CN108128192A - Charging system for electric automobile - Google Patents
Charging system for electric automobile Download PDFInfo
- Publication number
- CN108128192A CN108128192A CN201711428204.5A CN201711428204A CN108128192A CN 108128192 A CN108128192 A CN 108128192A CN 201711428204 A CN201711428204 A CN 201711428204A CN 108128192 A CN108128192 A CN 108128192A
- Authority
- CN
- China
- Prior art keywords
- fan
- vane
- aircraft
- mounting portion
- connecting tube
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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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
- B60L53/31—Charging columns specially adapted for electric 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
- 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
- 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
- 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
Abstract
The invention belongs to electric vehicle charging fields, more particularly to a kind of charging system for electric automobile, include multiple electric poles being equidistantly vertically installed at along road by road, it is fixedly mounted on the guide rail being located on electric pole above road, multiple trolleies being slidably connected on guide rail, the terminal pad being connect with each trolley, the electric vehicle of the aircraft being movably connected in above terminal pad and traveling on road.The present invention is arranged on by road, can in time be charged to electric vehicle on road, and not by time restriction, and driver can charge to electric vehicle while driving, and save driver and charge the time waited；It is connected by trolley with power transmission line and is powered to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered.
Description
Technical field
The invention belongs to electric vehicle charging fields, and in particular to a kind of charging system for electric automobile.
Background technology
Electric vehicle has the advantages that prominent the problem of existing simultaneously charging aspect as energy-saving and environment-friendly automobile.It is existing
Charging modes are mainly charging pile, but charging pile, since installation site is fixed, electric vehicle can only rest in charging when charging
Stake is nearby charged；And the time that charging pile needs when charging is long, and electric vehicle can not move when charging.
Invention content
The technical problems to be solved by the invention are：It is filled in view of the deficienciess of the prior art, providing a kind of electric vehicle
Electric system.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of charging system for electric automobile, including
There are multiple electric poles being equidistantly vertically installed at along road by road, be fixedly mounted on the guide rail being located on electric pole above road
And multiple trolleies being slidably connected on guide rail；Power transmission line is installed below the guide rail；The trolley is equipped with charging wire；
The charging wire end is fixedly connected with the terminal pad for being useful for charging to electric vehicle；Further include it is multiple for carry terminal pad shifting
Dynamic aircraft.
Preferably：Each electric pole includes the upright bar of vertical direction setting；The upper part of telegraph pole is fixed
It is connected with towards what road direction was set and parks disk；The upright bar upper end is fixedly connected with towards the horizontally disposed horizontal stroke of road direction
Bar；The crossbar end is fixedly connected with the guide rail；The guide rail includes the symmetrical right angle guide rail of two horizontal directions；
The power transmission line is fixedly mounted on right angle guide rail lower end；The trolley includes trolley framework；The trolley framework includes level side
To bottom plate and two vertical side plates for being fixedly connected on bottom plate upper end both sides；Two side plate upper inner rotations connect
It is connected to multiple feeder wheels；It is fixedly connected at corresponding each feeder wheel on the outside of the side plate multiple for driving the advance
Take turns the first motor of rotation；The trolley is moved by the feeder wheel on the right angle guide rail；On the side plate relative to
The roller being mutually butted on the outside of the right angle guide rail is rotatably connected at the right angle guide rail；The bottom plate upper end be fixedly connected with by
Electrical component；The electric receiving component includes being fixedly connected on transmission of electricity seat of the bottom plate perpendicular to the side plate, is fixedly connected on institute
The guide rod frame of direction upward among transmission of electricity seat is stated, the guide rod frame end is fixedly connected on and is parallel to transmission of electricity the horizontal of seat and lead
Bar；The horizontal guide rod upper end is corresponded to below the power transmission line along installation there are two contact slide plate, the contact slide plate with it is described defeated
Electric wire is slidably connected；Compression spring is fixedly connected between the contact slide plate and the horizontal guide rod；
Two side plate lower rotationals are equipped with reel；Described reel one end is fixedly connected with brush；The reel
On be wound with charging wire, described charging wire one end is fixedly connected with the brush；The transmission of electricity seat, which is located at the brush side, to be fixed
Brush is connected with, the brush is slidably connected with the brush；The charging wire other end pass through bottom plate and with the terminal pad
Electrical connection；It is equipped with that the reel is driven to rotate at the corresponding reel on the outside of side plate far from the brush side
The second motor；
The electric vehicle upper end is equipped with charging board；The charging board upper end is equipped with the first receiving electrode；The charging board
Upper end be located at be fixedly connected on the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnet；
The insulation tank parked disk upper end and form annular；It is described park disk upper end and be located on the outside of the insulation tank be fixedly connected
There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through-hole；The terminal pad lower end corresponds to and is equipped with the first confession at first receiving electrode
Electrode；The take-up reel lower end is equipped with and each corresponding iron block in second electromagnet position；In the terminal pad
End periphery is fixedly connected with the annular iron block for being useful for being connect with terminal pad for aircraft；It is described annular iron block on be equipped with it is described
Corresponding second current electrode of second receiving electrode；
The aircraft, trolley, electric vehicle are connected by wireless signal and the server communication of system；
The contact slide plate lower end is fixedly connected with the electrode wires being electrically connected with the brush.
Preferably：The aircraft includes main part, and the main part includes the fan installation of tubular
Portion, the connecting tube for four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion and is connected to
Each connecting tube outer end and go out vane with what corresponding position connecting tube was connected；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving wind is installed on the upper bracket
Fan；It is located in the fan mounting portion below connecting tube and is connected with lower carriage, lower driving fan is installed on the lower carriage；
The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion
Diameter is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade diameter of upper driving fan is more than lower driving wind
The fan blade diameter of fan, the interior wind pressure superatmospheric between upper driving fan and lower driving fan of the fan mounting portion,
Wind pressure is formed in vane so that going out；
It is described go out vane include the vane upper shell of sealed connection and vane lower housing, the vane lower housing inner circumferential upper end into
Type has interior curved wall, and there are one air outlet guard board, air outlet guard board upper end and wind by the connection of multiple dowels for the inner circumferential of the interior curved wall
Ring upper shell inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board
The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction and formed
The angle of 5-20 degree, and the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane generates
Direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting group in each connecting tube
Part includes motor, coaxially connected screw rod and the valve plate being connect with screw flight with motor output shaft；The valve plate top
Close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube for periphery；The connecting tube internal upper part 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；Upper end direction to go out the inclined baffle in vane direction there are one the connections of lower part in the connecting tube,
The conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly form on air intake cover strip into
Air port；
The main part is tightly connected and forms for upper shell and lower housing；
The lower, outer perimeter of the fan mounting portion is battery installation section, is connected in battery installation section and is electrically connected with control circuit board
Accumulator；Positioned at the top of battery installation section for a circuit board installation cavity on the fan mounting portion, the control circuit
Plate is mounted in circuit board installation cavity, and there are one the cover boards of annular for the circuit board installation cavity lower end connection；The circuit board peace
The upper surface behaveing affectedly uniformly forms the air inlet hole connected in fan mounting portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is equipped with the camera being electrically connected with control circuit board；
It is each it is described go out position of the vane inner circumferential far from connecting tube form Holder joint of rising and falling, it is each in each Holder joint of rising and falling
There are one undercarriages for connection；The undercarriage includes the supporting rod being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet far from Holder joint one end of rising and falling on bar, the supporting rod is downwards；It is installed below first electromagnet
It is useful for the second receiving electrode to charge to aircraft.
Preferably：Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint of rising and falling, it is each
Respectively there are one undercarriages for connection in the Holder joint of rising and falling；The undercarriage, which includes, to be fixedly connected and passes through with Holder joint of rising and falling
Holder joint of rising and falling is with going out the connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connecting tube
Body is connected to the first electricity far from Holder joint one end of rising and falling on supporting rod close to the supporting rod for Holder joint one end rotation connection of rising and falling
Magnet and the respectively connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod；Installation is useful below first electromagnet
In the second receiving electrode to charge to aircraft；
The connection pipe body forms hinged seat close to the Holder joint one end wall that rises and falls, and described supporting rod one end is rotated with hinged seat
Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position is connected with hinged
Head, described connecting rod one end are rotatablely connected with articulated joint, and side wall of the connection pipe body far from Holder joint one end of rising and falling forms confession
The strip shape gob that articulated joint passes through；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap
Inner end is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against piston respectively
Between sealing cap inner end；The connecting rod tank that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod.
Preferably：It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction of vane
The angle of 5-20 degree is formed between horizontal direction, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and upper drive
The rotation direction of the fan blade of dynamic fan is opposite.
Preferably：Diameter of a circle where the annular iron block center line is corresponding after being unfolded with the aircraft support bar
Circumscribed circle diameter where the rectangle that first electromagnet is connected to is equal.
Preferably：First current electrode, the second current electrode, the first receiving electrode, the second receiving electrode
Respectively include two annular electro polar rings being arranged concentrically.Installation on the position of brush is corresponded in the brush, and there are two set with one heart
The annular electro polar ring put.
Preferably：The end terrain clearance of trying to get to the heart of a matter of parking is 3.5-4m.
Preferably：Speed limit 40km/h during the electric vehicle charging.
Preferably：The through-hole diameter is more than the accumulator outer diameter.
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 moves, and so as to make to establish connection between power transmission line and electric vehicle, and then charges to electric vehicle.When not filled
During electric task, terminal pad, which is parked in, parks on disk, terminal pad is made to be connect with parking disk by the way that iron block and permanent magnet are attracting, and described
One current electrode is plugged in the insulation tank, while the first electromagnet without the aircraft under aerial mission and annular iron block phase
Suction makes aircraft be connect with terminal pad, and the second current electrode connect to charge to aircraft with the second receiving electrode.When
During electric vehicle not enough power supply, below electric automobile during traveling to guide rail, and the signal of charge request, service are sent to server
After device receives charge request signal, according to the location of electric vehicle, and feed back electric vehicle open to direction of traffic most before
It holds below the trolley that remains static, while instruction, flight is sent by the server nearest aircraft of the trolley of adjusting the distance
The terminal pad upper end that device artificially controls the trolley that flies to be connected by being mounted on the camera of lower section, the aircraft declined
The second electromagnet power-off described in journey on electric vehicle, each first electromagnet with annular iron block is attracting makes aircraft with connecting
Disk is connected；The corresponding second motor work of server controls trolley extends charging wire while aircraft is controlled to carry terminal pad
It is moved to above electric vehicle, the second electromagnet on electric vehicle is powered at this time, and control aircraft decline makes the first power supply electric
Pole is connect with the first receiving electrode, so as to which electric vehicle be made to charge, aircraft is then controlled to drive connection disc spins, makes terminal pad
The second electromagnet on the iron block and charging board of lower end is attracting, so as to which terminal pad be made to be fixed on charging board；It is controlled in charging process
The first motor work of trolley processed, makes trolley be moved with electric automobile during traveling；Then control carry-on first electromagnet
Power-off, aircraft disengage with terminal pad and carry out other tasks.Aircraft is controlled to be moved to after electric vehicle charges electronic
It is connected after above automobile with terminal pad, the second electromagnet power-off on electric vehicle, terminal pad is disconnected with charging board, then flown
Row device carries terminal pad and is connected on subsequent electric vehicle charging or parks terminal pad to parking on disk.When aircraft fills
When electric, the terminal pad parked on disk is parked in by the camera judgement below aircraft, control aircraft is moved to the connection
Above disk, then droping in the terminal pad makes the first electromagnet attracting so as to be attached to aircraft with annular iron block, together
When the second current electrode be electrically connected with the second receiving electrode, so as to charging to aircraft.
The present invention is arranged on by road, can in time be charged to electric vehicle on road, not by time restriction, and be driven
Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；Pass through trolley and power transmission line
It is connected and powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft carries connection
Disk charges to electric vehicle, security risk when can avoid manual powered；When Rechargeable vehicle starts to charge up, aircraft and company
Disk is connect to disconnect, compared in the case of aircraft and terminal pad one can more rationally using aircraft and save into
This；It is described park disk be fixedly connected the terminal pad for, making not need on utility poles to charge to electric vehicle fix storage rather than
Suspension causes to generate hidden danger in the air；Terminal pad fixation is stored in when parking on disk, can be simultaneously to flying under off working state
Row device charges, and stores place to the offer of aircraft.
Description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is the structure diagram of electric pole and guide rail.
Fig. 3 is the structure diagram of electric vehicle.
Fig. 4 is the structure diagram of trolley.
Fig. 5, Fig. 6 are the schematic cross-sectional views of trolley.
Fig. 7, Fig. 8 are the structure diagrams of terminal pad.
Structure diagram when Fig. 9 is aircraft grounding state or carries terminal pad.
Figure 10 is the structure diagram under aircraft free flight state.
Figure 11 is the schematic cross-sectional view of aircraft.
Figure 12 is the A portions schematic enlarged-scale view of Figure 11.
Figure 13 is the B portions schematic enlarged-scale view of Figure 11.
The structure diagram of each component that Figure 14 is upper shell and is connect with upper shell.
Figure 15 is the structure diagram of lower housing section.
Figure 16 is the schematic cross-sectional view of lower housing section.
Figure 17 is the schematic cross-sectional view of undercarriage part.
Figure 18 is the decomposition texture schematic diagram of undercarriage part.
1st, electric pole；11st, mobile jib；12nd, disk is parked；121st, permanent magnet；122nd, insulation tank；13rd, cross bar；2nd, trolley；21st, it is small
Vehicle framework；211st, side plate；212nd, bottom plate；213rd, feeder wheel；2131st, the first motor；214th, roller；22nd, reel；221st, it brushes
Disk；222nd, the second motor；23rd, electric receiving component；231st, transmission of electricity seat；232nd, guide rod frame；233rd, brush；234th, horizontal guide rod；235th, it connects
Touch slide plate；236th, electrode wires；237th, compression spring；24th, charging wire；31st, charging board；32nd, the first receiving electrode；33rd, the second electricity
Magnet；4th, terminal pad；41st, annular iron block；42nd, the first current electrode；43rd, iron block；44th, the second current electrode；45th, through-hole；5、
Aircraft；51st, main part；51a, upper shell；51b, lower housing；510th, fan mounting portion；5101st, upper bracket；5102nd, lower branch
Frame；5103rd, battery installation section；5104th, circuit board installation cavity；5105th, air inlet hole；5106th, vent；5107th, camera；511、
Go out vane；5110th, it rises and falls Holder joint；5111st, vane upper shell；5112nd, vane lower housing；51121st, interior curved wall；51122nd, even
Connect muscle；51123rd, air outlet guard board；51124th, training wall；512nd, connecting tube；5121st, motor mounting plate；5122nd, valve plate guide rod；
5123rd, baffle；513rd, cover board；52nd, accumulator；53rd, undercarriage；531st, connection pipe body；5311st, hinged seat；5312nd, strip shape gob；
532nd, sliding tube；5321st, piston；5322nd, articulated joint；533rd, sealing cap；5331st, spring positioning bar；534th, connecting rod；535th, it supports
Bar；5351st, connecting rod tank；536th, the first electromagnet；5361st, the second receiving electrode；537th, spring；54th, air intake cover；551st, upper drive
Dynamic fan；552nd, lower driving fan；56th, adjusting part；561st, motor；562nd, screw rod；563rd, valve plate；57th, control circuit board；6、
Guide rail；61st, right angle guide rail；62nd, power transmission line.
Specific embodiment
Embodiment 1
According to Fig. 1 to Figure 18, the present embodiment is a kind of charging system for electric automobile, and it is multiple equidistantly vertical along road to include
Electric pole 1 by road is fixedly mounted on electric pole and is located at the guide rail 6 above road and multiple is slidably connected at
Trolley 2 on guide rail；Power transmission line 62 is installed below the guide rail；The trolley is equipped with charging wire 24；The charging wire end
End is fixedly connected with the terminal pad 4 for being useful for charging to electric vehicle；Further include multiple aircraft for being used to carry terminal pad movement
5。
Each electric pole includes the upright bar 11 of vertical direction setting；The upper part of telegraph pole is fixedly connected with towards road
Disk 12 is parked in direction setting；The upright bar upper end is fixedly connected with towards the horizontally disposed cross bar 13 of road direction；The horizontal stroke
Boom end is fixedly connected with the guide rail.
The guide rail includes the symmetrical right angle guide rail 61 of two horizontal directions；The power transmission line is fixedly mounted on right angle
Guide rail lower end.
The trolley includes trolley framework 21；Bottom plate 212 and two of the trolley framework including horizontal direction are vertical
It is fixedly connected on the side plate 211 of bottom plate upper end both sides；Two side plate upper inners are rotatably connected to multiple feeder wheels 213；
Multiple the first electricity for the feeder wheel to be driven to rotate are fixedly connected on the outside of the side plate at corresponding each feeder wheel
Machine 2131；The trolley is moved by the feeder wheel on the right angle guide rail；It is led on the side plate relative to the right angle
The roller 214 being mutually butted on the outside of the right angle guide rail is rotatably connected at rail；The bottom plate upper end is fixedly connected with electric receiving component
23；The electric receiving component includes being fixedly connected on transmission of electricity seat 231 of the bottom plate perpendicular to the side plate, is fixedly connected on described
The guide rod frame 232 of direction upward among transmission of electricity seat is fixedly connected on the guide rod frame end and is parallel to the horizontal stroke of the transmission of electricity seat
Guide rod 234；The horizontal guide rod upper end corresponds to edge installation below the power transmission line, and there are two contact slide plate 235, the contact slide plates
It is slidably connected with the power transmission line；Compression spring 237 is fixedly connected between the contact slide plate and the horizontal guide rod.Described
One motor controls the feeder wheel rotation that the trolley is made to be moved along the guide rail.The compression spring is to the contact slide plate production
Raw upward power makes the contact slide plate effectively be contacted with the power transmission line.
Two side plate lower rotationals are equipped with reel 22；Described reel one end is fixedly connected with brush 221；Institute
It states and charging wire 24 is wound on reel, described charging wire one end is fixedly connected with the brush；The transmission of electricity seat is located at the brush
Disk side is fixedly connected with brush 233, and the brush is slidably connected with the brush；The charging wire other end passes through bottom plate simultaneously
It is electrically connected with the terminal pad.It is equipped at the corresponding reel for driving on the outside of side plate far from the brush side
State the second motor 222 of reel rotation.The length of the free end of the charging wire by second motor control it is described around
Spool rotation is controlled.Electric current is exported from power transmission line, successively by contact slide plate, electric receiving component is transferred to, through brush after
Charging wire is reached after being transferred to brush, finally reaches terminal pad.
The aircraft includes main part 51, and the main part includes the fan mounting portion 510 of tubular, is connected to
Fan mounting portion periphery and the connecting tube 512 for four equidistant arrangements being connected with fan mounting portion and it is connected to each company
It takes over outer end and what is be connected with corresponding position connecting tube goes out vane 511.
It is located in the fan mounting portion above connecting tube and is connected with upper bracket 5101, is equipped on the upper bracket
Driving fan 551；It is located in the fan mounting portion below connecting tube and is connected with lower carriage 5102, is installed on the lower carriage
There is lower driving fan 552；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install
The internal diameter of driving fan part is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade of upper driving fan
Diameter is more than the fan blade diameter of lower driving fan, and the fan mounting portion is interior between upper driving fan and lower driving fan
Wind pressure superatmospheric so that go out and wind pressure is formed in vane.
It is described go out vane include the vane upper shell 5111 of sealed connection and vane lower housing 5112, the vane lower casing
Internal Zhou Shangduan forms interior curved wall 51121, and there are one air outlet guard boards by the connection of multiple dowels for the inner circumferential of the interior curved wall
51123, air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；On being formed between the interior curved wall and air outlet guard board
Narrow outlet air gap under width, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing is located at outlet air
The lower section in gap is training wall 51124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface residing for the training wall is 20-30 degree.
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction
The angle of 5-20 degree is formed, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and the fan blade of upper driving fan
Rotation direction is opposite.
It is equipped with to adjust the adjusting part 56 that corresponding position goes out vane outlet air speed in each connecting tube, it is described
Adjusting part includes motor 561, the screw rod 562 coaxially connected with motor output shaft and the valve plate being connect with screw flight
563；For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；Institute
It states connecting tube internal upper part to form that the motor mounting plate 5121 of the motor is installed, the motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod 5122 being slidably connected with the valve plate；There are one upper end courts for lower part connection in the connecting tube
To the inclined baffle 5123 in vane direction is gone out, the conducting adjustable air passage of area is formed between the baffle and valve plate.
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board 57.
The main part upper end connects the air intake cover 54 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover
The air inlet of shape.
The main part is tightly connected for upper shell 51a and lower housing 51b and forms.
Aircraft provides driving force, upper driving fan production by upper driving fan, the lower driving fan in fan mounting portion
Raw fraction from it is each go out vane outlet air gap blow out downwards, and combine adjusting part adjustment each go out vane outlet air
Speed, so as to fulfill the horizontal flight or steering of aircraft, due to be located at aircraft periphery it is each go out vane only play tune
The effect of whole attitude of flight vehicle without the fan for being provided with power, goes out when vane generates touching with foreign object and does not easily lead to aircraft
Out of control or generate injury to human or animal, safety is good.
Further, it is described go out vane outlet air gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward together, flown in this way
When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly
The stabilization of row device flight attitude.
Further, it is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction and water of vane
The angle of 5-20 degree is formed square between, and the horizontal wind-force that generates of the wind for going out the outlet air gap blowout of vane and upper driving wind
The rotation direction of the fan blade of fan is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset
The reaction force that driving fan and lower driving fan generate when rotating；Also, change by adjusting each adjusting part simultaneously
Vane goes out wind velocity, it can be achieved that the whole forward or reverse of aircraft.Make one by adjusting one or two adjusting part
It is a or two go out vane go out wind velocity, it can be achieved that aircraft can drive aircraft in water in this way generally in heeling condition
Square to flight.
The lower, outer perimeter of the fan mounting portion is battery installation section 5103, is connected in battery installation section and control circuit
The accumulator 52 of plate electrical connection；The top for being located at battery installation section on the fan mounting portion is a circuit board installation cavity
5104, the control circuit board 57 is mounted in circuit board installation cavity, and there are one annulars for the circuit board installation cavity lower end connection
Cover board 513；The upper surface of the circuit board installation cavity uniformly forms the air inlet hole 5105 connected in fan mounting portion, institute
The lateral wall for stating circuit board installation cavity uniformly forms vent 5106；The lower driving fan lower end is equipped with and control circuit
The camera 5107 of plate electrical connection.
Go out position of the vane inner circumferential far from connecting tube described in each and form Holder joint 5110 of rising and falling, each undercarriage
Respectively there are one undercarriages 53 for connection on connector；The undercarriage includes the supporting rod 535 being fixedly connected with the Holder joint of rising and falling
And the first electromagnet 536 far from Holder joint one end of rising and falling on supporting rod is connected to, the supporting rod is downwards；Described
The second receiving electrode 5361 for charging to aircraft is installed below one electromagnet.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, and the control circuit board is risen
To cooling effect.
The electric vehicle upper end is equipped with charging board 31；The charging board upper end is equipped with the first receiving electrode 32；Institute
State charging board upper end be located at be fixedly connected on the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnetism
Iron 33.
The insulation tank 122 parked disk upper end and form annular；The disk upper end of parking is located on the outside of the insulation tank
Be fixedly connected with circumferentially be equally spaced have multiple permanent magnets 121.
The terminal pad is carried and is moved by the aircraft and charged to the electric vehicle.When the aircraft carries
During the terminal pad movement, the aircraft is connect with the terminal pad upper end；During the electric vehicle charging, the charging board
It is connect with the terminal pad lower end.
The terminal pad intermediary form has through-hole 45, and the through-hole diameter is more than the accumulator outer diameter；The terminal pad
Lower end, which corresponds to, is equipped with the first current electrode 42 at first receiving electrode；The take-up reel lower end is equipped with corresponding each institute
State the iron block 43 of the second electromagnet；Terminal pad upper end periphery is fixedly connected with the ring for being useful for being connect with terminal pad for aircraft
Shape iron block 41, corresponding first electromagnetism iron phase after diameter of a circle where the annular iron block center line is unfolded with the aircraft support bar
Circumscribed circle diameter where the rectangle being linked to be is equal；The annular iron block corresponds to is equipped with the second confession at second receiving electrode
Electrode 44.
The aircraft, trolley, electric vehicle are connected by wireless signal and the server communication of system.
The contact slide plate lower end is fixedly connected with the electrode wires 236 being electrically connected with the brush.
The end terrain clearance of trying to get to the heart of a matter of parking is 3.5-4m.
First current electrode, the second current electrode, the first receiving electrode, the second receiving electrode respectively include two
The annular electro polar ring being arranged concentrically.Installation on the position of brush is corresponded in the brush, and there are two the annular electrodes being arranged concentrically
Ring.
Speed limit 40km/h during the electric vehicle charging.
The present invention is installed along by road, and carrying terminal pad by aircraft moves, so as to make power transmission line and electric vehicle it
Between establish connection, and then to electric vehicle charge.When not having to carry out charging tasks, terminal pad, which is parked in, parks on disk, passes through
Iron block and permanent magnet is attracting that terminal pad is made to be connect with parking disk, first current electrode is plugged in the insulation tank, simultaneously
Iron block is attracting that aircraft is made connect with terminal pad with annular for first electromagnet of the aircraft under no aerial mission, second power it is electric
Pole connect to charge to aircraft with the second receiving electrode.When electric vehicle not enough power supply, electric automobile during traveling is extremely
Below guide rail, and the signal of charge request is sent to server, after server receives charge request signal, according to electronic vapour
The location of vehicle, and feed back electric vehicle and open below the trolley to remain static to direction of traffic front end, pass through simultaneously
The server nearest aircraft of the trolley of adjusting the distance sends instruction, and by being mounted on the camera of lower section, artificially control flies aircraft
The terminal pad upper end connected toward the trolley, the second electromagnet during the aircraft declines on the electric vehicle break
Electricity, iron block is attracting that aircraft is made to be connected with terminal pad with annular for each first electromagnet；Server controls trolley corresponding
The work of two motors extends charging wire while aircraft carrying terminal pad is controlled to be moved to above electric vehicle, at this time electric vehicle
On the second electromagnet be powered, control aircraft decline the first current electrode is made to be connect with the first receiving electrode, it is electronic so as to make
Automobile charges, and aircraft is then controlled to drive connection disc spins, makes the second electromagnetism on the iron block and charging board of terminal pad lower end
Iron phase is inhaled, so as to which terminal pad be made to be fixed on charging board；The first motor work of trolley is controlled in charging process, makes trolley with electricity
Electrical automobile is travelled and is moved；Carry-on first electromagnet is then controlled to power off, aircraft disengages with terminal pad and carries out other
Task.It is connected after aircraft being controlled to be moved to above electric vehicle after electric vehicle charges with terminal pad, electronic vapour
The second electromagnet power-off on vehicle, terminal pad are disconnected with charging board, and subsequent aircraft carrying terminal pad is connected to subsequent electronic
Charging or terminal pad is parked on automobile to parking on disk.When aircraft charges, sentenced by the camera below aircraft
Disconnected to be parked in the terminal pad parked on disk, control aircraft is moved to above the terminal pad, and then droping in the terminal pad makes
First electromagnet is attracting so as to be attached to aircraft with annular iron block, while the second current electrode and the second receiving electrode electricity
Connection, so as to charge to aircraft.
The present invention is arranged on by road, can in time be charged to electric vehicle on road, not by time restriction, and be driven
Sailing people can charge to electric vehicle while driving, and save driver and charge the time waited；Pass through trolley and power transmission line
It is connected and powers to electric vehicle, has more flexibility compared to charging pile, the place of charging is unfettered；Aircraft carries connection
Disk charges to electric vehicle, security risk when can avoid manual powered；When Rechargeable vehicle starts to charge up, aircraft and company
Disk is connect to disconnect, compared in the case of aircraft and terminal pad one can more rationally using aircraft and save into
This；It is described park disk be fixedly connected the terminal pad for, making not need on utility poles to charge to electric vehicle fix storage rather than
Suspension causes to generate hidden danger in the air；Terminal pad fixation is stored in when parking on disk, can be simultaneously to flying under off working state
Row device charges, and stores place to the offer of aircraft.
Embodiment 2
The present embodiment has done following improvement on the basis of embodiment 1：Go out position of the vane inner circumferential far from connecting tube described in each
Form Holder joint 5110 of rising and falling, respectively there are one undercarriages 53 for connection in each Holder joint of rising and falling；The undercarriage includes
Have and be fixedly connected with Holder joint of rising and falling and by Holder joint of rising and falling with going out the connection pipe body 531 being connected inside vane, slide peace
Sliding tube 532 in connection pipe body with connection pipe body close to the supporting rod 535 for Holder joint one end rotation connection of rising and falling, connects
Be connected on the first electromagnet 536 far from Holder joint one end of rising and falling on supporting rod and respectively in the middle part of sliding tube, in the middle part of supporting rod
The connecting rod 534 of rotation connection；The second receiving electrode 5361 for charging to aircraft is installed below first electromagnet.
The connection pipe body forms hinged seat 5311, described supporting rod one end and hinge close to the Holder joint one end wall that rises and falls
Joint chair is rotatablely connected；The sliding tube is connected with piston 5321, the slip pipe outer wall middle part position close to Holder joint one end of rising and falling
It puts and is connected with articulated joint 5322, described connecting rod one end is rotatablely connected with articulated joint, and the connection pipe body is far from Holder joint one of rising and falling
The side wall at end forms the strip shape gob 5312 passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling, which is fixed, to be connected
Sealing cap 533 is connected to, the inner end of sealing cap is connected with spring positioning bar 5331, spring is arranged on the spring positioning bar
537, the both ends of the spring is against respectively between piston and sealing cap inner end；It is formed on the supporting rod and packs up shape in supporting rod
The connecting rod tank 5351 of the connecting rod is accommodated during state.
The supporting rod is in unfolded state when the spring is in extended configuration, and the upper driving fan is in work shape
After state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The undercarriage is with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, goes out
Wind pressure in vane makes piston be moved together with sliding tube to sealing cap one end, so as to which sliding tube be made to drive connecting rod one end to sealing cap
Direction is moved, so as to which supporting rod lower end be made also to be rotated to sealing cap one end, so as to which undercarriage be made to be in collapsed state.Work as aircraft
During landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved together with piston toward hinged seat direction, so as to make sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, so as to which supporting rod lower end be made to turn to extreme position to hinged seat one end, so as to
Undercarriage is made to be in unfolded state.
The strip shape gob plays the role of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch
After length, supporting rod turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each supporting rod is equal
In stable state.Aircraft is carried in the moving process of terminal pad, since the first electromagnet and annular iron block are attracting, but outlet air
The power that wind pressure in ring generates is insufficient to allow supporting rod to pack up.
Claims (1)
1. a kind of charging system for electric automobile, it is characterised in that：Include and multiple be equidistantly vertically installed at by road along road
Electric pole is fixedly mounted on guide rail and the multiple trolleies being slidably connected on guide rail being located on electric pole above road；Institute
It states and power transmission line is installed below guide rail；The trolley is equipped with charging wire；The charging wire end is connected with for electronic vapour
The terminal pad of vehicle charging；Further include multiple aircraft for being used to carry terminal pad movement；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan installation
Portion periphery and the connecting tube for four equidistant arrangements being connected with fan mounting portion and be connected to each connecting tube outer end and with
What corresponding position connecting tube was connected goes out vane；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving wind is installed on the upper bracket
Fan；It is located in the fan mounting portion below connecting tube and is connected with lower carriage, lower driving fan is installed on the lower carriage；
The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion
Diameter is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, and the fan blade diameter of upper driving fan is more than lower driving wind
The fan blade diameter of fan, the interior wind pressure superatmospheric between upper driving fan and lower driving fan of the fan mounting portion,
Wind pressure is formed in vane so that going out；
It is described go out vane include the vane upper shell of sealed connection and vane lower housing, the vane lower housing inner circumferential upper end into
Type has interior curved wall, and there are one air outlet guard board, air outlet guard board upper end and wind by the connection of multiple dowels for the inner circumferential of the interior curved wall
Ring upper shell inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board
The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction and formed
The angle of 5-20 degree, and the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane generates
Direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting group in each connecting tube
Part includes motor, coaxially connected screw rod and the valve plate being connect with screw flight with motor output shaft；The valve plate top
Close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube for periphery；The connecting tube internal upper part 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；Upper end direction to go out the inclined baffle in vane direction there are one the connections of lower part in the connecting tube,
The conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly form on air intake cover strip into
Air port；
The main part is tightly connected and forms for upper shell and lower housing；
The lower, outer perimeter of the fan mounting portion is battery installation section, is connected in battery installation section and is electrically connected with control circuit board
Accumulator；Positioned at the top of battery installation section for a circuit board installation cavity on the fan mounting portion, the control circuit
Plate is mounted in circuit board installation cavity, and there are one the cover boards of annular for the circuit board installation cavity lower end connection；The circuit board peace
The upper surface behaveing affectedly uniformly forms the air inlet hole connected in fan mounting portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is equipped with the camera being electrically connected with control circuit board；
It is each it is described go out position of the vane inner circumferential far from connecting tube form Holder joint of rising and falling, it is each in each Holder joint of rising and falling
There are one undercarriages for connection；The undercarriage includes the supporting rod being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet far from Holder joint one end of rising and falling on bar, the supporting rod is downwards；It is installed below first electromagnet
It is useful for the second receiving electrode to charge to aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711428204.5A CN108128192A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488458.XA CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428204.5A CN108128192A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710488458.XA Division CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108128192A true CN108128192A (en) | 2018-06-08 |
Family
ID=60019577
Family Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711428204.5A Withdrawn CN108128192A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428494.3A Withdrawn CN108081997A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201710488458.XA Active CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428167.8A Withdrawn CN108081996A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Family Applications After (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711428494.3A Withdrawn CN108081997A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201710488458.XA Active CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428167.8A Withdrawn CN108081996A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Country Status (1)
| Country | Link |
|---|---|
| CN (4) | CN108128192A (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN110316005B (en) * | 2019-07-18 | 2020-12-18 | 温州新国余机械科技有限公司 | Low-temperature lithium battery charger bearing mechanism with electrostatic protection function |
| GB2583982B (en) | 2019-09-03 | 2021-11-03 | Hector Macdonald Benjamin | Cable support |
| CN110949134B (en) * | 2019-12-10 | 2021-07-16 | 深圳供电局有限公司 | Arc extinguishing type carbon brush electricity taking device |
| CN112224071A (en) * | 2020-10-13 | 2021-01-15 | 上海义阳新能源科技有限公司 | Movable fills electric pile based on direct current bus |
| WO2022095332A1 (en) * | 2020-11-05 | 2022-05-12 | 北星空间信息技术研究院(南京)有限公司 | Algorithm for variable angle at receiving terminal of wireless charging of unmanned aerial vehicle |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8839890B2 (en) * | 2009-05-26 | 2014-09-23 | Anthony Nicholas Caruso | Apparatus and system for low voltage direct current at industrial power recharging of hybrid high occupancy capacity on-road transportation vehicles |
| US10137800B2 (en) * | 2014-01-31 | 2018-11-27 | Honda Motor Co., Ltd. | Power feeding device and contact power feeding system |
| CN103935266B (en) * | 2014-04-08 | 2016-08-17 | 福州开发区和世林实业发展有限公司 | Driving electric supply installation |
| CN205944904U (en) * | 2016-08-18 | 2017-02-08 | 国网湖南省电力公司带电作业中心 | Cloth cable pulls component |
| CN106427591A (en) * | 2016-09-27 | 2017-02-22 | 高卫国 | Traffic system |
-
2017
- 2017-06-23 CN CN201711428204.5A patent/CN108128192A/en not_active Withdrawn
- 2017-06-23 CN CN201711428494.3A patent/CN108081997A/en not_active Withdrawn
- 2017-06-23 CN CN201710488458.XA patent/CN107244253B/en active Active
- 2017-06-23 CN CN201711428167.8A patent/CN108081996A/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| CN107244253A (en) | 2017-10-13 |
| CN108081996A (en) | 2018-05-29 |
| CN108081997A (en) | 2018-05-29 |
| CN107244253B (en) | 2018-07-03 |
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