CN107264316A - A kind of charging system for electric automobile of use guide rail transmission of electricity - Google Patents
A kind of charging system for electric automobile of use guide rail transmission of electricity Download PDFInfo
- Publication number
- CN107264316A CN107264316A CN201710488123.8A CN201710488123A CN107264316A CN 107264316 A CN107264316 A CN 107264316A CN 201710488123 A CN201710488123 A CN 201710488123A CN 107264316 A CN107264316 A CN 107264316A
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- China
- Prior art keywords
- fan
- vane
- guide rail
- plate
- electric automobile
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- 230000005540 biological transmission Effects 0.000 title claims abstract description 35
- 230000005611 electricity Effects 0.000 title claims abstract description 28
- 238000009434 installation Methods 0.000 claims description 77
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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 13
- 238000009413 insulation Methods 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 230000033228 biological regulation Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000003068 static effect Effects 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 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
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000001149 thermolysis Methods 0.000 description 1
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
- B60L5/00—Current collectors for power supply lines of electrically-propelled vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—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
- 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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- H02J7/0027—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (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 charging system for electric automobile of use guide rail transmission of electricity, include multiple electric poles being equidistantly vertically installed at along road by 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 charging electric vehicle system of use guide rail transmission of electricity
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 defeated using guide rail
The charging system for electric automobile of electricity.
To realize the purpose of the present invention, it is achieved using following technical scheme：A kind of electronic vapour of use guide rail transmission of electricity
Car charging system, includes multiple electric poles being equidistantly vertically installed at along road by road, is fixedly mounted on electric pole upper
Guide rail and multiple trolley components being slidably connected on guide rail above road；
The guide rail includes horizontally disposed traveling rail；The traveling rail upper center is formed for positioning the trolley component
Transmission of electricity mounting rail；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail for power supply；The traveling rail is close to institute
Electric pole one end is stated to form for preventing the position-limited rail of the trolley component inclination；
At the location and installation plate inwall upper end correspondence transmission guide rail contact is installed with along trolley component length direction
Draw runner, the contact strip is slidably connected with the transmission guide rail；The traveling plate and the installing plate upper surface are fixed respectively
It is connected with two motor mounting plates；The motor mounting plate side is provided with multiple advance turbin generators；Each described feeder wheel electricity
The output shaft end of machine is fixedly connected with the feeder wheel for making trolley component advance；The traveling plate is corresponding with the installing plate each
Multiple square holes for being used to pass through for the feeder wheel are formed at the individual feeder wheel；The power supply installing plate is located remotely from described
Electric pole side；Multiple roll with upper surface in the position-limited rail is installed along the dolly length direction on the traveling plate to connect
The roller connect；The feeding pannel upper surface is fixedly connected with the second electromagnet；The confession of annular is installed on second electromagnet
Electrode；
The trolley component includes the location and installation plate being slidably connected on the guide rail, is integrally formed respectively in location and installation plate
Lower end both sides and horizontally disposed power supply installing plate and traveling plate, and the power supply being fixedly connected on the power supply installing plate
Disk；
Electromobile at top is provided with wire spool；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.
Preferably：Each electric pole includes the vertical rod that vertical direction is set；The vertical rod upper end, which is fixed, to be connected
It is connected to towards the horizontally disposed cross bar of road direction；The crossbar end is fixedly connected with the guide rail；
Feeding pannel upper surface center 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.
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 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
Below trolley component that direction remains static foremost, 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.
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；Aircraft is taken
Band terminal pad is to charging electric vehicle, potential safety hazard when can avoid manual powered；When electric automobile is started to charge up, flight
Device is disconnected with terminal pad, compared to aircraft with more rationally using aircraft and can be saved in the case of terminal pad one
About cost；The disk of parking is fixedly connected on electric automobile, to deposit the terminal pad under non-charged state；Not to electronic
The trolley component that automobile is carried out under charged state charges to the aircraft under off working state, and is deposited to the offer of aircraft
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, Fig. 6 are the structural representations of trolley component.
Fig. 7, Fig. 8 are the structural representations of terminal pad.
Structural representation when Fig. 9 is aircraft grounding state or carries terminal pad.
Figure 10 is the structural representation under aircraft free flight state.
Figure 11 is the cross section structure diagram of aircraft.
Figure 12 is Figure 11 A portions schematic enlarged-scale view.
Figure 13 is Figure 11 B portions schematic enlarged-scale view.
The structural representation of each part that Figure 14 is upper shell and is connected with upper shell.
Figure 15 is the structural representation of lower housing section.
Figure 16 is the cross section structure diagram of lower housing section.
Figure 17 is the cross section structure diagram of undercarriage part.
Figure 18 is the decomposition texture schematic diagram of undercarriage part.
1st, electric pole；11st, mobile jib；12nd, cross bar；2nd, trolley component；21st, location and installation plate；211st, contact strip；22nd, supply
Electric installing plate；221st, the first telltale mark；23rd, feeding pannel；231st, the second electromagnet；232nd, current electrode；24th, feeder wheel；25、
Advance turbin generator；26th, motor mounting plate；27th, roller；28th, square hole；29th, traveling plate；31st, wire spool；311st, charging wire；32nd, stop
Sale at reduced prices；321st, ring electromagnet；322nd, insulation tank；323rd, the second telltale mark；4th, terminal pad；41st, 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, arrange
Air holes；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；5121st, motor is pacified
Fill plate；5122nd, valve plate guide rod；5123rd, baffle plate；513rd, cover plate；52nd, battery；53rd, undercarriage；531st, connection pipe body；5311、
Hinged seat；5312nd, strip shape gob；532nd, sliding tube；5321st, piston；5322nd, articulated joint；533rd, sealing cap；5331st, spring is positioned
Bar；534th, connecting rod；535th, support bar；5351st, connecting rod tank；536th, the first electromagnet；5361st, the second receiving electrode；537th, bullet
Spring；54th, air intake cover；551st, upper driving fan；552nd, lower driving fan；56th, adjusting part；561st, motor；562nd, screw rod；563、
Valve plate；57th, control board；6th, guide rail；61st, traveling rail；62nd, position-limited rail；63rd, transmission of electricity mounting rail；64th, transmission guide rail.
Embodiment
Embodiment 1
According to Fig. 1 to Figure 16, the present embodiment is the charging system for electric automobile that a kind of use guide rail is transmitted electricity, and is included multiple
The electric pole 1 by road is equidistantly vertically installed at along road, be fixedly mounted on electric pole be located at road above guide rail 6 and
Multiple trolley components 2 being slidably connected on guide rail.
The trolley component includes the location and installation plate 21 being slidably connected on the guide rail, is integrally formed respectively in positioning
Installing plate lower end both sides and horizontally disposed power supply installing plate 22 and traveling plate 29, and it is fixedly connected on the power supply installing plate
On feeding pannel 23.
Electromobile at top is provided with wire spool 31；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 towards road
The horizontally disposed cross bar 12 in direction；The crossbar end is fixedly connected with the guide rail.
The guide rail includes horizontally disposed traveling rail 61；The traveling rail upper center forms described small for positioning
The transmission of electricity mounting rail 63 of car component；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail 64 for power supply；The row
Enter rail to form for preventing the position-limited rail 62 of the trolley component inclination close to described electric pole one end.
It is installed with the location and installation plate inwall upper end correspondence transmission guide rail along trolley component length direction
Contact strip 211, the contact strip is slidably connected with the transmission guide rail；The traveling plate and the installing plate upper surface point
Two motor mounting plates 26 are not fixedly connected with；The motor mounting plate side is provided with multiple advance turbin generators 25；Each institute
The output shaft end for stating advance turbin generator is fixedly connected with for making the feeder wheel 24 of trolley component advance；The traveling plate and described
Installing plate, which is corresponded to, forms multiple square holes 28 for being used to pass through for the feeder wheel at each described feeder wheel；The power supply is installed
Plate is located remotely from the electric pole side；The multiple and position-limited rail is installed along the dolly length direction on the traveling plate
Interior upper surface rolls the roller 27 of connection；The feeding pannel upper surface is fixedly connected with the second electromagnet 231；Second electromagnetism
The current electrode 232 of annular is installed on iron；Feeding pannel upper surface center is painted with for for the Aerial vehicle position
First telltale mark 221.The position-limited rail offsets with the roller slip, prevents trolley component because of feeding pannel side preponderance
And roll, and therefore, it is possible to make between the contact strip and the transmission guide rail, the feeder wheel and the traveling rail it
Between effectively contact；Feeder wheel described in the feeder wheel motor control, which is rotated, makes the trolley component be moved along the guide rail.
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 strip, is transferred to feeding pannel, and charging electric vehicle is given after being transferred to charging wire through terminal pad after.
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 respectively include two annular electro polar rings being arranged concentrically.
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 and open under the trolley component remained static foremost to direction of traffic
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 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；Aircraft is taken
Band terminal pad is to charging electric vehicle, potential safety hazard when can avoid manual powered；When electric automobile is started to charge up, flight
Device is disconnected with terminal pad, compared to aircraft with more rationally using aircraft and can be saved in the case of terminal pad one
About cost；The disk of parking is fixedly connected on electric automobile, to deposit the terminal pad under non-charged state；Not to electronic
The trolley component that automobile is carried out under charged state charges to the aircraft under off working state, and is deposited to the offer of aircraft
Place.
Embodiment 2
According to Figure 17 to Figure 18, 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 charging system for electric automobile of use guide rail transmission of electricity, it is characterised in that：It is multiple equidistantly vertical along road to include
Electric pole by road, is fixedly mounted on the guide rail being located on electric pole above road and multiple be slidably connected at is led
Trolley component on rail；
The guide rail includes horizontally disposed traveling rail；The traveling rail upper center is formed for positioning the trolley component
Transmission of electricity mounting rail；The transmission of electricity mounting rail upper end is fixedly connected with the transmission guide rail for power supply；The traveling rail is close to institute
Electric pole one end is stated to form for preventing the position-limited rail of the trolley component inclination；
The trolley component includes the location and installation plate being slidably connected on the guide rail, is integrally formed respectively in location and installation plate
Lower end both sides and horizontally disposed power supply installing plate and traveling plate, and the power supply being fixedly connected on the power supply installing plate
Disk；Contact is installed with the location and installation plate inwall upper end correspondence transmission guide rail along trolley component length direction to slide
Bar, the contact strip is slidably connected with the transmission guide rail；The traveling plate and the installing plate upper surface are fixed respectively to be connected
It is connected to two motor mounting plates；The motor mounting plate side is provided with multiple advance turbin generators；Each described advance turbin generator
Output shaft end be fixedly connected with for make trolley component advance feeder wheel；The traveling plate it is corresponding with the installing plate each
Multiple square holes for being used to pass through for the feeder wheel are formed at the feeder wheel；The power supply installing plate is located remotely from the electricity
Line bar side；Multiple roll with upper surface in the position-limited rail is installed along the dolly length direction on the traveling plate to be connected
Roller；The feeding pannel upper surface is fixedly connected with the second electromagnet；The power supply of annular is installed on second electromagnet
Electrode；
Electromobile at top is provided with wire spool；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 charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 1, it is characterised in that：It is each described
Electric pole includes the vertical rod that vertical direction is 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；
Feeding pannel upper surface center 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 charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 1, it is characterised in that：The flight
Device includes main part, and the main part includes the fan installation portion of tubular, is connected to fan installation portion periphery and and wind
The connecting tube for four equidistant arrangements that fan installation portion is connected, and be connected to each connecting tube outer end and be connected with correspondence position
What pipe was 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 charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 3, it is characterised in that：Described in each
Go out position of the vane inner circumferential away from connecting tube and form Holder joint of rising and falling, one is respectively connected with Holder joint of rising and falling described in each and is risen
Fall frame；The undercarriage, which includes, to be fixedly connected with Holder joint of rising and falling and by Holder joint of rising and falling with going out what is be connected inside vane
Connection pipe body, is slidably mounted on the sliding tube in connection pipe body, rotates what is be connected close to Holder joint one end of rising and falling with connection pipe body
Support bar, 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
The connecting rod of connection is rotated in the middle part of bar；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 charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 3, it is characterised in that：The 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 5-20 degree angle,
And it is opposite with the rotation direction of the fan blade of upper driving fan to go out the horizontal wind-force of the wind generation of the air-out gap blowout of vane.
6. a kind of charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 2, it is characterised in that：Described second
Diameter of a circle where the center line of electromagnet, ring electromagnet and annular iron block with the aircraft support bar corresponding the after deploying
Circumscribed circle diameter where the rectangle that one electromagnet is connected to is equal.
7. a kind of charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 2, it is characterised in that：The power supply
Electrode, the first receiving electrode respectively include two annular electro polar rings being arranged concentrically.
8. a kind of charging system for electric automobile of use guide rail transmission of electricity as claimed in claim 2, it is characterised in that：It is described electronic
Speed limit 40km/h when automobile charges.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810112311.5A CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
| CN201710488123.8A CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
| CN201810112314.9A CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488123.8A CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810112311.5A Division CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
| CN201810112314.9A Division CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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| Publication Number | Publication Date |
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| CN107264316A true CN107264316A (en) | 2017-10-20 |
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| CN201810112314.9A Withdrawn CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
| CN201710488123.8A Withdrawn CN107264316A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile of use guide rail transmission of electricity |
| CN201810112311.5A Withdrawn CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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| CN201810112314.9A Withdrawn CN108263235A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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| CN201810112311.5A Withdrawn CN108237922A (en) | 2017-06-23 | 2017-06-23 | A kind of charging system for electric automobile transmitted electricity using guide rail |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110937126A (en) * | 2019-12-20 | 2020-03-31 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106740212B (en) * | 2016-12-29 | 2023-10-24 | 重庆金澳机械制造有限公司 | Electric vehicle charging system |
| CN110481354A (en) * | 2019-06-06 | 2019-11-22 | 上海荣灵电力科技有限公司 | Power supply system and its method of supplying power to based on electric pole charging unit |
| CN110667417A (en) * | 2019-09-23 | 2020-01-10 | 洛阳嘉盛电源科技有限公司 | Integrated pantograph charging system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110937126A (en) * | 2019-12-20 | 2020-03-31 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
| CN110937126B (en) * | 2019-12-20 | 2021-02-02 | 西北工业大学 | Unmanned aerial vehicle takes off and retrieves charging device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108237922A (en) | 2018-07-03 |
| CN108263235A (en) | 2018-07-10 |
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