CN107244253A - Charging system for electric automobile - Google Patents
Charging system for electric automobile Download PDFInfo
- Publication number
- CN107244253A CN107244253A CN201710488458.XA CN201710488458A CN107244253A CN 107244253 A CN107244253 A CN 107244253A CN 201710488458 A CN201710488458 A CN 201710488458A CN 107244253 A CN107244253 A CN 107244253A
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- CN
- China
- Prior art keywords
- fan
- vane
- charging
- fixedly connected
- aircraft
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
Abstract
The invention belongs to charging electric vehicle field, specifically related 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 dollies being slidably connected on guide rail, the terminal pad being connected with each dolly, is movably connected in the aircraft above terminal pad, and electric automobile of the traveling on road.The present invention is arranged on by road, can be on road to the timely charging of electric automobile, not by time restriction, and driver can save the time of driver's charging waiting while driving to charging electric vehicle；It is connected by dolly 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 system for electric automobile.
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：Filled in view of the deficienciess of the prior art, providing a kind of electric automobile
Electric system.
To realize the purpose of the present invention, it 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 dollies being slidably connected on guide rail；Power transmission line is installed below the guide rail；The dolly is provided with charging wire；
The charging wire end is fixedly connected with for the terminal pad to charging electric vehicle；Also include multiple for carrying terminal pad shifting
Dynamic aircraft.
Preferably：Each electric pole includes the vertical rod that vertical direction is set；The upper part of telegraph pole is fixed
It is connected with and parks disk towards what road direction was set；The vertical rod upper end is fixedly connected with towards the horizontally disposed horizontal stroke of road direction
Bar；The crossbar end is fixedly connected with the guide rail；The guide rail includes the symmetrical right angle guide rail of two horizontal directions；
The power transmission line is fixedly mounted on right angle guide rail lower end；The dolly includes dolly framework；The dolly 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 inners, which are rotated, to be connected
It is connected to multiple feeder wheels；It is fixedly connected with the outside of the side plate at each described feeder wheel of correspondence multiple for driving the advance
Take turns the first motor rotated；The dolly 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 in the middle of transmission of electricity seat is stated, the guide rod frame end is fixedly connected on and is led parallel to transmission of electricity the horizontal of seat
Bar；Along being provided with two contact slide plates below the horizontal guide rod upper end correspondence power transmission line, 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 provided 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 is fixed positioned at the brush side
Brush is connected with, the brush is slidably connected with the brush；The charging wire other end through bottom plate and with the terminal pad
Electrical connection；It is provided with the outside of side plate away from the brush side at the correspondence reel for driving the reel to rotate
The second motor；
The electric automobile upper end is provided with charging board；The charging board upper end is provided with the first receiving electrode；The charging board
Upper end be located at first receiving electrode on the outside of be fixedly connected with circumferentially be equally spaced have multiple second electromagnet；
It is described to park the insulation tank that disk upper end forms annular；The disk upper end of parking is fixedly connected on the outside of the insulation tank
There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through hole；The first confession is installed at the terminal pad lower end correspondence first receiving electrode
Electrode；The take-up reel lower end is provided with the iron block corresponding with the second electromagnet position each described；In the terminal pad
End periphery is fixedly connected with the annular iron block for being connected for aircraft with terminal pad；Be provided with the annular iron block with it is described
Corresponding second current electrode of second receiving electrode；
The aircraft, dolly, electric automobile are connected by wireless signal and the server communication of system；
The contact slide plate lower end is fixedly connected with the electrode wires electrically connected with the brush.
Preferably：The aircraft includes main part, and the fan that the main part includes tubular is installed
Portion, is connected to the connecting tube of fan installation portion periphery and four equidistant arrangements being connected with fan installation portion, and is connected to
Each connecting tube outer end and with correspondence position connecting tube is connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than the internal diameter that lower driving fan section is installed in fan installation portion, and the fan blade diameter of upper driving fan is more than lower driving wind
Blast superatmospheric in the fan blade diameter of fan, the fan installation portion between upper driving fan and lower driving fan,
Blast is formed in vane so that going out；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction formed
The angle of 5-20 degree, and go out the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
In the opposite direction；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes motor, the coaxially connected screw rod with motor output shaft, and the valve plate being connected with screw flight；The valve plate top
Periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube internal upper part into
Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane
The valve plate guide rod that plate is slidably connected；Bottom is connected with upper end towards going out the inclined baffle plate in vane direction in the connecting tube,
The conducting adjustable airway of area is formed between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected with control board respectively；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port；
The main part is that upper shell and lower house are tightly connected composition；
The lower, outer perimeter of the fan installation portion is to be connected with to electrically connect with control board in battery installation section, battery installation section
Battery；It is a circuit board installation cavity, the control circuit to be located at the top of battery installation section on the fan installation portion
Plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular cover plate；The circuit board peace
The upper surface behaveing affectedly uniformly forms the fresh air inlet connected with fan installation portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is provided with the camera electrically connected with control board；
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, it is each in Holder joint of rising and falling described in each
It is connected with a undercarriage；The undercarriage includes the support bar being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet away from Holder joint one end of rising and falling on bar, the support bar is downwards；Installed below first electromagnet
There is the second receiving electrode for being charged to aircraft.
Preferably：Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, each
A undercarriage is respectively connected with the Holder joint of rising and falling；The undercarriage, which includes, to be fixedly connected and passes through with Holder joint of rising and falling
The connection pipe body that Holder joint of rising and falling is connected with going out inside vane, is slidably mounted on the sliding tube in connection pipe body, with connecting tube
Body rotates the support bar of connection close to Holder joint one end of rising and falling, and is connected to the first electricity away from Holder joint one end of rising and falling on support bar
Magnet, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar；Use is installed below first electromagnet
In the second receiving electrode charged to aircraft；
The connection pipe body forms hinged seat close to Holder joint one end side wall that rises and falls, and described support bar one end is rotated with hinged seat
Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position, which is connected with, to be hinged
Head, described connecting rod one end rotates with articulated joint and is connected, and side wall of the connection pipe body away from Holder joint one end of rising and falling forms confession
The strip shape gob that articulated joint is passed through；The one end of the connection pipe body away from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap
The inner is connected with spring locating rod, the spring locating rod and is arranged with spring, and the both ends of the spring is against piston respectively
And between sealing cap is inner；The connecting rod tank that the connecting rod is accommodated in support bar collapsed state is formed on the support bar.
Preferably：The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out the axial direction of vane with
The angle of 5-20 degree is formed between horizontal direction, and goes out horizontal wind-force and upper driving that the wind of the air-out gap blowout of vane is produced
The rotation direction of the fan blade of fan is opposite.
Preferably：Diameter of a circle where the annular iron block center line is corresponding with after aircraft support bar expansion
Circumscribed circle diameter where the rectangle that first electromagnet is connected to is equal.
Preferably：First current electrode, the second current electrode, the first receiving electrode, the second receiving electrode
Respectively include two annular electro polar rings being arranged concentrically.Two are provided with the brush on the position of correspondence brush to set with one heart
The annular electro polar ring put.
Preferably：The end terrain clearance of trying to get to the heart of a matter of parking is 3.5-4m.
Preferably：Speed limit 40km/h during the charging electric vehicle.
Preferably：The through-hole diameter is more than the battery external diameter.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is installed along by road, is carried by aircraft
Terminal pad is moved, so that connection is set up between power transmission line and electric automobile, and then to charging electric vehicle.Filled when no
During electric task, terminal pad, which is parked in, parks on disk, terminal pad is connected with parking disk by the way that iron block and permanent magnet are attracting, and described
One current electrode is plugged in the insulation tank, while the first electromagnet without the aircraft under aerial mission and annular iron block phase
Suction makes aircraft be connected with terminal pad, and the second current electrode is connected to charge to aircraft with the second receiving electrode.When
During electric automobile not enough power supply, below electric automobile during traveling to guide rail, and the signal of charge request, service are sent to server
Device is received after charge request signal, according to the location of electric automobile, and feed back electric automobile open to direction of traffic most before
Hold below the dolly that remains static, while send and instruct by the server nearest aircraft of the dolly of adjusting the distance, flight
Device is flown to the terminal pad upper end that the dolly connected by the camera manual control installed in lower section, and the aircraft declined
The second electromagnet power-off described in journey on electric automobile, each first electromagnet with annular iron block is attracting makes aircraft with being connected
Disk is connected；The corresponding second motor work of server controls dolly makes charging wire elongation while controlling aircraft to carry terminal pad
It is moved to above electric automobile, now the second electromagnet on electric automobile is powered, control aircraft, which declines, makes the first power supply electricity
Pole is connected with the first receiving electrode, so that charging electric vehicle, then control aircraft, which drives, connects disc spins, makes terminal pad
The second electromagnet on the iron block and charging board of lower end is attracting, so that terminal pad is fixed on charging board；Controlled in charging process
The first motor work of dolly processed, makes dolly be moved with electric automobile during traveling；Then control carry-on first electromagnet
Power-off, aircraft disengages with terminal pad and carries out other tasks.Aircraft is controlled to be moved to after charging electric vehicle is finished electronic
It is connected after above automobile with terminal pad, the second electromagnet power-off on electric automobile, terminal pad disconnects with charging board, then flown
Row device carries terminal pad and is connected on follow-up electric automobile charging or parks terminal pad to parking on disk.When aircraft fills
When electric, judge to be parked in the terminal pad parked on disk by the camera 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 electrically connected with the second receiving electrode, so as to be charged to aircraft.
The present invention is arranged on by road, not by time restriction, and can be driven on road to the timely charging of electric automobile
The time of driver's charging waiting can be saved while driving to charging electric vehicle by sailing people；Pass through dolly and power transmission line
It is connected and electric automobile is powered, flexibility is had more compared to charging pile, the place of charging is unfettered；Aircraft carries connection
Disk is to charging electric vehicle, potential safety hazard when can avoid manual powered；When Rechargeable vehicle is started to charge up, aircraft and company
Connect disk to disconnect, compared to aircraft with more rationally using aircraft and can save into the case of terminal pad one
This；The disk of parking is fixedly connected on utility poles, makes that storage need not be fixed to the terminal pad of charging electric vehicle, rather than
Suspension causes to produce hidden danger in the air；Terminal pad, which is fixed, to be stored in when parking on disk, can be simultaneously to flying under off working state
Row device charges, and deposits place to the offer of aircraft.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of electric pole and guide rail.
Fig. 3 is the structural representation of electric automobile.
Fig. 4 is the structural representation of dolly.
Fig. 5, Fig. 6 are the cross section structure diagrams of dolly.
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, disk is parked；121st, permanent magnet；122nd, insulation tank；13rd, cross bar；2nd, dolly；21st, it is small
Car framework；211st, side plate；212nd, bottom plate；213rd, feeder wheel；2131st, the first motor；214th, roller；22nd, reel；221st, brush
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, connect
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 house；510th, fan installation portion；5101st, upper bracket；5102nd, lower branch
Frame；5103rd, battery installation section；5104th, circuit board installation cavity；5105th, fresh air inlet；5106th, vent；5107th, camera；511、
Go out vane；5110th, rise and fall Holder joint；5111st, vane upper shell；5112nd, vane lower house；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 plate；513rd, cover plate；52nd, battery；53rd, undercarriage；531st, connection pipe body；5311st, hinged seat；5312nd, strip shape gob；
532nd, sliding tube；5321st, piston；5322nd, articulated joint；533rd, sealing cap；5331st, spring locating rod；534th, connecting rod；535th, support
Bar；5351st, connecting rod tank；536th, the first electromagnet；5361st, the second receiving electrode；537th, spring；54th, air intake cover；551st, it is upper to drive
Dynamic fan；552nd, lower driving fan；56th, adjusting part；561st, motor；562nd, screw rod；563rd, valve plate；57th, control board；6、
Guide rail；61st, right angle guide rail；62nd, power transmission line.
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
Dolly 2 on guide rail；Power transmission line 62 is installed below the guide rail；The dolly is provided with charging wire 24；The charging wire end
End is fixedly connected with for the terminal pad 4 to charging electric vehicle；Also include multiple aircraft for being used to carry terminal pad movement
5。
Each electric pole includes the vertical rod 11 that vertical direction is set；The upper part of telegraph pole is fixedly connected with towards road
What direction was set parks disk 12；The vertical rod upper end is fixedly connected with towards the horizontally disposed cross bar 13 of road direction；The horizontal stroke
Boom end is fixedly connected with the guide rail.
The guide rail includes the 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 dolly includes dolly framework 21；The dolly framework includes the bottom plate 212 of horizontal direction, and two 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 being used to drive the feeder wheel to rotate are fixedly connected with the outside of the side plate at each described feeder wheel of correspondence
Machine 2131；The dolly is moved by the feeder wheel on the right angle guide rail；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 in the middle of transmission of electricity seat, is fixedly connected on the guide rod frame end and parallel to the horizontal stroke of the transmission of electricity seat
Guide rod 234；Edge is provided with two contact slide plates 235, the contact slide plate below the horizontal guide rod upper end correspondence power transmission line
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
Feeder wheel described in one motor control, which is rotated, makes the dolly 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 provided with reel 22；Described reel one end is fixedly connected with brush 221；Institute
State and charging wire 24 is wound with 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
Electrically connected with the terminal pad.It is provided with the outside of side plate away from the brush side at the correspondence reel for driving institute
State the second motor 222 of reel rotation.The length of the free end of the charging wire by described in second motor control around
Spool is rotated and is controlled.Electric current is exported from power transmission line, is sequentially passed through contact slide plate, is transferred to electric receiving component, through brush after
It is transferred to after brush and reaches charging wire, finally reaches terminal pad.
The aircraft includes main part 51, and the main part includes the fan installation portion 510 of tubular, is connected to
Fan installation portion periphery and the connecting tube 512 for four equidistant arrangements being connected with fan installation portion, and it is connected to each company
That takes over outer end and be connected with correspondence position connecting tube goes out vane 511.
It is located to be connected with upper bracket 5101, the upper bracket above connecting tube in the fan installation portion and is provided with
Drive fan 551；It is located to be connected with lower carriage 5102, the lower carriage below connecting tube in the fan installation portion and installs
There is lower driving fan 552；The upper driving fan is with the lower steering for driving fan on the contrary, and being installed in the fan installation portion
The internal diameter of fan section is driven to be more than the internal diameter for installing lower driving fan section in fan installation portion, and the fan blade of upper driving fan
Diameter is more than in the fan blade diameter of lower driving fan, the fan installation portion and is located between upper driving fan and lower driving fan
Blast superatmospheric so that go out and blast is formed in vane.
It is described go out vane include the vane upper shell 5111 and vane lower house 5112 being tightly connected, the vane lower casing
Internal Zhou Shangduan forms interior curved wall 51121, and the inner circumferential of the interior curved wall is connected with an air outlet guard board by multiple dowels
51123, air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；On being formed between the interior curved wall and air outlet guard board
Narrow air-out gap under width, the bottom width in air-out gap is 0.8-1.5mm；The inner circumferential of the vane lower house is located at air-out
The lower section in gap is training wall 51124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree.
It is described go out vane axial direction and the radial direction of fan installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction
The angle of 5-20 degree is formed, and goes out horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
Rotation direction is opposite.
It is provided with to adjust the adjusting part 56 that correspondence position goes out vane air-out speed in each described connecting tube, it is described
Adjusting part includes motor 561, the screw rod 562 coaxially connected with motor output shaft, and the valve plate being connected with screw flight
563；The valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；Institute
State connecting tube internal upper part to form that the motor mounting plate 5121 of the motor is installed, the motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod 5122 being slidably connected with the valve plate；Bottom is connected with a upper end court in the connecting tube
To the inclined baffle plate 5123 in vane direction is gone out, the conducting adjustable airway of area is formed between the baffle plate and valve plate.
The upper driving fan, lower driving fan and each motor are electrically connected with control board 57 respectively.
The main part upper end is connected with the air intake cover 54 of a semiellipse spherical shape, air intake cover and uniformly forms bar
The air inlet of shape.
The main part is that upper shell 51a and lower house 51b is tightly connected composition.
Aircraft provides driving force, upper driving fan production by the upper driving fan in fan installation portion, lower driving fan
Raw fraction is blown out downwards from each air-out gap for going out vane, and combines the air-out that adjusting part adjustment each goes out vane
Speed, so as to realize the horizontal flight or steering of aircraft, due to going out vane positioned at each of aircraft periphery and only play tune
The effect of whole attitude of flight vehicle, without the fan for being provided with power, goes out when vane produces touching with foreign object and is not easily caused aircraft
Out of control or produce injury to human or animal, security is good.
Further, it is described go out vane air-out gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward in the lump, so fly
When the part in air-out gap is stopped in row device flight course, the overall airflow influence that air-out gap is formed is small, is conducive to flying
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out axial direction and the level of vane
The angle of 5-20 degree is formed between direction, and goes out horizontal wind-force and upper driving fan that the wind of the air-out gap blowout of vane is produced
Fan blade rotation direction it is opposite.Pass through such design so that the wind energy for going out the air-out gap blowout of vane enough offsets drive
The reaction force produced when dynamic fan and the rotation of lower driving fan；Also, change air-out by adjusting each adjusting part simultaneously
Ring goes out wind velocity, and the overall forward or reverse of aircraft can be achieved.Make one by adjusting one or two adjusting part
Or two go out vane go out wind velocity, aircraft can be achieved generally in heeling condition, aircraft can be so driven in level
Fly in direction.
The lower, outer perimeter of the fan installation portion is to be connected with battery installation section 5103, battery installation section and control circuit
The battery 52 of plate electrical connection；It is a circuit board installation cavity to be located at the top of battery installation section on the fan installation portion
5104, the control board 57 is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular
Cover plate 513；The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet 5105 connected with fan installation portion, institute
The lateral wall for stating circuit board installation cavity uniformly forms vent 5106；The lower driving fan lower end is provided with and control circuit
The camera 5107 of plate electrical connection.
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint 5110 of rising and falling, each described undercarriage
A undercarriage 53 is respectively connected with joint；The undercarriage includes the support bar 535 being fixedly connected with the Holder joint of rising and falling
And the first electromagnet 536 away from Holder joint one end of rising and falling on support bar is connected to, the support bar is downwards；Described
The second receiving electrode 5361 for being charged to aircraft is installed below one electromagnet.
A small amount of air-flow of the fan installation portion enters from fresh air inlet and from vent discharge, the control board is risen
To thermolysis.
The electric automobile upper end is provided with charging board 31；The charging board upper end is provided with the first receiving electrode 32；Institute
State charging board upper end be fixedly connected with the outside of first receiving electrode be circumferentially equally spaced have multiple second electromagnetism
Iron 33.
It is described to park the insulation tank 122 that disk upper end forms annular；The disk upper end of parking is on the outside of the insulation tank
Be fixedly connected with circumferentially be equally spaced have multiple permanent magnets 121.
The terminal pad is carried by the aircraft and moved to the charging electric vehicle.When the aircraft is carried
During the terminal pad movement, the aircraft is connected with the terminal pad upper end；During the charging electric vehicle, the charging board
It is connected with the terminal pad lower end.
The terminal pad intermediary form has through hole 45, and the through-hole diameter is more than the battery external diameter；The terminal pad
The first current electrode 42 is installed at lower end correspondence first receiving electrode；The take-up reel lower end is provided with each institute of correspondence
State the iron block 43 of the second electromagnet；Terminal pad upper end periphery is fixedly connected with the ring for being connected for aircraft with terminal pad
Shape iron block 41, diameter of a circle where the annular iron block center line and corresponding first electromagnetism iron phase after aircraft support bar expansion
Circumscribed circle diameter where the rectangle being linked to be is equal；The second confession is installed at the annular iron block correspondence second receiving electrode
Electrode 44.
The aircraft, dolly, electric automobile 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 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.Two annular electrodes being arranged concentrically are installed on the position of correspondence brush in the brush
Ring.
Speed limit 40km/h during the charging electric vehicle.
The present invention is installed along by road, and carrying terminal pad by aircraft moves so that power transmission line and electric automobile it
Between set up connection, and then to charging electric vehicle.When no progress charging tasks, terminal pad, which is parked in, parks on disk, passes through
Iron block and permanent magnet is attracting makes terminal pad be connected with parking disk, first current electrode is plugged in the insulation tank, simultaneously
Iron block is attracting aircraft be connected with terminal pad for the first electromagnet without the aircraft under aerial mission and annular, second power it is electric
Pole is connected to charge to aircraft with the second receiving electrode.When electric automobile not enough power supply, electric automobile during traveling is extremely
Below guide rail, and the signal of charge request is sent to server, server is received after charge request signal, according to electronic vapour
The location of car, and feed back electric automobile and open to direction of traffic below the dolly remained static foremost, pass through simultaneously
The server nearest aircraft of the dolly of adjusting the distance sends instruction, and aircraft is flown by the camera manual control installed in lower section
The terminal pad upper end connected toward the dolly, the second electromagnet during the aircraft declines on the electric automobile breaks
Electricity, iron block is attracting aircraft is connected with terminal pad with annular for each first electromagnet；Server controls dolly corresponding
The work of two motors makes charging wire elongation and is moved to while controlling aircraft to carry terminal pad above electric automobile, now electric automobile
On the second electromagnet be powered, control aircraft decline the first current electrode is connected with the first receiving electrode so that electronic
Automobile charges, and then control aircraft drives connection disc spins, makes the second electromagnetism on the iron block and charging board of terminal pad lower end
Iron phase is inhaled, so that terminal pad is fixed on charging board；The first motor work of dolly is controlled in charging process, makes dolly with electricity
Electrical automobile is travelled and moved；Carry-on first electromagnet is then controlled to power off, aircraft disengages with terminal pad and carries out other
Task.Aircraft is controlled to be connected after being moved to above electric automobile with terminal pad after charging electric vehicle is finished, electronic vapour
The second electromagnet power-off on car, terminal pad and charging board disconnect, subsequent aircraft carry terminal pad be connected to it is follow-up 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 be charged to aircraft.
The present invention is arranged on by road, not by time restriction, and can be driven on road to the timely charging of electric automobile
The time of driver's charging waiting can be saved while driving to charging electric vehicle by sailing people；Pass through dolly and power transmission line
It is connected and electric automobile is powered, flexibility is had more compared to charging pile, the place of charging is unfettered；Aircraft carries connection
Disk is to charging electric vehicle, potential safety hazard when can avoid manual powered；When Rechargeable vehicle is started to charge up, aircraft and company
Connect disk to disconnect, compared to aircraft with more rationally using aircraft and can save into the case of terminal pad one
This；The disk of parking is fixedly connected on utility poles, makes that storage need not be fixed to the terminal pad of charging electric vehicle, rather than
Suspension causes to produce hidden danger in the air；Terminal pad, which is fixed, to be stored in when parking on disk, can be simultaneously to flying under off working state
Row device charges, and deposits 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 away from connecting tube described in each
Holder joint 5110 of rising and falling is formed, a undercarriage 53 is respectively connected with Holder joint of rising and falling described in each；The undercarriage includes
There is the connection pipe body 531 for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling, slide peace
Sliding tube 532 in connection pipe body, rotates the support bar 535 being connected, even with connection pipe body close to Holder joint one end of rising and falling
Be connected on support bar away from first electromagnet 536 of Holder joint one end of rising and falling, and respectively with the middle part of sliding tube, in the middle part of support bar
Rotate the connecting rod 534 of connection；The second receiving electrode 5361 for being charged to aircraft is installed below first electromagnet.
The connection pipe body forms hinged seat 5311, described support bar one end and hinge close to Holder joint one end side wall that rises and falls
Joint chair rotates connection；The sliding tube is connected with position in the middle part of piston 5321, the slip pipe outer wall close to Holder joint one end of rising and falling
Put and be connected with articulated joint 5322, described connecting rod one end rotates with articulated joint and is connected, the connection pipe body is away from Holder joint one of rising and falling
The side wall at end forms the strip shape gob 5312 passed through for articulated joint；The one end of the connection pipe body away from Holder joint of rising and falling, which is fixed, to be connected
Sealing cap 533 is connected to, the inner of sealing cap, which is connected with spring locating rod 5331, the spring locating rod, is arranged with spring
537, the both ends of the spring is against between piston and sealing cap the inner respectively；Formed on the support bar and pack up shape in support bar
The connecting rod tank 5351 of the connecting rod is accommodated during state.
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in work shape
After state, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
The undercarriage is packed up or deployed as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out
Blast in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drivening rod one end is to sealing cap
Direction is moved, so that support bar lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft
During landing, the blast gone out in vane reduces, and Spring driving sliding tube is moved together with piston toward hinged seat direction, so that sliding tube
Drivening rod one end is moved to hinged seat direction, so that support bar lower end turns to extreme position to hinged seat one end, so that
Undercarriage is set to be in deployed condition.
The strip shape gob plays a part of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch
After length, support bar turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each support bar is equal
In stable state.Aircraft is carried in the moving process of terminal pad, because the first electromagnet and annular iron block are attracting, but air-out
The power that blast in ring is produced is insufficient to allow support bar to pack up.
Claims (10)
1. a kind of charging system for electric automobile, it is characterised in that：Include and multiple be equidistantly vertically installed at along road by road
Electric pole, is fixedly mounted on the guide rail and multiple dollies being slidably connected on guide rail being located on electric pole above road；Institute
State and power transmission line is installed below guide rail；The dolly is provided with charging wire；The charging wire end is connected with for electronic vapour
The terminal pad of car charging；Also include multiple aircraft for being used to carry terminal pad movement.
2. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：It is vertical that each electric pole includes
The vertical rod that direction is set；The upper part of telegraph pole is fixedly connected with and parks disk towards what road direction was set；The vertical rod upper end is consolidated
Surely it is connected with towards the horizontally disposed cross bar of road direction；The crossbar end is fixedly connected with the guide rail；
The guide rail includes the symmetrical right angle guide rail of two horizontal directions；The power transmission line is fixedly mounted under right angle guide rail
End；
The dolly includes dolly framework；The dolly framework includes the bottom plate of horizontal direction, and two are fixedly connected vertically
Side plate in bottom plate upper end both sides；Two side plate upper inners are rotatably connected to multiple feeder wheels；It is right on the outside of the side plate
Answer and multiple the first motors for being used to drive the feeder wheel to rotate are fixedly connected with each described feeder wheel；The dolly passes through
The feeder wheel is moved on the right angle guide rail；Mutually it is butted on the side plate relative to being rotatably connected at the right angle guide rail
Roller on the outside of the right angle guide rail；The bottom plate upper end is fixedly connected with electric receiving component；The electric receiving component includes fixed connect
Transmission of electricity seat of the bottom plate perpendicular to the side plate is connected on, the guide rod frame of direction upward in the middle of the transmission of electricity seat is fixedly connected on,
It is fixedly connected on the guide rod frame end and parallel to the horizontal guide rod of the transmission of electricity seat；The horizontal guide rod upper end correspondence transmission of electricity
Along two contact slide plates are provided with below line, the contact slide plate is slidably connected with the power transmission line；The contact slide plate and institute
State and be fixedly connected with compression spring between horizontal guide rod；
Two side plate lower rotationals are provided 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 is fixed positioned at the brush side
Brush is connected with, the brush is slidably connected with the brush；The charging wire other end through bottom plate and with the terminal pad
Electrical connection；It is provided with the outside of side plate away from the brush side at the correspondence reel for driving the reel to rotate
The second motor；
The electric automobile upper end is provided with charging board；The charging board upper end is provided with the first receiving electrode；The charging board
Upper end be located at first receiving electrode on the outside of be fixedly connected with circumferentially be equally spaced have multiple second electromagnet；
It is described to park the insulation tank that disk upper end forms annular；The disk upper end of parking is fixedly connected on the outside of the insulation tank
There is what is be circumferentially equally spaced there are multiple permanent magnets；
The terminal pad intermediary form has through hole；The first confession is installed at the terminal pad lower end correspondence first receiving electrode
Electrode；The take-up reel lower end is provided with the iron block corresponding with the second electromagnet position each described；In the terminal pad
End periphery is fixedly connected with the annular iron block for being connected for aircraft with terminal pad；Be provided with the annular iron block with it is described
Corresponding second current electrode of second receiving electrode；
The aircraft, dolly, electric automobile are connected by wireless signal and the server communication of system；
The contact slide plate lower end is fixedly connected with the electrode wires electrically connected with the brush.
3. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：The aircraft includes main body
Portion, the main part includes the fan installation portion of tubular, is connected to fan installation portion periphery and is connected with fan installation portion
The connecting tube of four logical equidistant arrangements, and be connected to each connecting tube outer end and with going out that correspondence position connecting tube is connected
Vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than the internal diameter that lower driving fan section is installed in fan installation portion, and the fan blade diameter of upper driving fan is more than lower driving wind
Blast superatmospheric in the fan blade diameter of fan, the fan installation portion between upper driving fan and lower driving fan,
Blast is formed in vane so that going out；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan installation portion it is perpendicular, and go out between the axial direction of vane and horizontal direction formed
The angle of 5-20 degree, and go out the rotation of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
In the opposite direction；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes motor, the coaxially connected screw rod with motor output shaft, and the valve plate being connected with screw flight；The valve plate top
Periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube internal upper part into
Type has the motor mounting plate for installing the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane
The valve plate guide rod that plate is slidably connected；Bottom is connected with upper end towards going out the inclined baffle plate in vane direction in the connecting tube,
The conducting adjustable airway of area is formed between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected with control board respectively；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port；
The main part is that upper shell and lower house are tightly connected composition；
The lower, outer perimeter of the fan installation portion is to be connected with to electrically connect with control board in battery installation section, battery installation section
Battery；It is a circuit board installation cavity, the control circuit to be located at the top of battery installation section on the fan installation portion
Plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular cover plate；The circuit board peace
The upper surface behaveing affectedly uniformly forms the fresh air inlet connected with fan installation portion, and the lateral wall of the circuit board installation cavity is uniform
Form vent；The lower driving fan lower end is provided with the camera electrically connected with control board；
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, it is each in Holder joint of rising and falling described in each
It is connected with a undercarriage；The undercarriage includes the support bar being fixedly connected with the Holder joint of rising and falling and is connected to support
The first electromagnet away from Holder joint one end of rising and falling on bar, the support bar is downwards；Installed below first electromagnet
There is the second receiving electrode for being charged to aircraft.
4. a kind of charging system for electric automobile as claimed in claim 3, it is characterised in that：Go out vane inner circumferential described in each remote
The position of connecting tube forms Holder joint of rising and falling, and a undercarriage is respectively connected with Holder joint of rising and falling described in each；It is described to rise and fall
Frame includes the connection pipe body for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling, and slides
Sliding tube in connection pipe body, rotates the support bar being connected close to Holder joint one end of rising and falling with connection pipe body, is connected to
Away from first electromagnet of Holder joint one end of rising and falling on support bar, and respectively with the company of rotation in the middle part of sliding tube, in the middle part of support bar
The connecting rod connect；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 as claimed in claim 3, it is characterised in that：Pacify with fan the axial direction of the vane
The radial direction in dress portion is perpendicular, and goes out between the axial direction of vane and horizontal direction to be formed the angle of 5-20 degree, and goes out the air-out of vane
The horizontal wind-force that the wind of gap blowout is produced is opposite with the rotation direction of the fan blade of upper driving fan.
6. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：Circle where the annular iron block center line
Diameter and the aircraft support bar deploy after circumscribed circle diameter where the rectangle that is connected to of corresponding first electromagnet it is equal.
7. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：First current electrode, second
Current electrode, the first receiving electrode, the second receiving electrode respectively include two annular electro polar rings being arranged concentrically；
Two annular electro being arranged concentrically polar rings are installed on the position of correspondence brush in the brush.
8. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：It is described to park end terrain clearance of trying to get to the heart of a matter
For 3.5-4m.
9. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：The speed limit during charging electric vehicle
40km/h。
10. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：The through-hole diameter is more than described
Battery external diameter.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488458.XA CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428167.8A CN108081996A (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 |
| CN201711428494.3A CN108081997A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710488458.XA CN107244253B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Related Child Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711428494.3A Division CN108081997A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428167.8A Division CN108081996A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201711428204.5A Division CN108128192A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107244253A true CN107244253A (en) | 2017-10-13 |
| CN107244253B CN107244253B (en) | 2018-07-03 |
Family
ID=60019577
Family Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| 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 |
| 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 |
Family Applications After (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711428167.8A Withdrawn CN108081996A (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| 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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (4) | CN107244253B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN114407688A (en) * | 2020-11-05 | 2022-04-29 | 北星空间信息技术研究院(南京)有限公司 | Wireless charging receiving end included angle-variable unmanned aerial vehicle and use method |
Families Citing this family (3)
| 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 |
| 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 |
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| US20100300780A1 (en) * | 2009-05-26 | 2010-12-02 | Anthony Nicholas Caruso | Apparatus and system for low voltage direct current at industrial power recharging of hybrid high occupany capacity on-road transporation vehicles |
| CN103935266A (en) * | 2014-04-08 | 2014-07-23 | 杨有岳 | Traveling vehicle power supply device |
| EP3100900A1 (en) * | 2014-01-31 | 2016-12-07 | Honda Motor Co., Ltd. | Power feeding device and contact power feeding system |
| CN205944904U (en) * | 2016-08-18 | 2017-02-08 | 国网湖南省电力公司带电作业中心 | Cloth cable pulls component |
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- 2017-06-23 CN CN201710488458.XA patent/CN107244253B/en active Active
- 2017-06-23 CN CN201711428167.8A patent/CN108081996A/en not_active Withdrawn
- 2017-06-23 CN CN201711428204.5A patent/CN108128192A/en not_active Withdrawn
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| US20100300780A1 (en) * | 2009-05-26 | 2010-12-02 | Anthony Nicholas Caruso | Apparatus and system for low voltage direct current at industrial power recharging of hybrid high occupany capacity on-road transporation vehicles |
| EP3100900A1 (en) * | 2014-01-31 | 2016-12-07 | Honda Motor Co., Ltd. | Power feeding device and contact power feeding system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN114407688A (en) * | 2020-11-05 | 2022-04-29 | 北星空间信息技术研究院(南京)有限公司 | Wireless charging receiving end included angle-variable unmanned aerial vehicle and use method |
| CN114407688B (en) * | 2020-11-05 | 2024-04-12 | 北星空间信息技术研究院(南京)有限公司 | Unmanned aerial vehicle with variable included angle of wireless charging receiving end and using method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107244253B (en) | 2018-07-03 |
| CN108128192A (en) | 2018-06-08 |
| CN108081996A (en) | 2018-05-29 |
| CN108081997A (en) | 2018-05-29 |
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Effective date of registration: 20211116 Address after: 266071 No. 3 Heze Road, Shinan District, Qingdao, Shandong Patentee after: Yu Qing Address before: 325000 building 3, block a, No. 329, Jinhai Third Road, economic and Technological Development Zone, Wenzhou City, Zhejiang Province Patentee before: Wenzhou ruichu Technology Co., Ltd |