subsequent aircraft is taken
Band terminal pad is parked to parking on disk.The dolly group for not carrying out charging tasks is parked in front of the trolley component in charging tasks
During part, feed back to server and sending move moves forward the trolley component not charged, until small in charging
Car component completes charging tasks.
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；Led by dolly with transmission of electricity
Rail is connected powers to electric automobile, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft, which is carried, to be connected
Disk is connect to charging electric vehicle, potential safety hazard when can avoid manual powered；When Rechargeable vehicle is started to charge up, aircraft with
Terminal pad is disconnected, compared to aircraft with more rationally using aircraft and can be saved into the case of terminal pad one
This；Trolley component is set to complete charging tasks arrival side road pair with the connection rail that one end end is connected with two vertical rails
Should stand can be moved to above reverse track after the end of rail along connection rail；The disk of parking is fixedly connected on electric automobile,
To deposit the terminal pad under non-charged state；The dolly under charged state is not carried out to electric automobile under off working state
Aircraft charging, and to aircraft offer storage place.
Embodiment 2
According to Figure 19 to Figure 20, the present embodiment has done following improvement on the basis of embodiment 1：Go out described in each in vane
Week forms Holder joint 5110 of rising and falling away from the position of connecting tube, and a undercarriage is respectively connected with Holder joint of rising and falling described in each
53；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 531, is slidably mounted on the sliding tube 532 in connection pipe body, and company is rotated close to Holder joint one end of rising and falling with connection pipe body
The support bar 535 connect, is connected on support bar away from first electromagnet 536 of Holder joint one end of rising and falling, and respectively with slip
The connecting rod 534 of connection is rotated in the middle part of pipe, in the middle part of support bar；It is provided with below first electromagnet for being charged to aircraft
Second receiving electrode 5361.
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 iron block groove are attracting, but goes out vane
The power that interior blast is produced is insufficient to allow support bar to pack up.
Claims (8)
1. a kind of pure electric automobile electric power system, it is characterised in that：Include it is multiple along in the middle of road it is equidistant be vertically installed at it is double
To the electric pole in the middle of track, it is fixedly mounted on the guide rail that is located on electric pole above road and multiple is slidably connected at guide rail
On trolley component；
Each electric pole includes the vertical rod that vertical direction is set；The vertical rod upper end is fixedly connected with two towards road two
The horizontally disposed cross bar in side；The crossbar end is fixedly connected with the guide rail；
The guide rail includes two vertical rails arranged in parallel, and is fixedly connected on two vertical rails with one end for described
The connection rail of the arc of trolley component turning commutation；The vertical rail of connection and the connection rail upper end form head track；The company
Connect vertical rail and the connection rail lower end forms bottom rail；The head track end forms the overhead gage being directed downward；The bottom rail
End forms the lower baffle plate of direction upward；The vertical rail of connection and the connection rail lateral surface are installed with transmission guide rail；
The trolley component includes two moving assemblies being slidably connected on guide rail and rotated with two moving assemblies
The feeding pannel of connection；The moving assembly is connected with the feeding pannel by pin rotation；The moving assembly includes being used to pacify
Fill the supporting plate of feeding pannel；The supporting plate lower end forms the tilt prop for supporting trolley component；Install the tilt prop end
There are multiple the first rollers being connected with lower baffle plate lateral surface rolling；The supporting plate is located between the overhead gage and lower baffle plate
Form riser；The riser upper end forms upper shifting board；The supporting plate is located in guide rail with the upper shifting board respectively to be installed
There is the feeder wheel for making trolley component advance；It is installed on the feeder wheel on upper shifting board and side roll in the overhead gage
Connection, the feeder wheel being installed on supporting plate is rolled with the vertical rail and is connected；The upper shifting board upper surface is provided with multiple
The three rollers being connected are rolled with the overhead gage lower end；The supporting plate lower surface is provided with the multiple and lower baffle plate upper end and rolled
Second roller of dynamic connection；It is provided with the supporting plate feeder wheel corresponding with the upper shifting board for driving the advance
Take turns the advance turbin generator rotated；The riser is located at the contact cunning for being provided with and being slidably connected with the transmission guide rail in the guide rail
Block；The upper shifting board upper end is fixedly connected with towards the inside support block on the inside of the overhead gage；The internal support block court
The branch fastener offseted with the overhead gage medial surface is installed on the inside of to the overhead gage；The supporting plate is away from described guide rail one end
The first connection electrode for being connected with the feeding pannel is installed；The first connection electrode center forms first through hole；
The feeding pannel upper surface is fixedly connected with the second electromagnet；The current electrode of annular is installed on second electromagnet；Institute
Two the second through holes are formed at the first through hole for stating feeding pannel two moving assemblies of correspondence；The feeding pannel lower end correspondence
Two the second connection electrodes are installed at the first connection electrode of two moving assemblies；
Wire spool is installed at the top of Rechargeable vehicle；Passed on rear side of the wire spool for the charging wire to charging electric vehicle；
The charging wire other end is connected with terminal pad；The wire spool upper end, which is fixedly connected with, parks disk；The terminal pad may move
It is connected to described park in disk or the trolley component；Also include multiple aircraft for being used to carry terminal pad movement.
2. a kind of pure electric automobile electric power system as claimed in claim 1, it is characterised in that：Feeding pannel upper surface center
It is painted with for the first telltale mark for the Aerial vehicle position；
Described park is fixedly connected with ring electromagnet on disk；The insulation tank of annular is installed on the ring electromagnet；It is described
The controller of ring electromagnet is arranged on electric automobile；
The terminal pad is circular disk；The terminal pad upper end is provided with multigroup iron block groove, and every group of iron block groove is four installations
There is the circular groove of iron block；The terminal pad lower end is provided with the annular iron block of annular；The annular iron block lower end be provided with for
First receiving electrode of the feeding pannel electrical connection；
The aircraft, trolley component, electric automobile are connected by wireless signal and the server communication of system.
3. a kind of pure electric automobile electric power system as claimed in claim 1, it is characterised in that：The aircraft includes main body
Portion, the main part includes the fan installation portion of tubular, is connected to fan installation portion periphery and is connected with fan installation portion
The connecting tube of four logical equidistant arrangements, and be connected to each connecting tube outer end and with going out that correspondence position connecting tube is connected
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 pure electric automobile electric power system as claimed in claim 3, it is characterised in that：Go out vane inner circumferential described in each remote
Position from connecting tube forms Holder joint of rising and falling, and a undercarriage is respectively connected with Holder joint of rising and falling described in each；Described
Fall frame and include the connection pipe body 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, it is sliding
The dynamic sliding tube in connection pipe body, the support bar being connected, connection are rotated with connection pipe body close to Holder joint one end of rising and falling
The first electromagnet away from Holder joint one end of rising and falling on support bar, and respectively with being rotated in the middle part of sliding tube, in the middle part of support bar
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 pure electric automobile electric power system as claimed in claim 3, it is characterised in that：The axial direction of the vane and fan
The radial direction of installation portion is perpendicular, and goes out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and goes out going out for vane
The horizontal wind-force that the wind of wind gap blowout is produced is opposite with the rotation direction of the fan blade of upper driving fan.
6. a kind of pure electric automobile electric power system as claimed in claim 2, it is characterised in that：Second electromagnet, annular
Diameter of a circle where the center line of electromagnet and annular iron block and corresponding first electromagnetism iron phase after aircraft support bar expansion
Circumscribed circle diameter where the rectangle being linked to be is equal.
7. a kind of pure electric automobile electric power system as claimed in claim 2, it is characterised in that：The current electrode, first connect
Receiving electrode, the first connection electrode, the second connection electrode respectively includes two annular electro polar rings being arranged concentrically.
8. a kind of pure electric automobile electric power system as claimed in claim 2, it is characterised in that：The charging electric vehicle time limit
Fast 40km/h.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810109939.XA CN108312872A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile power supply system |
| CN201810109951.0A CN108215919A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
| CN201710488025.4A CN107310413B (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488025.4A CN107310413B (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
Related Child Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810109951.0A Division CN108215919A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
| CN201810109939.XA Division CN108312872A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile power supply system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107310413A true CN107310413A (en) | 2017-11-03 |
| CN107310413B CN107310413B (en) | 2018-05-01 |
Family
ID=60180259
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810109939.XA Withdrawn CN108312872A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile power supply system |
| CN201710488025.4A Active CN107310413B (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
| CN201810109951.0A Withdrawn CN108215919A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810109939.XA Withdrawn CN108312872A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile power supply system |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810109951.0A Withdrawn CN108215919A (en) | 2017-06-23 | 2017-06-23 | A kind of pure electric automobile electric power system |
Country Status (1)
| Country | Link |
|---|---|
| CN (3) | CN108312872A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583444A (en) * | 2018-05-14 | 2018-09-28 | 福建三龙新能源汽车有限公司 | One kind carrying the shared electric classic car of staircase structure |
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| US20120085612A1 (en) * | 2009-02-20 | 2012-04-12 | Churchill Frederick | Vehicle propulsion energy and utility power delivery system |
| CN203410320U (en) * | 2012-01-31 | 2014-01-29 | 乔伊·姆·特拉华公司 | Vehicle and overhead electric structure for vehicle |
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| US20170136887A1 (en) * | 2015-11-13 | 2017-05-18 | NextEv USA, Inc. | Electric vehicle aerial vehicle charging system and method of use |
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- 2017-06-23 CN CN201810109939.XA patent/CN108312872A/en not_active Withdrawn
- 2017-06-23 CN CN201710488025.4A patent/CN107310413B/en active Active
- 2017-06-23 CN CN201810109951.0A patent/CN108215919A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201102628Y (en) * | 2007-09-10 | 2008-08-20 | 新疆生产建设兵团建筑工程科学技术研究院有限责任公司 | Connecting line power aerial vehicle |
| US20120085612A1 (en) * | 2009-02-20 | 2012-04-12 | Churchill Frederick | Vehicle propulsion energy and utility power delivery system |
| CN203410320U (en) * | 2012-01-31 | 2014-01-29 | 乔伊·姆·特拉华公司 | Vehicle and overhead electric structure for vehicle |
| US20170136887A1 (en) * | 2015-11-13 | 2017-05-18 | NextEv USA, Inc. | Electric vehicle aerial vehicle charging system and method of use |
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| CN108583444A (en) * | 2018-05-14 | 2018-09-28 | 福建三龙新能源汽车有限公司 | One kind carrying the shared electric classic car of staircase structure |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108215919A (en) | 2018-06-29 |
| CN108312872A (en) | 2018-07-24 |
| CN107310413B (en) | 2018-05-01 |
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| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Li Fangren Inventor after: Tian Enping Inventor after: Qi Ruihao Inventor after: Shang Qingdong Inventor before: Yu Lili Inventor before: Jiang Jiahui |
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| TA01 | Transfer of patent application right | ||
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Effective date of registration: 20180321 Address after: 276500 No. 1 Rizhao East Road, Juxian Economic Development Zone, Shandong, Rizhao City Applicant after: HAIHUI NEW ENERGY MOTOR Co.,Ltd. Address before: 325000 Wenzhou economic and Technological Development Zone, Wenzhou, Zhejiang Province, 3 A District, No. 329, Jinhai, No. 329 Applicant before: WENZHOU RUICHU TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20211224 Address after: 276500 No. 23, Caihong Road, Zhaoxian Town, Ju county, Rizhao City, Shandong Province Patentee after: HAIHUI MOTOR Co.,Ltd. Patentee after: HAIHUI NEW ENERGY MOTOR Co.,Ltd. Address before: 276500 1 Rizhao East Road, Juxian Economic Development Zone, Rizhao City, Shandong Patentee before: HAIHUI NEW ENERGY MOTOR Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: A Pure Electric Vehicle Power Supply System Effective date of registration: 20230614 Granted publication date: 20180501 Pledgee: Bank of Rizhao Co.,Ltd. Juxian sub branch Pledgor: HAIHUI MOTOR Co.,Ltd. Registration number: Y2023980043838 |