CN108688516A - A kind of electric vehicle power supply system - Google Patents
A kind of electric vehicle power supply system Download PDFInfo
- Publication number
- CN108688516A CN108688516A CN201810517625.3A CN201810517625A CN108688516A CN 108688516 A CN108688516 A CN 108688516A CN 201810517625 A CN201810517625 A CN 201810517625A CN 108688516 A CN108688516 A CN 108688516A
- Authority
- CN
- China
- Prior art keywords
- guide rail
- vane
- fan
- motor
- electric vehicle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60M—POWER SUPPLY LINES, AND DEVICES ALONG RAILS, FOR ELECTRICALLY- PROPELLED VEHICLES
- B60M1/00—Power supply lines for contact with collector on vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60M—POWER SUPPLY LINES, AND DEVICES ALONG RAILS, FOR ELECTRICALLY- PROPELLED VEHICLES
- B60M7/00—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land 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
- B60L2240/00—Control parameters of input or output; Target parameters
- B60L2240/70—Interactions with external data bases, e.g. traffic centres
-
- 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
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Power Engineering (AREA)
- Toys (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a kind of electric vehicle power supply systems, include the multiple power transmission rods for being fixedly mounted on both sides of the road, transmission guide rail between each power transmission rod, the guide rail car for rolling or being slidably mounted on the transmission guide rail and be electrically connected with transmission guide rail, the aircraft that can be rested on electric vehicle and be electrically connected with electric vehicle, and be connected between guide rail car and aircraft electric energy to be transferred to the conducting wire on electric vehicle from transmission guide rail.Electric vehicle is realized without stopping the function that can be charged, and coordinates guide rail car to realize by aircraft and the electric energy on transmission guide rail is transferred on electric vehicle, in this way electric vehicle in the case that it is fully charged or it is other can at any time with aircraft be detached from, freely travelling for electric vehicle will not be caused to limit.
Description
Technical field
The invention belongs to electric vehicle corollary system fields, and in particular to a kind of electric vehicle power supply system.
Background technology
With popularizing for electric vehicle, the inconvenient problem of electric vehicle charging also increasingly highlights;Purchase electric vehicle at present
User be typically limited to only city use on and off duty, need for a long time at a distance outgoing user then still tend to use fuel oil
Vehicle.Even and city short distance traveling, user are also required to pay attention to very much the remaining capacity of electric vehicle, are otherwise susceptible on the way
The case where no electricity casts anchor.And what similar two-wheeled battery truck was taken is arranged the scheme of charging equipment in roadside, for electric vehicle
Speech is not just most suitable, and the floor space of one side electric vehicle is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills
Electricity may cause traffic congestion, and on the other hand, electric vehicle power consumption also many bigger than the battery truck of two-wheeled charges in current battery
In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
Invention content
The technical problem to be solved by the present invention is to:In view of the deficienciess of the prior art, a kind of charging of offer is convenient, and
The electric vehicle power supply system of user hours underway is not delayed.
Purpose to realize the present invention, is achieved using following technical scheme:A kind of electric vehicle power supply system, including
There are the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail being mounted between each power transmission rod, rolls or sliding is pacified
The guide rail car being electrically connected on the transmission guide rail and with transmission guide rail, can rest on electric vehicle and and electric vehicle
The aircraft of electrical connection, and be connected between guide rail car and aircraft electric energy is transferred to electronic vapour from transmission guide rail
Conducting wire on vehicle.
Preferably:Two groups are at least connected between two groups of transmission guide rails of both sides of the road to change for guide rail car
To commutation guide rail;
The transmission guide rail, commutation guide rail have respectively included two tracks disposed in parallel, there are one each track includes at least
For guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part between two tracks
It is oppositely arranged.
Preferably:The guide rail car includes upper sweep, and is fixedly connected on the lower sweep below sweep;
The upper sweep upper left side front and rear portions are fixedly mounted there are two first motor, and the upper upper right side front and rear portions of sweep are equipped with two
A the second motor that can be moved along guide rail car left and right directions;The first motor, the second motor lower end have been respectively fixedly connected with
The driving wheel of connection is rolled with both sides transmission guide rail;
Sweep left and right directions forms the bar shaped perforation slided for the second motor in the upper sweep upper edge;Pacify on the upper sweep
Equipped with driving the second motor close to the pushing meanss of transmission guide rail;
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at sliding
In seat and horizontally disposed sliding bar, and it is set in the socket being fixedly connected on the outside of the second motor and with two sliding bar one end
Part;Compressed spring is installed between the sliding bar and sliding seat;
The lower sweep both sides are rotatably connected to by shaft and roll the idler wheel that be electrically connected with transmission guide rail so that the shaft and
The transmission guide rail of homonymy is electrically connected.
Preferably:Guide rail car bottom surface intermediary form has mounting base, the mounting base lower part to form coiling
Disk mounting groove, the wire spool mounting groove intermediary form have shaft, wire spool are rotatably connected in the shaft;
Be provided in an axial direction in the shaft of non-conducting material two electrodes a, two electrode a respectively with lower sweep both sides turn
Axis is electrically connected;The wire spool intermediary form has roll;The roll intermediary form has shaft interface, the wire spool
It is set on the outside of shaft by the rotation of shaft interface;It is provided on the shaft interface inner wall and is slided respectively with two electrode a
Two electrode b of dynamic electrical connection;The Wire-wound is in the wire spool, and one end of conducting wire and two electrode b electricity
Connection;
4th motor is installed in the mounting base;Output axis connection with the 4th motor is installed in the wire spool mounting groove
Driving gear;The driven internal gear with driving gear engaged transmission is formed on the wire spool;
The wire spool installation groove sidewall forms the retractable cable mouth passed through for conducting wire.
Preferably:The aircraft includes main part, and the main part includes the fan installation of tubular
Portion, the connecting tube of four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion, and be 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 bracket, lower driving fan is installed on the lower bracket;
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 the interior installation of fan mounting portion, is located at upper driving fan under in the fan mounting portion
Wind pressure superatmospheric between driving fan so that go out and form wind pressure in vane;
It is described go out vane include sealed connection vane upper shell and vane lower housing, the vane lower housing inner circumferential upper end at
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 is 20-30 degree;
The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out and form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of the horizontal wind-force and the fan blade of upper driving fan of the wind generation of the outlet air gap blowout of vane
To 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 third motor, the coaxially connected screw rod with third motor output shaft, and the valve plate being connect with screw flight;It is described
For 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;The connecting tube
Internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate;There are one upper end directions to go out for lower part connection in the connecting tube
The inclined baffle in vane direction forms the conducting adjustable air passage of area between the baffle and valve plate;
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively;
The main part is that upper shell and lower housing are tightly connected and constitute;
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly formed on air intake cover strip into
Air port.
Preferably:First electromagnet, first electromagnet are installed at the top of the air intake cover of the aircraft
Top camera is installed;
The upper camera and the first electromagnet are electrically connected with control circuit board respectively;
Wire spool mounting groove lower end is fixedly connected with the second cover board;Second cover board lower end forms cross positioning mark
Note;The position that second cover board lower end corresponds to telltale mark is connected with the permanent magnet sucked by magnetic force with the first electromagnet.
Preferably:The lower, outer perimeter of the fan mounting portion is charging transmitting module mounting portion, charging transmitting mould
The charging transmitting module being electrically connected with control circuit board is connected on block mounting portion;
The lower bracket bottom of the aircraft is equipped with lower camera, and the lower camera is electrically connected with control circuit board;
The electromobile at top is equipped with the charging receiving module being electrically connected with charging transmitting module.
Preferably:Go out position of the vane inner circumferential far from connecting tube described in each and forms 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 includes to be fixedly connected and pass through with Holder joint of rising and falling
Holder joint of rising and falling with go 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 on supporting rod far from Holder joint one end of rising and falling close to the supporting rod for Holder joint one end rotation connection of rising and falling inhaling
Tightly in the second electromagnet of electromobile at top, and the connecting rod with rotation connection in the middle part of sliding tube middle part, supporting rod respectively;
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 sliding 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;
The spring is in supporting rod when extended configuration and is in unfolded state, and the upper driving fan is in running order
Afterwards, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
Preferably:The top for being located at charging transmitting module mounting portion on the fan mounting portion is a circuit board
Installation cavity, the control circuit board are mounted in circuit board installation cavity, and there are one annulars for the connection of circuit board installation cavity lower end
The first cover board;The upper surface of the circuit board installation cavity uniformly forms the air inlet hole being connected to in fan mounting portion, described
The lateral wall of circuit board installation cavity uniformly forms vent.
Compared with prior art, the beneficial effects of the invention are as follows:The present invention on transmission guide rail by travelling and keeping
The guide rail car of travel speed identical with electric vehicle coordinates the aircraft being connect with guide rail car conducting wire to be electronic in traveling
Automobile charges, and realizes electric vehicle and coordinates guide rail car to realize without stopping the function that can be charged, and by aircraft
Electric energy on transmission guide rail is transferred on electric vehicle, such electric vehicle in the case that it is fully charged or it is other can be at any time
It is detached from aircraft, freely travelling for electric vehicle will not be caused to limit.The electronic of pantograph is set in roof with existing
Bus is compared, and only a charging receiving module need to be arranged in electromobile at top in the present invention(Such as the contact that the prior art is common
The electrode or wireless charging receiving module that formula electrically connects), the not too large appearance for influencing electric vehicle, and convenient for existing electricity
Electrical automobile is transformed.
Since the quantity of electric vehicle and travel direction that charge on each section of road are random, therefore
It needs to connect at least two groups commutation guide rail between two transmission guide rails of both sides of the road, in order to which guide rail car is from road side
Transmission guide rail is moved on the transmission guide rail of the other side.
Further, since in commutation guide rail and transmission guide rail junction and transmission guide rail, in road, there are corners
Certainly exist non-directional track(It is general as arc-shaped in being designed as in Fig. 1), therefore the second design of electrical motor of side is on guide rail car
It can be moved along guide rail car left and right directions so that when driving into arc-shaped track the driving wheel of both sides can keep guide rail car
It offsets with the holding of two siding tracks.
The aircraft passes through the first electromagnet in off working state(Iron core)It sucks below the second cover board forever
On magnet, when aircraft works, the first electromagnet is powered to generating keeps aircraft and the second cover board de- with the reversed magnetic field of permanent magnet
From.
When there is electric vehicle to need charging, the 4th motor drives wire spool rotation to release conducting wire, while aircraft is detached from
Guide rail car is simultaneously flown on electric vehicle, and aircraft sucks the gold in electromobile at top by the second electromagnet of undercarriage lower end
Belong on vehicle shell.
The aircraft provides driving force, the part that upper driving fan generates by the upper driving fan in fan mounting portion
Air-flow from it is each go out vane outlet air gap downwards blow out, and combine adjusting part adjustment each to go out vane and go out wind velocity, from
And realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only play adjustment aircraft
The effect of posture, without the fan for being provided with power, go out not easily leading to when vane generates touching with foreign object aircraft it is out of control or
Injury is generated to human or animal, safety is good.Similar to four-axle aircraft, four go out vane and only play adjusting appearance the aircraft appearance
The function of state, therefore the present invention substantially should be uniaxial aircraft.
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, the axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out the axial direction and level of vane
The horizontal wind-force and upper driving fan that the wind for forming the angle of 5-20 degree between direction, and going out the outlet air gap blowout of vane generates
Fan blade rotation direction it is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset and driven
The reaction force that dynamic fan or upper driving fan and lower driving fan generate when rotating;Also, by adjusting each adjusting simultaneously
Component change vane go out wind velocity, it can be achieved that aircraft whole forward or reverse.It is adjusted by adjusting one or two
Section component makes what one or two went out vane to go out wind velocity, it can be achieved that aircraft can be driven in this way generally in heeling condition
Aircraft flies in the horizontal direction.
The undercarriage with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, go out
Wind pressure in vane makes piston be moved to sealing cap one end together with sliding tube, to make sliding tube drive connecting rod one end to sealing cap
Direction is moved, to make supporting rod lower end also be rotated to sealing cap one end, to make undercarriage be in collapsed state.Work as aircraft
When landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved toward hinged seat direction together with piston, to make sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, to make supporting rod lower end turn to extreme position to hinged seat one end, to
Undercarriage is set 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 makes spring 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.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention.
Fig. 2, Fig. 3 are the structural schematic diagrams of aircraft and guide rail car.
Fig. 4, Fig. 5 are the structural schematic diagrams of guide rail car.
Fig. 6 is the explosive view of guide rail car.
Fig. 7 is the structural schematic diagram of lower sweep and each component on lower sweep.
Fig. 8 is the structural schematic diagram of wire spool.
Fig. 9 is the structural schematic diagram of aircraft shutdown status.
Figure 10 is the structural schematic diagram of aircraft flight state.
Figure 11 is the schematic cross-sectional view of aircraft.
Figure 12 is the portions the A schematic enlarged-scale view of Figure 11.
Figure 13 is the portions the B schematic enlarged-scale view of Figure 11.
The structural schematic diagram of each component that Figure 14 is upper shell and is connect with upper shell.
Figure 15 is the structural schematic diagram of lower housing section.
Figure 16 is the schematic cross-sectional view of lower housing section.
Figure 17 is the structural schematic diagram of air intake cover.
Figure 18 is the decomposition texture schematic diagram of undercarriage part.
Figure 19 is the schematic cross-sectional view of undercarriage part.
1, power transmission rod;2, transmission guide rail;3, commutate guide rail;4, guide rail car;5, conducting wire;9, aircraft;41, upper sweep;
411, bar shaped is perforated;412, driving wheel;414, first motor;415, the second motor;416, Coupling;417, sliding seat;418,
Sliding bar;42, lower sweep;422, idler wheel;423, mounting base;4231, retractable cable mouth;424, the 4th motor;425, wire spool is pacified
Tankage;426, shaft;427, gear is driven;43, wire spool;433, roll;435, driven internal gear;437, shaft grafting
Mouthful;44, the second cover board;441, telltale mark;91, main part;91a, upper shell;91b, lower housing;910, fan mounting portion;
9101, upper bracket;9102, lower bracket;9103, charge transmitting module mounting portion;9104, circuit board installation cavity;9105, it enters the wind
Hole;9106, vent;9107, lower camera;911, go out vane;9110, it rises and falls Holder joint;9111, vane upper shell;9112,
Vane lower housing;91121, interior curved wall;91122, dowel;91123, air outlet guard board;91124, training wall;912, connecting tube;
9121, third motor mounting plate;9122, valve plate guide rod;9123, baffle;913, the first cover board;92, charge transmitting module;93,
Undercarriage;931, connection pipe body;9311, hinged seat;9312, strip shape gob;932, sliding tube;9321, piston;9322, articulated joint;
933, sealing cap;9331, spring positioning bar;934, connecting rod;935, supporting rod;9351, connecting rod tank;936, the second electromagnet;
937, spring;94, air intake cover;941, the first electromagnet;942, upper camera;951, upper driving fan;952, lower driving fan;
96, adjusting part;961, third motor;962, screw rod;963, valve plate;97, control circuit board.
Specific implementation mode
Embodiment 1
According to Fig. 1 to Figure 17, the present embodiment is a kind of electric vehicle power supply system, includes to be fixedly mounted on both sides of the road
Multiple power transmission rods 1, be mounted on each power transmission rod between transmission guide rail 2, roll or be slidably mounted on the transmission guide rail
And the guide rail car 4 being electrically connected with transmission guide rail, the aircraft 9 that can be rested on electric vehicle and be electrically connected with electric vehicle,
And be connected between guide rail car and aircraft electric energy to be transferred to the conducting wire 5 on electric vehicle from transmission guide rail.
Two groups of commutation guide rails for guide rail car commutation are at least connected between two groups of transmission guide rails of both sides of the road
3;The transmission guide rail, commutation guide rail have respectively included two tracks disposed in parallel, and each track is including at least there are one use
In guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part phase between two tracks
To setting.
The guide rail car includes upper sweep 41, and is fixedly connected on the lower sweep 42 below sweep;It is described to get on the bus
There are two first motors 414 for the fixed installation of plate upper left side front and rear portions, and there are two energy for the upper upper right side front and rear portions installation of sweep
Enough the second motors 415 moved along guide rail car left and right directions;The first motor, the second motor lower end be respectively fixedly connected with
Both sides transmission guide rail rolls the driving wheel 412 of connection.
Sweep left and right directions forms the bar shaped perforation 411 slided for the second motor 415 in the upper sweep upper edge;It is described
The pushing meanss for driving the second motor close to transmission guide rail are installed on upper sweep.
The pushing meanss include being fixedly connected on the sliding seat 417 of the upper both sides of perforating in bar shaped of sweep, and sliding connects
It is connected in sliding seat and horizontally disposed sliding bar 418, and is set on the outside of the second motor and solid with two sliding bar one end
Surely the Coupling 416 connected;Compressed spring is installed between the sliding bar and sliding seat.
The lower sweep both sides are rotatably connected to by shaft and roll the idler wheel 422 being electrically connected with transmission guide rail so that institute
Shaft is stated to be electrically connected with the transmission guide rail of homonymy.The lower sweep is being at least non-conductive material with the link position of shaft
Material.
The vertical plate portion cooperation of the driving wheel and the track rolls connection, the idler wheel then with the horizontal plate part of track
Rolling electrically connects, and the idler wheel is metal wheel, and 2-3 idler wheel is arranged in each side of lower sweep, is on the one hand conducive to guide rail car in this way
On the other hand steady traveling on transmission guide rail can ensure good between idler wheel and transmission guide rail electrically connect.Further
It says, can be connected by bearing between idler wheel and shaft, then also form Electricity Federation between the metal material inner ring of bearing, outer ring and ball
It connects, and larger resistance may be caused between ball and inner ring, outer ring there are lubricant medium, therefore guide rail car passes through 2-3 per side
Idler wheel is rolled with transmission guide rail and is connected, and can ensure the continuity transmitted electricity between guide rail car and transmission guide rail, ensures stable electricity
Pressure, electric current.
Since the quantity of electric vehicle and travel direction that charge on each section of road are random, therefore
It needs to connect at least two groups commutation guide rail between two transmission guide rails of both sides of the road, in order to which guide rail car is from road side
Transmission guide rail is moved on the transmission guide rail of the other side.
Further, since in commutation guide rail and transmission guide rail junction and transmission guide rail, in road, there are corners
Certainly exist non-directional track(It is general as arc-shaped in being designed as in Fig. 1), therefore the second design of electrical motor of side is on guide rail car
It can be moved along guide rail car left and right directions so that when driving into arc-shaped track the driving wheel of both sides can keep guide rail car
It offsets with the holding of two siding tracks.
Guide rail car bottom surface intermediary form has mounting base 423, the mounting base lower part to form wire spool mounting groove
425, the wire spool mounting groove intermediary form has shaft 426, and wire spool 43 is rotatably connected in the shaft;Non-conducting material
The shaft on be provided with two electrode a in an axial direction, two electrode a are electrically connected with the shaft of lower sweep both sides respectively;It is described
Wire spool intermediary form has roll 433;The roll intermediary form has shaft interface 437, and the wire spool is by turning
The rotation of axis interface is set on the outside of shaft;It is provided on the shaft interface inner wall and is electrically connected respectively with two electrode a slidings
The two electrode b connect;The Wire-wound is in the wire spool, and one end of conducting wire is electrically connected with two electrode b;Institute
It states and the 4th motor 424 is installed in mounting base;It is equipped in the wire spool mounting groove and the output axis connection of the 4th motor
Drive gear 427;The driven internal gear 435 with driving gear engaged transmission is formed on the wire spool;The wire spool peace
Tankage side wall forms the retractable cable mouth 4231 passed through for conducting wire.
The controller electrically connected with first motor, the second motor, the 4th motor is installed, controller is logical on the guide rail car
The control system communication for crossing wireless network and server and electric vehicle, needs to charge when server receives electric vehicle
Request when, the controller of the guide rail car of server controls nearby is communicated with the electric vehicle of request charging;Then guide rail car control
Aircraft processed flies on electric vehicle and charges to electric vehicle.
In the guide rail car working condition, wire spool releases conducting wire under the driving of the 4th motor, enables aircraft
It flies on electric vehicle to be charged;Wire spool is driven by the 4th motor in guide rail car off working state and rolls conducting wire, is kept away
Exempt from that vehicular traffic is caused to hinder.
The aircraft includes main part 91, and the main part includes the fan mounting portion 910 of tubular, is connected to
Fan mounting portion periphery and the connecting tube 912 of 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 911.
It is located in the fan mounting portion above connecting tube and is connected with upper bracket 9101, is equipped on the upper bracket
Driving fan 951;It is located in the fan mounting portion below connecting tube and is connected with lower bracket 9102, is installed on the lower bracket
There is lower driving fan 952;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, position in the fan mounting portion
Wind pressure superatmospheric between upper driving fan and lower driving fan so that go out and form wind pressure in vane.
It is described go out vane include sealed connection vane upper shell 9111 and vane lower housing 9112, the vane lower casing
Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected by multiple dowels 91122 there are one air outlet guard board,
Air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end;Shape between the interior curved wall 91121 and air outlet guard board 91123
At outlet air gap wide at the top and narrow at the bottom, the lower end width in outlet air gap is 0.8-1.5mm;The inner circumferential of the vane lower housing is located at
The lower section in outlet air gap is training wall 91124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree.
The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out shape between the axial direction of vane and horizontal direction
At the angle of 5-20 degree, and go out the horizontal wind-force of wind generation and the turning for the fan blade of upper driving fan of the outlet air gap blowout of vane
Dynamic direction is opposite.
It is equipped with to adjust the adjusting part 96 that corresponding position goes out vane outlet air speed in each connecting tube, it is described
Adjusting part includes third motor 961, the screw rod 962 coaxially connected with third motor output shaft, and is connected with screw flight
The valve plate 963 connect;For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the middle part of upper and lower directions in connecting tube
Position;The connecting tube internal upper part forms to install the third motor mounting plate of the third motor, the third motor
Mounting plate 9121 is connected with the valve plate guide rod 9122 being slidably connected with the valve plate towards the side for going out vane;In the connecting tube
There are one upper ends for lower part connection towards the inclined baffle 9123 in vane direction is gone out, and conducting area is formed between the baffle and valve plate
Adjustable air passage.
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board 97 respectively.
The main part is upper shell 91a and lower housing 91b is tightly connected and constitutes.
The main part upper end connects the air intake cover 94 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover
The air inlet of shape.
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, to realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only play tune
The effect of whole attitude of flight vehicle goes out when vane generates touching with foreign object without the fan for being provided with power and does not easily lead to aircraft
Out of control or generate injury to human or animal, safety is good.The aircraft appearance is similar to four-axle aircraft, therefore with four-axle aircraft
It is named, four go out vane i.e. so-called " four axis " and only play the function of adjusting posture, therefore this aircraft substantially should be uniaxial
Aircraft.
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, the axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out the axial direction and level of vane
The horizontal wind-force and upper driving fan that the wind for forming the angle of 5-20 degree between direction, and going out the outlet air gap blowout of vane generates
Fan blade rotation direction it is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset and driven
The reaction force that dynamic fan and lower driving fan generate when rotating;Also, change outlet air by adjusting each adjusting part simultaneously
Ring go out wind velocity, it can be achieved that aircraft whole forward or reverse.Make one by adjusting one or two adjusting part
Or two go out vane go out wind velocity, it can be achieved that aircraft is generally in heeling condition, can be driven aircraft in this way in level
It flies in direction.
First electromagnet 941, the top installation of first electromagnet are installed at the top of the air intake cover of the aircraft
There is upper camera 942;The upper camera and the first electromagnet are electrically connected with control circuit board respectively;The wire spool installation
Slot lower end is fixedly connected with the second cover board 44;Second cover board lower end forms cross telltale mark 441;Second cover board
The position that lower end corresponds to telltale mark is connected with the permanent magnet sucked by magnetic force with the first electromagnet.
The aircraft passes through the first electromagnet in off working state(Iron core)It sucks below the second cover board forever
On magnet, when aircraft works, the first electromagnet is powered to generating keeps aircraft and the second cover board de- with the reversed magnetic field of permanent magnet
From.The upper camera is used to judge the position of aircraft opposite rail vehicle, in order to which aircraft can be by accurately resting in
On guide rail car.The upper camera shooting obtains the position of aircraft opposite rail vehicle, can be flown by manual operation remote control
Device is accommodated to by the first electromagnet on corresponding guide rail car, can also be automatically accommodated to by aircraft by machine vision technique
On corresponding guide rail car.
The lower, outer perimeter of the fan mounting portion is charging transmitting module mounting portion 9103, is charged on transmitting module mounting portion
It is connected with the charging transmitting module 92 being electrically connected with control circuit board;The lower bracket bottom of the aircraft is equipped with lower camera
9107, the lower camera is electrically connected with control circuit board;The electromobile at top is equipped with to be electrically connected with charging transmitting module
The charging receiving module connect.
The charging transmitting module, charging receiving module can be the electrodes of contact, can also be to pass through wireless charging
Power technology carries out the coil of power transmission.
The top for being located at charging transmitting module mounting portion on the fan mounting portion is a circuit board installation cavity 9104, institute
Control circuit board is stated in circuit board installation cavity, there are one the first cover boards of annular for the connection of circuit board installation cavity lower end
913;The upper surface of the circuit board installation cavity uniformly forms the air inlet hole 9105 being connected to in fan mounting portion, the circuit
The lateral wall of plate installation cavity uniformly forms vent 9106.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, is played to control circuit board scattered
Heat effect.
Go out position of the vane inner circumferential far from connecting tube described in each and forms Holder joint 9110 of rising and falling, each undercarriage
Respectively there are one undercarriages 93 for connection on connector;The undercarriage is equipped with to suck the second electromagnet in electromobile at top
936。
When there is electric vehicle to need charging, the 4th motor drives wire spool rotation to release conducting wire, while aircraft is detached from
Guide rail car is simultaneously flown on electric vehicle, and aircraft sucks the gold in electromobile at top by the second electromagnet of undercarriage lower end
Belong on vehicle shell.
Embodiment 2
In conjunction with Figure 18 to Figure 19, the present embodiment also makes following improvement on the basis of embodiment 1:Go out vane inner circumferential described in each
Position far from connecting tube forms Holder joint 9110 of rising and falling, and respectively there are one undercarriages for connection in each Holder joint of rising and falling
93;The undercarriage include be fixedly connected with Holder joint of rising and falling and by rise and fall Holder joint with go out the company being connected inside vane
Take over body 931, the sliding tube 932 being slidably mounted in connection pipe body connect with connection pipe body close to Holder joint one end rotation of rising and falling
The supporting rod 935 connect is connected on supporting rod far from Holder joint one end of rising and falling sucking second in electromobile at top
Electromagnet 936, and the connecting rod 934 with rotation connection in the middle part of sliding tube middle part, supporting rod respectively.
The connection pipe body forms hinged seat 9311, 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 9321, sliding pipe outer wall middle part position close to Holder joint one end of rising and falling
It sets and is connected with articulated joint 9322, 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 9312 passed through for articulated joint;The one end of 912 body of the connecting tube far from Holder joint of rising and falling is solid
Surely it is connected with sealing cap 933, the inner end of sealing cap is connected with spring positioning bar 9331, is arranged on the spring positioning bar
Spring 937, the both ends of the spring are against respectively between piston and sealing cap inner end;It forms on the supporting rod and is received in supporting rod
The connecting rod tank 9351 of the connecting rod is accommodated when the state of rising.
The spring is in supporting rod when extended configuration and is in unfolded state, 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 with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, go out
Wind pressure in vane makes piston be moved to sealing cap one end together with sliding tube, to make sliding tube drive connecting rod one end to sealing cap
Direction is moved, to make supporting rod lower end also be rotated to sealing cap one end, to make undercarriage be in collapsed state.Work as aircraft
When landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved toward hinged seat direction together with piston, to make sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, to make supporting rod lower end turn to extreme position to hinged seat one end, to
Undercarriage is set 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 makes spring 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.
Claims (2)
1. a kind of electric vehicle power supply system, it is characterised in that:Include the multiple power transmission rods for being fixedly mounted on both sides of the road, peace
Transmission guide rail between each power transmission rod is rolled or is slidably mounted on the transmission guide rail and is electrically connected with transmission guide rail
Guide rail car, the aircraft that can be rested on electric vehicle and be electrically connected with electric vehicle, and be connected to guide rail car with fly
Between row device electric energy to be transferred to the conducting wire on electric vehicle from transmission guide rail;
The guide rail car includes upper sweep, and is fixedly connected on the lower sweep below sweep;The upper sweep upper left side
There are two first motors for front and rear portions fixed installation, and there are two can be along a guide rail car left side for the upper upper right side front and rear portions installation of sweep
Second motor of right direction movement;The first motor, the second motor lower end have been respectively fixedly connected with rolls with both sides transmission guide rail
The driving wheel of dynamic connection;
Sweep left and right directions forms the bar shaped perforation slided for the second motor in the upper sweep upper edge;Pacify on the upper sweep
Equipped with driving the second motor close to the pushing meanss of transmission guide rail;
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at sliding
In seat and horizontally disposed sliding bar, and it is set in the socket being fixedly connected on the outside of the second motor and with two sliding bar one end
Part;Compressed spring is installed between the sliding bar and sliding seat;
The lower sweep both sides are rotatably connected to by shaft and roll the idler wheel that be electrically connected with transmission guide rail so that the shaft and
The transmission guide rail of homonymy is electrically connected;
Guide rail car bottom surface intermediary form has mounting base, the mounting base lower part to form wire spool mounting groove, the coiling
Disk mounting groove intermediary form has shaft, and wire spool is rotatably connected in the shaft;
Be provided in an axial direction in the shaft of non-conducting material two electrodes a, two electrode a respectively with lower sweep both sides turn
Axis is electrically connected;The wire spool intermediary form has roll;The roll intermediary form has shaft interface, the wire spool
It is set on the outside of shaft by the rotation of shaft interface;It is provided on the shaft interface inner wall and is slided respectively with two electrode a
Two electrode b of dynamic electrical connection;The Wire-wound is in the wire spool, and one end of conducting wire and two electrode b electricity
Connection;
4th motor is installed in the mounting base;Output axis connection with the 4th motor is installed in the wire spool mounting groove
Driving gear;The driven internal gear with driving gear engaged transmission is formed on the wire spool;
The wire spool installation groove sidewall forms the retractable cable mouth passed through for conducting wire;
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 of 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 bracket, lower driving fan is installed on the lower bracket;
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 the interior installation of fan mounting portion, is located at upper driving fan under in the fan mounting portion
Wind pressure superatmospheric between driving fan so that go out and form wind pressure in vane;
It is described go out vane include sealed connection vane upper shell and vane lower housing, the vane lower housing inner circumferential upper end at
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 is 20-30 degree;
The axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out and form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of the horizontal wind-force and the fan blade of upper driving fan of the wind generation of the outlet air gap blowout of vane
To 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 third motor, the coaxially connected screw rod with third motor output shaft, and the valve plate being connect with screw flight;It is described
For 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;The connecting tube
Internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate;There are one upper end directions to go out for lower part connection in the connecting tube
The inclined baffle in vane direction forms the conducting adjustable air passage of area between the baffle and valve plate;
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively;
The main part is that upper shell and lower housing are tightly connected and constitute;
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly formed on air intake cover strip into
Air port.
2. a kind of electric vehicle power supply system as described in claim 1, it is characterised in that:Two groups of transmissions of electricity positioned at both sides of the road
Two groups of commutation guide rails for guide rail car commutation are at least connected between guide rail;
The transmission guide rail, commutation guide rail have respectively included two tracks disposed in parallel, there are one each track includes at least
For guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part between two tracks
It is oppositely arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810517625.3A CN108688516B (en) | 2017-06-23 | 2017-06-23 | Power supply system of electric automobile |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810517625.3A CN108688516B (en) | 2017-06-23 | 2017-06-23 | Power supply system of electric automobile |
| CN201710488125.7A CN107176062B (en) | 2017-06-23 | 2017-06-23 | A kind of electric vehicle power supply system |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710488125.7A Division CN107176062B (en) | 2017-06-23 | 2017-06-23 | A kind of electric vehicle power supply system |
Publications (2)
| Publication Number | Publication Date |
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| CN108688516A true CN108688516A (en) | 2018-10-23 |
| CN108688516B CN108688516B (en) | 2020-01-14 |
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| CN201810517307.7A Active CN108749649B (en) | 2017-06-23 | 2017-06-23 | Power supply system of electric automobile |
| CN201710488125.7A Active CN107176062B (en) | 2017-06-23 | 2017-06-23 | A kind of electric vehicle power supply system |
| CN201810517625.3A Active CN108688516B (en) | 2017-06-23 | 2017-06-23 | Power supply system of electric automobile |
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| CN201810517307.7A Active CN108749649B (en) | 2017-06-23 | 2017-06-23 | Power supply system of electric automobile |
| CN201710488125.7A Active CN107176062B (en) | 2017-06-23 | 2017-06-23 | A kind of electric vehicle power supply system |
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| CN107826659A (en) * | 2017-12-19 | 2018-03-23 | 重庆扬明聚电新能源科技有限公司 | A kind of ring type moving track mechanism for mobile charging stake |
| CN110758139A (en) * | 2019-09-20 | 2020-02-07 | 南京浦口科学城建设发展有限公司 | Charger robot for stereo garage |
| CN112265455B (en) * | 2020-11-02 | 2022-05-31 | 北京智扬北方国际教育科技有限公司 | Portable mobile new energy automobile charging device |
| CN114407731B (en) * | 2022-01-06 | 2023-06-09 | 杭州申昊科技股份有限公司 | Subway assembled rigid contact net suspension device |
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- 2017-06-23 CN CN201810517307.7A patent/CN108749649B/en active Active
- 2017-06-23 CN CN201710488125.7A patent/CN107176062B/en active Active
- 2017-06-23 CN CN201810517625.3A patent/CN108688516B/en active Active
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| CN2853496Y (en) * | 2005-03-21 | 2007-01-03 | 钱致疆 | One-by-one step automatic charging type multiple power supply trolley bus |
| CN106575887A (en) * | 2014-06-25 | 2017-04-19 | Elix无线充电系统公司 | Methods and apparatus for automatic alignment of wireless power transfer systems |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN108749649A (en) | 2018-11-06 |
| CN107176062B (en) | 2018-08-28 |
| CN108688516B (en) | 2020-01-14 |
| CN108749649B (en) | 2021-10-22 |
| CN107176062A (en) | 2017-09-19 |
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Effective date of registration: 20220713 Address after: 310051 1, -10 5, No. 11, Ju Gong Road, Binjiang District Xi Xing street, Hangzhou, Zhejiang. Patentee after: Jiang Jiahui Address before: 310051 1, -10 5, No. 11, Ju Gong Road, Binjiang District Xi Xing street, Hangzhou, Zhejiang. Patentee before: HANGZHOU LIPU TECHNOLOGY Co.,Ltd. |