CN107215232A - A kind of New-energy electric vehicle charging system - Google Patents

A kind of New-energy electric vehicle charging system Download PDF

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Publication number
CN107215232A
CN107215232A CN201710488470.0A CN201710488470A CN107215232A CN 107215232 A CN107215232 A CN 107215232A CN 201710488470 A CN201710488470 A CN 201710488470A CN 107215232 A CN107215232 A CN 107215232A
Authority
CN
China
Prior art keywords
vane
fan
guide rail
seat
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.)
Granted
Application number
CN201710488470.0A
Other languages
Chinese (zh)
Other versions
CN107215232B (en
Inventor
虞丽丽
江佳辉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Yidian New Energy Technology Co ltd
Original Assignee
Wenzhou Rui Chu Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Wenzhou Rui Chu Technology Co Ltd filed Critical Wenzhou Rui Chu Technology Co Ltd
Priority to CN201711451190.9A priority Critical patent/CN108128199A/en
Priority to CN201711449781.2A priority patent/CN108128197A/en
Priority to CN201711451201.3A priority patent/CN108128200A/en
Priority to CN201710488470.0A priority patent/CN107215232B/en
Publication of CN107215232A publication Critical patent/CN107215232A/en
Application granted granted Critical
Publication of CN107215232B publication Critical patent/CN107215232B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14—Conductive energy transfer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • B60L53/32—Constructional details of charging stations by charging in short intervals along the itinerary, e.g. during short stops
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60M—POWER SUPPLY LINES, AND DEVICES ALONG RAILS, FOR ELECTRICALLY- PROPELLED VEHICLES
    • B60M7/00—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway
    • B60M7/003—Power lines or rails specially adapted for electrically-propelled vehicles of special types, e.g. suspension tramway, ropeway, underground railway for vehicles using stored power (e.g. charging stations)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • 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
    • B64C25/62—Spring shock-absorbers; Springs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/022—Tethered aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/12—Electric charging stations
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

The invention discloses a kind of New-energy electric vehicle charging system, include the multiple power transmission rods for being fixedly mounted on both sides of the road, transmission guide rail between each power transmission rod of road homonymy, the guide rail car for rolling or being slidably mounted on the transmission guide rail and electrically connected with transmission guide rail, can rest in guide rail car lower end and the aircraft electrically connected with guide rail car, and be connected between electric automobile and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；The present invention realizes electric automobile without stopping the function that can be charged, and electric automobile aircraft in the case of fully charged or other can depart from guide rail car at any time, will not cause limitation to freely travelling for electric automobile.

Description

A kind of New-energy electric vehicle charging system
Technical field
The invention belongs to electric automobile corollary system field, and in particular to a kind of New-energy electric vehicle charging system.
Background technology
With the popularization of electric automobile, the problem of charging electric vehicle is inconvenient is also increasingly highlighted；Electric automobile is bought at present User be typically limited to only that city is on and off duty to be used, it is necessary to which outgoing user then still tends to use fuel oil at a distance for a long time Car.And even city short distance is travelled, user is also required to note very much the dump energy of electric automobile, otherwise easily occurs on the way Situation about being cast anchor without electricity.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric automobile Speech is not just most suitable, and the floor space of one side electric automobile is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills Electricity is likely to result in traffic congestion, on the other hand, the big many of battery truck of the electric automobile power consumption also than two-wheeled, in current battery charging In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
The content of the invention
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, provide a kind of charging conveniently, and The electric automobile electric power system of user hours underway is not delayed.
To realize the purpose of the present invention, it is achieved using following technical scheme：A kind of New-energy electric vehicle Charging System, includes the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission of electricity between each power transmission rod of road homonymy Guide rail, the guide rail car for rolling or being slidably mounted on the transmission guide rail and electrically connected with transmission guide rail, can rest in guide rail Car lower end and the aircraft electrically connected with guide rail car, and be connected between electric automobile and aircraft to by electric energy from defeated Conductance rail is transferred to the wire on electric automobile；The transmission guide rail by two it is symmetrical, be open towards opposite U-shaped rail It is spliced, spliced transmission guide rail radial section is connected in I-shaped between two U-shaped rail by insulating materials；Institute State guide rail car lower end and be connected with power supply connecting seat, the power supply connecting seat, which includes the magnet being sequentially connected from top to bottom, to be fixed Seat, current electrode seat, insulation board and current electrode plate；Current electrode seat, current electrode plate respectively with two U-shaped rail Electricity Federations Connect；The current electrode seat lower end uniformly forms convex cavity under multiple circular groove shapes, and the current electrode seat is non-ferromagnetic material The metal of material is made, or is made up of nonmetallic materials；When current electrode seat is nonmetallic materials, the current electrode seat is extremely Few its lower surface convex chamber outer surface together with is coated with conductive layer；The magnet fixed seat lower end corresponds to the position of convex cavity under each Put and be connected with permanent magnet a, permanent magnet a is stretched under correspondence position in convex cavity；The lower end of the insulation board corresponds to convex under each The position of cavity forms the insulation sleeve of convex cavity lateral wall under insulating；Each insulation sleeve of correspondence on the current electrode plate Position form appearance hole；The first electromagnet sucked with permanent magnet a by magnetic force is installed at the top of the aircraft, described the The receiving electrode a for getting an electric shock and being connected with current electrode seated connection is installed at the top of one electromagnet；It is located at first at the top of the aircraft The periphery of electromagnet is connected with 3 elastic rods, and the upper end of elastic rod is connected with the reception electricity that electrical connection is contacted with current electrode plate Pole b；The receiving electrode a, receiving electrode b and wire are electrically connected, the control board electricity of first electromagnet and aircraft Connection；First electromagnet and the permanent magnet a of any position realize being electrically connected for receiving electrode a and current electrode after sucking Connect, then aircraft makes each elastic rod depart from there may be convex cavity lower surface under contact along the rotation of own central axis line, and The output electrode b of elastic rod bottom is set finally to contact electrical connection with current electrode plate.
Preferably：The guide rail car includes the overall vehicle frame in opening up U-shaped, the vehicle frame top two Side is two symmetrically arranged vehicle frame plates, and two vehicle frame plates inner sides are rotatablely equipped with more than 2 groups of driving wheel respectively, described The axis of driving wheel is horizontally disposed, and the position of each driving wheel of correspondence is provided with to band on the outside of two vehicle frame plates The motor that dynamic driving wheel is rotated；
Roller is also separately installed with the inside of two vehicle frame plates, the U-shaped rail contact of the roller and homonymy is electrically connected；Institute State roller to be rotatably installed in the roller mount of U-shaped, the sliding bar set along frame width direction, institute are connected with the roller mount The sliding seat for being provided with and being slidably connected with sliding bar on vehicle frame plate is stated, is provided with and is used between the sliding bar and sliding seat Pushing rolling wheels are against the spring on U-shaped rail；Connecting rod is connected between the roller mount of homonymy；
Roller mount or connecting rod positioned at vehicle frame both sides are electrically connected by electric wire with current electrode seat, current electrode plate so that transmission of electricity Guide rail is electrically connected with power supply connecting seat formation.
Preferably：The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes one The Wiinding cartridge of individual upper end open, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the magnetic material of Wiinding cartridge upper end Lid；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through.
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 in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
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；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction 20 degree of angle, and go out the rotation side 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 To opposite；
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 the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described 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；The connecting tube Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
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.
Preferably：The electromagnet, elastic rod are connected to the top of the air intake cover.
Preferably：The main part upper end is provided with camera, the upper camera and control board electricity Connection.
Preferably：The lower, outer perimeter of the fan installation portion is to connect on battery installation portion, battery installation portion It is connected to the battery electrically connected with control board；
The lower end of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board.
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 on support bar away from Holder joint one end of rising and falling to inhale Tight the second electromagnet in electromobile at top, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar；
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；
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in running order Afterwards, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
The present invention also provides another New-energy electric vehicle charging system, includes and is fixedly mounted on many of both sides of the road Individual power transmission rod, the transmission guide rail between each power transmission rod of road homonymy rolls or is slidably mounted on the transmission of electricity and leads The guide rail car electrically connected on rail and with transmission guide rail, can rest in guide rail car lower end and the aircraft electrically connected with guide rail car, And be connected between electric automobile and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The transmission guide rail by two it is symmetrical, opening be spliced towards opposite U-shaped rail, spliced transmission guide rail Radial section is connected in I-shaped between two U-shaped rail by insulating materials；
The guide rail car lower end is connected with power supply connecting seat, and the power supply connecting seat includes the magnet being sequentially connected from top to bottom Fixed seat, current electrode seat, insulation board and current electrode plate；Current electrode seat, current electrode plate are electric with two U-shaped rail respectively Connection；
The current electrode seat lower end uniformly forms convex cavity under multiple circular groove shapes, and the current electrode seat is non-ferromagnetic material The metal of material is made, or is made up of nonmetallic materials；When current electrode seat is nonmetallic materials, the current electrode seat is extremely Few its lower surface convex chamber outer surface together with is coated with conductive layer；
The position that the magnet fixed seat lower end corresponds to convex cavity under each is connected with permanent magnet a, and permanent magnet a stretches into correspondence position Under in convex cavity；
The lower end correspondence of the insulation board forms the insulation of convex cavity lateral wall under insulating in the position of convex cavity under each Set；
The position of each insulation sleeve of correspondence forms appearance hole on the current electrode plate；
The first electromagnet sucked with permanent magnet a by magnetic force, the top of first electromagnet are installed at the top of the aircraft Portion is provided with the receiving electrode a for getting an electric shock and being connected with current electrode seated connection；It is located at the periphery of the first electromagnet at the top of the aircraft 3 elastic rods are connected with, the upper end of elastic rod is connected with the receiving electrode b that electrical connection is contacted with current electrode plate；It is described to receive Electrode a, receiving electrode b and wire are electrically connected, and first electromagnet is electrically connected with the control board of aircraft；
First electromagnet and the permanent magnet a of any position realize being electrically connected for receiving electrode a and current electrode after sucking Connect, then aircraft makes each elastic rod depart from there may be convex cavity lower surface under contact along the rotation of own central axis line, and The output electrode b of elastic rod bottom is set finally to contact electrical connection with current electrode plate；
The guide rail car includes the overall vehicle frame in opening up U-shaped, and vehicle frame top both sides are two and are symmetrical arranged Vehicle frame plate, be rotatablely equipped with more than 2 groups of driving wheel on the inside of two vehicle frame plates respectively, the axis of the driving wheel is along water Square to setting, the position of each driving wheel of correspondence is provided with the drive for driving driving wheel to rotate on the outside of two vehicle frame plates Dynamic motor；
Roller is also separately installed with the inside of two vehicle frame plates, the U-shaped rail contact of the roller and homonymy is electrically connected；Institute State roller to be rotatably installed in the roller mount of U-shaped, the sliding bar set along frame width direction, institute are connected with the roller mount The sliding seat for being provided with and being slidably connected with sliding bar on vehicle frame plate is stated, is provided with and is used between the sliding bar and sliding seat Pushing rolling wheels are against the spring on U-shaped rail；Connecting rod is connected between the roller mount of homonymy；
Roller mount or connecting rod positioned at vehicle frame both sides are electrically connected by electric wire with current electrode seat, current electrode plate so that transmission of electricity Guide rail is electrically connected with power supply connecting seat formation；
The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes the coiling of a upper end open Box, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through；
The aircraft includes main part, and the main part includes the fan installation portion of tubular, is connected to fan installation Portion periphery and the connecting tube for four equidistant arrangements being connected with fan installation portion, and be connected to each connecting tube outer end and with What correspondence position connecting tube was connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed； It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
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；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction 20 degree of angle, and go out the rotation side 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 To opposite；
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 the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described 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；The connecting tube Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
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 electromagnet, elastic rod are connected to the top of the air intake cover；
The main part upper end is provided with camera, and the upper camera is electrically connected with control board;
The lower, outer perimeter of the fan installation portion is to be connected with battery installation portion, battery installation portion and control board electricity The battery of connection；
The lower end of the aircraft is provided with lower camera, and the lower camera is 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, which includes, to be fixedly connected with Holder joint of rising and falling and by Holder joint of rising and falling with going out vane The connection pipe body that inside is connected, is slidably mounted on the sliding tube in connection pipe body, with connection pipe body close to Holder joint one of rising and falling End rotates the support bar of connection, is connected on support bar away from Holder joint one end of rising and falling to suck in electromobile at top Second electromagnet, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar；
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；
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in running order Afterwards, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention on transmission guide rail by travelling and keeping With the guide rail car of electric automobile identical travel speed, coordinate the aircraft and guide rail car electricity being connected with electric automobile by wire Connection comes for the charging electric vehicle in traveling, realizes electric automobile without stopping the function that can be charged, and electricity Electrical automobile aircraft in the case of fully charged or other can depart from guide rail car at any time, will not be to the free walker of electric automobile Sail and cause limitation.
When aircraft does not work, the aircraft passes through the second electromagnet（Iron core）Suck in electromobile at top coiling The upper end of the lid of component, when aircraft works, the energization of the second electromagnet, which produces the magnetic field reverse with the lid of magnetic material, to be made Aircraft departs from electric automobile.
When electric automobile needs charging, the control system of electric automobile sends signal, clothes to the server of charging system The guide rail car of business device control nearby is kept travelling with electric automobile uniform velocity, and then the control system of electric automobile is sent out to aircraft The number of delivering letters, makes aircraft fly to corresponding guide rail car and rests in guide rail car lower end, electric automobile is formed electricity with transmission guide rail Connection；During aircraft flies out, control system controls the coiling electric motor of wire-winding unit to rotate simultaneously makes wire from wire spool Release；After charging electric vehicle is finished, aircraft flies back to electromobile at top, at the same coiling electric motor rotate backward make wire around Unroll on drum.
The aircraft provides driving force, the part that upper driving fan is produced by the upper driving fan in fan installation portion Air-flow blows out downwards from each air-out gap for going out vane, and combines adjusting part and adjust each to go out vane and go out wind velocity, from And the horizontal flight or steering of aircraft are realized, due to going out vane positioned at each of aircraft periphery and only play adjustment aircraft The effect of posture, without the fan for being provided with power, go out not being easily caused when vane and foreign object produce touching aircraft it is out of control or Injury is produced to human or animal, security is good.The similar four-axle aircraft of aircraft outward appearance, four go out vane and only play regulation appearance The function of state, therefore the present invention substantially should be single shaft aircraft.
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 Dynamic fan, or the reaction force produced when upper driving fan and the rotation of lower driving fan；Also, adjusted by adjusting each simultaneously Component change vane go out wind velocity, the overall forward or reverse of aircraft can be achieved.Adjusted by adjusting one or two Section component makes what one or two went out vane to go out wind velocity, and aircraft can be achieved generally in heeling condition, can so drive Aircraft flies in the horizontal direction.
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.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is that aircraft rests in structural representation when on electric automobile.
Fig. 3 is the decomposition texture schematic diagram of wire-winding unit.
Fig. 4 is the structural representation of aircraft and guide rail car.
Fig. 5 is the structural representation of power supply connecting seat.
Fig. 6 is the decomposition texture schematic diagram of power supply connecting seat.
Fig. 7 is the structural representation of aircraft stopped status.
Fig. 8 is the structural representation of aircraft flight state.
Fig. 9 is the cross section structure diagram of aircraft.
Figure 10 is Fig. 9 A portions schematic enlarged-scale view.
Figure 11 is Fig. 9 B portions schematic enlarged-scale view.
The structural representation of each part that Figure 12 is upper shell and is connected with upper shell.
Figure 13 is the structural representation of lower housing section.
Figure 14 is the cross section structure diagram of lower housing section.
Figure 15 is the structural representation of air intake cover.
Figure 16 is the decomposition texture schematic diagram of undercarriage part.
Figure 17 is the cross section structure diagram of undercarriage part.
1st, power transmission rod；2nd, transmission guide rail；3rd, commutate guide rail；4th, guide rail car；40th, vehicle frame；401st, mounting seat；41st, drive Wheel；411st, motor；42nd, roller；421st, roller mount；422nd, sliding bar；423rd, sliding seat；424th, connecting rod；43rd, power supply connection Seat；431st, magnet fixed seat；432nd, current electrode seat；433rd, insulation sleeve；434th, current electrode plate；5th, electric automobile；5a, coiling Component；51st, Wiinding cartridge；511st, line mouthful is crossed；52nd, coiling electric motor；53rd, wire spool；54th, lid；6th, wire；9th, aircraft；91、 Main part；91a, upper shell；91b, lower house；910th, fan installation portion；9101st, upper bracket；9102nd, lower carriage；9103rd, electric power storage Pond installation portion；9104th, circuit board installation cavity；9105th, fresh air inlet；9106th, vent；9107th, lower camera；911st, vane is gone out； 9110th, rise and fall Holder joint；9111st, vane upper shell；9112nd, vane lower house；91121st, interior curved wall；91122nd, dowel； 91123rd, air outlet guard board；91124th, training wall；912nd, connecting tube；9121st, the 3rd motor mounting plate；9122nd, valve plate guide rod； 9123rd, baffle plate；913rd, the first cover plate；913rd, upper camera；92nd, battery；93rd, undercarriage；931st, connection pipe body；9311st, cut with scissors Joint chair；9312nd, strip shape gob；932nd, sliding tube；9321st, piston；9322nd, articulated joint；933rd, sealing cap；9331st, spring locating rod； 934th, connecting rod；935th, support bar；9351st, connecting rod tank；936th, the second electromagnet；937th, spring；94th, air intake cover；941st, first Electromagnet；942nd, receiving electrode a；943rd, elastic rod；944th, receiving electrode b；951st, upper driving fan；952nd, lower driving fan； 96th, adjusting part；961st, the 3rd motor；962nd, screw rod；963rd, valve plate；97th, control board.
Embodiment
Embodiment 1
According to Fig. 1 to 6, the present embodiment is a kind of New-energy electric vehicle charging system, includes and is fixedly mounted on road Multiple power transmission rods 1 of both sides, the transmission guide rail 2 between each power transmission rod of road homonymy, roll or are slidably mounted on The guide rail car 4 electrically connected on the transmission guide rail and with transmission guide rail, can rest in guide rail car lower end and be electrically connected with guide rail car The aircraft 9 connect, and be connected between electric automobile and aircraft electric energy is transferred into electronic vapour from transmission guide rail Wire 6 on car.
The wire is referred in whole line, wire comprising 2 electric wires.
The transmission guide rail by two it is symmetrical, opening be spliced towards opposite U-shaped rail, spliced transmission of electricity Guide rail radial section is connected in I-shaped between two U-shaped rail by insulating materials.
Be connected with two commutation guide rails 3 between the end of the transmission guide rail of both sides of the road, commutation guide rail 3 at least with Transmission guide rail junction is circular arc, and commutation guide rail is spliced as transmission guide rail by two U-shaped rail.
Because quantity and travel direction that the electric automobile charged is needed on each section of road are random, therefore Need to connect at least two groups commutation guide rails 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 opposite side.
Further, due to there is corner in road in commutation guide rail and transmission guide rail junction, and transmission guide rail Certainly exist non-directional track（Circular arc is designed as in general such as Fig. 1）, therefore the roller on guide rail car is designed to edge and led Rail car left and right directions is moved so that when driving into the track of circular arc the roller of both sides can keep and both sides U-shaped guide rail car Rail keeps offseting.
The guide rail car lower end is connected with power supply connecting seat 43, and the power supply connecting seat includes to be sequentially connected from top to bottom Magnet fixed seat 431, current electrode seat 432, insulation board 433 and current electrode plate 434；Current electrode seat, current electrode plate Electrically connected respectively with two U-shaped rail.
The current electrode seat lower end uniformly forms convex cavity under multiple circular groove shapes, and the current electrode seat is non-ferric The metal of magnetic material is made, or is made up of nonmetallic materials；When current electrode seat is nonmetallic materials, the current electrode Seat at least its lower surface convex chamber outer surface together with is coated with conductive layer.
The position that the magnet fixed seat lower end corresponds to convex cavity under each is connected with permanent magnet a, and permanent magnet a stretches into correspondence Under position in convex cavity.
The position that the lower end of the insulation board corresponds to convex cavity under each forms convex cavity lateral wall under insulating Insulation sleeve；The position of each insulation sleeve of correspondence forms appearance hole on the current electrode plate.
The first electromagnet 941 sucked with permanent magnet a by magnetic force, first electromagnetism are installed at the top of the aircraft The receiving electrode a942 for getting an electric shock and being connected with current electrode seated connection is installed at the top of iron；It is located at the first electromagnetism at the top of the aircraft The periphery of iron is connected with 3 elastic rods 943, and the upper end of elastic rod is connected with the receiving electrode that electrical connection is contacted with current electrode plate b944；The receiving electrode a, receiving electrode b and wire are electrically connected, the control board electricity of first electromagnet and aircraft Connection.
First electromagnet and the permanent magnet a of any position realize receiving electrode a and current electrode seat after sucking Electrical connection, then aircraft along own central axis line rotation make each elastic rod depart from there may be convex cavity lower end under contact Face, and the output electrode b of elastic rod bottom is finally contacted electrical connection with current electrode plate.
The guide rail car includes the overall vehicle frame 40 in opening up U-shaped, and vehicle frame top both sides are two right Claim the vehicle frame plate set, two vehicle frame plates inner sides are rotatablely equipped with more than 2 groups of driving wheel 41 respectively, the driving wheel Axis is horizontally disposed, and the position of each driving wheel of correspondence is provided with to drive driving wheel on the outside of two vehicle frame plates The motor 411 of rotation.
Roller 42, the U-shaped rail contact electricity of the roller and homonymy are also separately installed with the inside of two vehicle frame plates Connection；The roller is rotatably installed in the roller mount 421 of U-shaped, is connected with along frame width direction and is set in the roller mount Sliding bar 422, the sliding seat 423 being slidably connected with sliding bar, the sliding bar and cunning are installed on the vehicle frame plate The spring being against to pushing rolling wheels on U-shaped rail is installed between dynamic seat；Connecting rod is connected between the roller mount of homonymy 424。
It is provided with to control the controller of motor rotation direction and rotating speed on the vehicle frame.
Roller mount or connecting rod positioned at vehicle frame both sides are electrically connected by electric wire with current electrode seat, current electrode plate so that Transmission guide rail is electrically connected with power supply connecting seat formation.
Vehicle frame lower end centre position is connected with mounting seat 401, and the power supply connecting seat is fixedly connected under mounting seat End.
It can be connected between roller and roller mount by bearing, then between metal material inner ring, outer ring and the ball of bearing Formation is electrically connected, and be there is lubricant medium between ball and inner ring, outer ring and be likely to result in larger resistance, therefore guide rail car leads to per side Cross 2-3 roller to be connected with transmission guide rail rolling, ensure that the continuity transmitted electricity between guide rail car and transmission guide rail, it is ensured that steady Fixed voltage, electric current.
The electromobile at top is provided with a wire-winding unit 5a, and the wire-winding unit includes upper end open Wiinding cartridge 51, is rotatably installed in the wire spool 53 in Wiinding cartridge, and be connected to the lid 54 of the magnetic material of Wiinding cartridge upper end.
Centre position is provided with a coiling electric motor 52 in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, it is described around The rotor of line motor is fixedly connected with wire spool.
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with Slide the annular electrode b electrically connected with two annular electrode a, the battery of the annular electrode a and electric automobile or Charge controller is electrically connected, and the wire is electrically connected with annular electrode b.
The Wiinding cartridge side offers and crosses line mouthful 511 for what wire was passed through.
In addition, the aircraft is also powered by transmission guide rail.
The present invention is coordinated by being travelled on transmission guide rail and keeping the guide rail car with electric automobile identical travel speed The aircraft being connected by wire with electric automobile and guide rail car electrically connect for the charging electric vehicle in traveling, to realize electricity Electrical automobile is without stopping the function that can be charged, and electric automobile aircraft in the case of fully charged or other Depart from any time with guide rail car, limitation will not be caused to freely travelling for electric automobile.
When aircraft does not work, the aircraft passes through the second electromagnet（Iron core）Suck in electromobile at top coiling The upper end of the lid of component, when aircraft works, the energization of the second electromagnet, which produces the magnetic field reverse with the lid of magnetic material, to be made Aircraft departs from electric automobile.
When electric automobile needs charging, the control system of electric automobile sends signal, clothes to the server of charging system The guide rail car of business device control nearby is kept travelling with electric automobile uniform velocity, and then the control system of electric automobile is sent out to aircraft The number of delivering letters, makes aircraft fly to corresponding guide rail car and rests in guide rail car lower end, electric automobile is formed electricity with transmission guide rail Connection；During aircraft flies out, control system controls the coiling electric motor of wire-winding unit to rotate simultaneously makes wire from wire spool Release；After charging electric vehicle is finished, aircraft flies back to electromobile at top, at the same coiling electric motor rotate backward make wire around Unroll on drum.
Embodiment 2
With reference to shown in Fig. 7 to Figure 15, the present embodiment makes following improvement on the basis of embodiment 1：The aircraft includes Main part 91, the main part includes the fan installation portion 910 of tubular, is connected to fan installation portion periphery and pacifies with fan The connecting tube for four equidistant arrangements that dress portion is connected, and be connected to each connecting tube outer end and with correspondence position connecting tube phase What is connected goes out vane 911.
It is located to be connected with upper bracket 9101, the upper bracket above connecting tube in the fan installation portion and is provided with Drive fan 951；It is located to be connected with lower carriage 9102, the lower carriage below connecting tube in the fan installation portion and installs There is lower driving fan 952；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 position in the internal diameter for installing lower driving fan section in fan installation portion, the fan installation portion Blast superatmospheric between upper driving fan and lower driving fan so that go out and blast is formed in vane.
It is described go out vane include the vane upper shell 9111 and vane lower house 9112 being tightly connected, the vane lower casing Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board by multiple dowels 91122, 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 Into air-out gap wide at the top and narrow at the bottom, the bottom width in air-out gap is 0.8-1.5mm；The inner circumferential of the vane lower house is located at The lower section in air-out 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 installation portion are perpendicular, and go out shape between the axial direction of vane and horizontal direction Into the angle of 5-20 degree, and go out turn 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 It is dynamic in opposite direction.
It is provided with to adjust the adjusting part 96 that correspondence position goes out vane air-out speed in each described connecting tube, it is described Adjusting part includes the 3rd motor 961, the coaxially connected screw rod 962 with the 3rd motor output shaft, and connects with screw flight The valve plate 963 connect；The valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the middle part of above-below direction in connecting tube Position；The connecting tube internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, the 3rd motor Installing 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 Bottom is connected with a upper end towards the inclined baffle plate 9123 in vane direction is gone out, and conducting area is formed between the baffle plate and valve plate Adjustable airway.
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board 97 respectively.Institute State main part and be tightly connected composition for upper shell 91a and lower house 91b.
The main part upper end is connected with the air intake cover 94 of a semiellipse spherical shape, air intake cover and uniformly forms bar The air inlet of shape.
The electromagnet, elastic rod are connected to the top of the air intake cover.The main part upper end is provided with camera 913, the upper camera is electrically connected with control board.
The lower, outer perimeter of the fan installation portion is to be connected with and control on battery installation portion 9103, battery installation portion The battery 92 of circuit board electrical connection；
The lower end of the aircraft is provided with lower camera 9108, and the lower camera is electrically connected with control board.
The upper camera, lower camera can shoot acquisition aircraft opposite rail car, the position of electric automobile, can be by people Work operation remote control aircraft is accommodated on corresponding guide rail car by the first electromagnet, or is sucked by the second electromagnet In electric automobile roof；Corresponding guide rail car or electric automobile can also be accommodated to automatically by aircraft by machine vision technique On.
It is a circuit board installation cavity 9104, the control to be located at the top of battery installation portion on the fan installation portion Circuit board is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with a first annular cover plate 913；Institute The upper surface for stating circuit board installation cavity uniformly forms the fresh air inlet 9105 connected with fan installation portion, and the circuit board is installed The lateral wall of chamber uniformly forms vent 9106.
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.The similar four-axle aircraft of aircraft outward appearance, therefore with four-axle aircraft It is named, four go out the function that vane i.e. so-called " four axles " only plays regulation posture, therefore this aircraft substantially should be single shaft Aircraft.
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.
A small amount of air-flow of the fan installation portion enters from fresh air inlet and from vent discharge, plays scattered to control board Heat effect.
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint 9110 of rising and falling, each described undercarriage A undercarriage 93 is respectively connected with joint；The undercarriage is provided with to suck the second electromagnet in electromobile at top 936。
When aircraft does not work, aircraft is sucked in electromobile at top by the second electromagnet of undercarriage lower end On lid.
Embodiment 3
With reference to Figure 16 to Figure 17, the present embodiment also makes following improvement on the basis of embodiment 2：Go out vane inner circumferential described in each Holder joint 9110 of rising and falling is formed away from the position of connecting tube, a undercarriage is respectively connected with Holder joint of rising and falling described in each 93；The undercarriage includes the company for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling Adapter body 931, is slidably mounted on the sliding tube 932 in connection pipe body, and company is rotated close to Holder joint one end of rising and falling with connection pipe body The support bar 935 connect, is connected on support bar away from Holder joint one end of rising and falling to suck the second of electromobile at top Electromagnet 936, and the connecting rod 934 being connected respectively with rotation in the middle part of sliding tube middle part, support bar.
The connection pipe body forms hinged seat 9311, 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 9321, the slip pipe outer wall close to Holder joint one end of rising and falling Put and be connected with articulated joint 9322, 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 9312 passed through for articulated joint；The one end of the body of connecting tube 912 away from Holder joint of rising and falling is consolidated Surely sealing cap 933 is connected with, the inner of sealing cap, which is connected with spring locating rod 9331, the spring locating rod, to be arranged with Spring 937, the both ends of the spring is against between piston and sealing cap the inner respectively；Form and received in support bar on the support bar The connecting rod tank 9351 of the connecting rod is accommodated during the state of rising.
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.

Claims (9)

1. a kind of New-energy electric vehicle charging system, it is characterised in that：Include and be fixedly mounted on the multiple defeated of both sides of the road Electric pole, the transmission guide rail between each power transmission rod of road homonymy, rolls or is slidably mounted on the transmission guide rail And the guide rail car electrically connected with transmission guide rail, guide rail car lower end and the aircraft electrically connected with guide rail car can be rested in, and Be connected between electric automobile and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The transmission guide rail by two it is symmetrical, opening be spliced towards opposite U-shaped rail, spliced transmission guide rail Radial section is connected in I-shaped between two U-shaped rail by insulating materials；
The guide rail car lower end is connected with power supply connecting seat, and the power supply connecting seat includes the magnet being sequentially connected from top to bottom Fixed seat, current electrode seat, insulation board and current electrode plate；Current electrode seat, current electrode plate are electric with two U-shaped rail respectively Connection；
The current electrode seat lower end uniformly forms convex cavity under multiple circular groove shapes, and the current electrode seat is non-ferromagnetic material The metal of material is made, or is made up of nonmetallic materials；When current electrode seat is nonmetallic materials, the current electrode seat is extremely Few its lower surface convex chamber outer surface together with is coated with conductive layer；
The position that the magnet fixed seat lower end corresponds to convex cavity under each is connected with permanent magnet a, and permanent magnet a stretches into correspondence position Under in convex cavity；
The lower end correspondence of the insulation board forms the insulation of convex cavity lateral wall under insulating in the position of convex cavity under each Set；
The position of each insulation sleeve of correspondence forms appearance hole on the current electrode plate；
The first electromagnet sucked with permanent magnet a by magnetic force, the top of first electromagnet are installed at the top of the aircraft Portion is provided with the receiving electrode a for getting an electric shock and being connected with current electrode seated connection；It is located at the periphery of the first electromagnet at the top of the aircraft 3 elastic rods are connected with, the upper end of elastic rod is connected with the receiving electrode b that electrical connection is contacted with current electrode plate；It is described to receive Electrode a, receiving electrode b and wire are electrically connected, and first electromagnet is electrically connected with the control board of aircraft；
First electromagnet and the permanent magnet a of any position realize being electrically connected for receiving electrode a and current electrode after sucking Connect, then aircraft makes each elastic rod depart from there may be convex cavity lower surface under contact along the rotation of own central axis line, and The output electrode b of elastic rod bottom is set finally to contact electrical connection with current electrode plate.
2. a kind of New-energy electric vehicle charging system as claimed in claim 1, it is characterised in that：The guide rail car includes Overall is in the vehicle frame of opening up U-shaped, and vehicle frame top both sides are two symmetrically arranged vehicle frame plates, two vehicle frames More than 2 groups of driving wheel is rotatablely equipped with the inside of plate respectively, the axis of the driving wheel is horizontally disposed, two cars The position of each driving wheel of correspondence is provided with the motor for driving driving wheel to rotate on the outside of frame plate；
Roller is also separately installed with the inside of two vehicle frame plates, the U-shaped rail contact of the roller and homonymy is electrically connected；Institute State roller to be rotatably installed in the roller mount of U-shaped, the sliding bar set along frame width direction, institute are connected with the roller mount The sliding seat for being provided with and being slidably connected with sliding bar on vehicle frame plate is stated, is provided with and is used between the sliding bar and sliding seat Pushing rolling wheels are against the spring on U-shaped rail；Connecting rod is connected between the roller mount of homonymy；
Roller mount or connecting rod positioned at vehicle frame both sides are electrically connected by electric wire with current electrode seat, current electrode plate so that transmission of electricity Guide rail is electrically connected with power supply connecting seat formation.
3. a kind of New-energy electric vehicle charging system as claimed in claim 1, it is characterised in that：The electromobile at top One wire-winding unit is installed, the wire-winding unit includes the Wiinding cartridge of a upper end open, is rotatably installed in Wiinding cartridge Wire spool, and be connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through.
4. a kind of New-energy electric vehicle charging system as claimed in claim 1, it is characterised in that：The aircraft includes Main part, the main part includes the fan installation portion of tubular, be connected to fan installation portion periphery and with fan installation portion The connecting tube for four equidistant arrangements being connected, and be connected to each connecting tube outer end and be connected with correspondence position connecting tube Go 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 in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
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；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction 20 degree of angle, and go out the rotation side 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 To opposite；
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 the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described 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；The connecting tube Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
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.
5. a kind of New-energy electric vehicle charging system as claimed in claim 4, it is characterised in that：The electromagnet, elasticity Bar is connected to the top of the air intake cover.
6. a kind of New-energy electric vehicle charging system as claimed in claim 4, it is characterised in that：The main part upper end peace Equipped with upper camera, the upper camera is electrically connected with control board.
7. a kind of New-energy electric vehicle charging system as claimed in claim 4, it is characterised in that：The fan installation portion Lower, outer perimeter is to be connected with the battery electrically connected with control board on battery installation portion, battery installation portion；
The lower end of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board.
8. a kind of New-energy electric vehicle charging system as claimed in claim 4, it is characterised in that：Go out described in each in vane Week forms Holder joint of rising and falling away from the position of connecting tube, and a undercarriage is respectively connected with Holder joint of rising and falling described in each；Institute State undercarriage and include the connecting tube 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 Body, is slidably mounted on the sliding tube in connection pipe body, and the support bar being connected is rotated close to Holder joint one end of rising and falling with connection pipe body, It is connected on support bar away from Holder joint one end of rising and falling to suck the second electromagnet in electromobile at top, and difference The connecting rod being connected is rotated with the middle part of sliding tube middle part, support bar；
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；
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in running order Afterwards, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
9. a kind of New-energy electric vehicle charging system, it is characterised in that：Include and be fixedly mounted on the multiple defeated of both sides of the road Electric pole, the transmission guide rail between each power transmission rod of road homonymy, rolls or is slidably mounted on the transmission guide rail And the guide rail car electrically connected with transmission guide rail, guide rail car lower end and the aircraft electrically connected with guide rail car can be rested in, and Be connected between electric automobile and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The transmission guide rail by two it is symmetrical, opening be spliced towards opposite U-shaped rail, spliced transmission guide rail Radial section is connected in I-shaped between two U-shaped rail by insulating materials；
The guide rail car lower end is connected with power supply connecting seat, and the power supply connecting seat includes the magnet being sequentially connected from top to bottom Fixed seat, current electrode seat, insulation board and current electrode plate；Current electrode seat, current electrode plate are electric with two U-shaped rail respectively Connection；
The current electrode seat lower end uniformly forms convex cavity under multiple circular groove shapes, and the current electrode seat is non-ferromagnetic material The metal of material is made, or is made up of nonmetallic materials；When current electrode seat is nonmetallic materials, the current electrode seat is extremely Few its lower surface convex chamber outer surface together with is coated with conductive layer；
The position that the magnet fixed seat lower end corresponds to convex cavity under each is connected with permanent magnet a, and permanent magnet a stretches into correspondence position Under in convex cavity；
The lower end correspondence of the insulation board forms the insulation of convex cavity lateral wall under insulating in the position of convex cavity under each Set；
The position of each insulation sleeve of correspondence forms appearance hole on the current electrode plate；
The first electromagnet sucked with permanent magnet a by magnetic force, the top of first electromagnet are installed at the top of the aircraft Portion is provided with the receiving electrode a for getting an electric shock and being connected with current electrode seated connection；It is located at the periphery of the first electromagnet at the top of the aircraft 3 elastic rods are connected with, the upper end of elastic rod is connected with the receiving electrode b that electrical connection is contacted with current electrode plate；It is described to receive Electrode a, receiving electrode b and wire are electrically connected, and first electromagnet is electrically connected with the control board of aircraft；
First electromagnet and the permanent magnet a of any position realize being electrically connected for receiving electrode a and current electrode after sucking Connect, then aircraft makes each elastic rod depart from there may be convex cavity lower surface under contact along the rotation of own central axis line, and The output electrode b of elastic rod bottom is set finally to contact electrical connection with current electrode plate；
The guide rail car includes the overall vehicle frame in opening up U-shaped, and vehicle frame top both sides are two and are symmetrical arranged Vehicle frame plate, be rotatablely equipped with more than 2 groups of driving wheel on the inside of two vehicle frame plates respectively, the axis of the driving wheel is along water Square to setting, the position of each driving wheel of correspondence is provided with the drive for driving driving wheel to rotate on the outside of two vehicle frame plates Dynamic motor；
Roller is also separately installed with the inside of two vehicle frame plates, the U-shaped rail contact of the roller and homonymy is electrically connected；Institute State roller to be rotatably installed in the roller mount of U-shaped, the sliding bar set along frame width direction, institute are connected with the roller mount The sliding seat for being provided with and being slidably connected with sliding bar on vehicle frame plate is stated, is provided with and is used between the sliding bar and sliding seat Pushing rolling wheels are against the spring on U-shaped rail；Connecting rod is connected between the roller mount of homonymy；
Roller mount or connecting rod positioned at vehicle frame both sides are electrically connected by electric wire with current electrode seat, current electrode plate so that transmission of electricity Guide rail is electrically connected with power supply connecting seat formation；
The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes the coiling of a upper end open Box, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through；
The aircraft includes main part, and the main part includes the fan installation portion of tubular, is connected to fan installation Portion periphery and the connecting tube for four equidistant arrangements being connected with fan installation portion, and be connected to each connecting tube outer end and with What correspondence position connecting tube was connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed； It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
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；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction 20 degree of angle, and go out the rotation side 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 To opposite；
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 the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described 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；The connecting tube Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
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 electromagnet, elastic rod are connected to the top of the air intake cover；
The main part upper end is provided with camera, and the upper camera is electrically connected with control board;
The lower, outer perimeter of the fan installation portion is to be connected with battery installation portion, battery installation portion and control board electricity The battery of connection；
The lower end of the aircraft is provided with lower camera, and the lower camera is 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, which includes, to be fixedly connected with Holder joint of rising and falling and by Holder joint of rising and falling with going out vane The connection pipe body that inside is connected, is slidably mounted on the sliding tube in connection pipe body, with connection pipe body close to Holder joint one of rising and falling End rotates the support bar of connection, is connected on support bar away from Holder joint one end of rising and falling to suck in electromobile at top Second electromagnet, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar；
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；
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in running order Afterwards, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
CN201710488470.0A 2017-06-23 2017-06-23 A kind of New-energy electric vehicle charging system Expired - Fee Related CN107215232B (en)

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CN201711451201.3A CN108128200A (en) 2017-06-23 2017-06-23 A kind of New-energy electric vehicle charging system
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EP4292866A1 (en) * 2022-06-14 2023-12-20 Solér, Ola Vehicle power adaptor

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