CN107215230A - A kind of charging system for electric automobile - Google Patents

A kind of charging system for electric automobile Download PDF

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Publication number
CN107215230A
CN107215230A CN201710488146.9A CN201710488146A CN107215230A CN 107215230 A CN107215230 A CN 107215230A CN 201710488146 A CN201710488146 A CN 201710488146A CN 107215230 A CN107215230 A CN 107215230A
Authority
CN
China
Prior art keywords
guide rail
fan
vane
motor
installation portion
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
CN201710488146.9A
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Chinese (zh)
Other versions
CN107215230B (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.)
Ruan Fang
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 CN201711348760.1A priority Critical patent/CN108081987A/en
Priority to CN201711351795.0A priority patent/CN108099657A/en
Priority to CN201711351805.0A priority patent/CN107972518A/en
Priority to CN201710488146.9A priority patent/CN107215230B/en
Publication of CN107215230A publication Critical patent/CN107215230A/en
Application granted granted Critical
Publication of CN107215230B publication Critical patent/CN107215230B/en
Active 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
    • B60L53/60—Monitoring or controlling 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
    • B60L53/30—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
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/22—Operating mechanisms fluid
    • 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
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
    • B64C2025/125—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways into the fuselage, e.g. main landing gear pivotally retracting into or extending out of the fuselage
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention discloses a kind of charging system for electric automobile, include the multiple power transmission rods for being fixedly mounted on both sides of the road, transmission guide rail between each power transmission rod, the guide rail car for rolling or being slidably mounted on the transmission guide rail and electrically connected with transmission guide rail, the aircraft that can be rested on electric automobile and be electrically connected with electric automobile, and be connected between guide rail car and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile.Electric automobile is realized without stopping the function that can be charged, and coordinate guide rail car realization that the electric energy on transmission guide rail is transferred on electric automobile by aircraft, so electric automobile can depart from aircraft at any time in the case of fully charged or other, will not cause limitation to freely travelling for electric automobile.

Description

A kind of charging system for electric automobile
Technical field
The invention belongs to electric automobile corollary system field, and in particular to a kind of charging system for electric automobile.
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 charging system for electric automobile, including There are the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail between each power transmission rod rolls or slided peace The guide rail car electrically connected on the transmission guide rail and with transmission guide rail, can be rested on electric automobile and and electric automobile The aircraft of electrical connection, and be connected between guide rail car and aircraft electric energy is transferred into electronic vapour from transmission guide rail Wire on car；
The guide rail car lower end is rotatably connected to a winding mechanism that can be horizontally rotated；The winding mechanism includes one Bobbin winder bracket, the wire spool for the horizontally disposed non-metallic material of rotating shaft being rotatably connected on bobbin winder bracket, and installed in bobbin winder bracket Side and the coiling electric motor being connected with wire spool one end；
The wire spool both sides are provided with electrode a, and the both sides of the bobbin winder bracket are provided with the electrode a sliding contacts Electricity Federation with homonymy The electrode b connect, described wire one end is electrically connected with two electrode a.
Preferably：The bobbin winder bracket lower end is connected with an aircraft and stops plate, and the aircraft is stopped on plate The both sides of end correspondence bobbin winder bracket are fixedly connected between two defeated line plates, two defeated line plates is provided with two phases by axis of rotation The line-transmitting wheel of mutual engaged transmission, two line-transmitting wheel periphery symmetrical moldings have rolls the circle being connected between wire by stiction The driving concave surface of arc, the wire passes through between two driving concave surfaces.
Preferably：The line-transmitting wheel includes the driving wheel and driven pulley connected by meshed transmission gear；Two It is provided between individual defeated line plate fixed on the outside of a polygonal drive shaft being slidably connected with driving wheel, a defeated line plate One defeated line motor being fixedly connected with drive shaft one end is installed；One is provided between two defeated line plates to rotate with driven pulley And the cylinder-shaped shaft being slidably connected；The both sides of the driven pulley form two limiting plates, and the driving wheel both sides are limited in Between two limiting plates.
Preferably：The coiling electric motor, defeated line motor pass through wire and the control on guide rail car respectively Device is electrically connected, and the bobbin winder bracket upper end forms a lower limit projection, and the guide rail car lower end is fixedly connected with one and institute The mounting seat that bobbin winder bracket rotates connection is stated, the lower end of the mounting seat forms two with lower limit male cooperation to limit coiling The upper limit of frame slewing area is raised.
Preferably：The guide rail car includes sweep, and is fixedly connected on the lower sweep below sweep； The upper sweep upper left side front and rear portions are installed with two the first motors, and the upper upper right side front and rear portions of sweep are provided with two Individual the second motor that can be moved along guide rail car left and right directions；First motor, the second motor lower end have been respectively fixedly connected with The driving wheel being connected is rolled with both sides transmission guide rail；
The bar shaped perforation slided for the second motor is formed on the upper sweep along upper sweep left and right directions；Pacify on the upper sweep Equipped with to drive the second motor close to the pushing meanss of transmission guide rail；
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at slip In seat and horizontally disposed sliding bar, and it is fixedly connected on what is be fixedly connected on the outside of the second motor and with two sliding bar one end Motor fixing seat；Compression spring is installed between the sliding bar and sliding seat；
The lower sweep both sides are connected with by axis of rotation and roll the roller that electrically connect with transmission guide rail so that the rotating shaft and The transmission guide rail electrical connection of homonymy, while rotating shaft is electrically connected with the electrode b on bobbin winder bracket.
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：First electromagnet, first electromagnet are installed at the top of the air intake cover of the aircraft Top camera is installed；
The upper camera and the first electromagnet are electrically connected with control board respectively；
The aircraft stops plate lower end and is provided with cross telltale mark；The aircraft stops plate at least its underpart The permanent magnet that one electromagnet is sucked by magnetic force.
Preferably：The lower, outer perimeter of the fan installation portion is charging transmitter module installation portion, charging transmitting mould The charging transmitter module electrically connected with control board is connected with block installation portion；
The lower carriage bottom of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board；
The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module.
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 provides another charging system for electric automobile, includes the multiple transmissions of electricity for being fixedly mounted on both sides of the road Bar, the transmission guide rail between each power transmission rod is rolled or is slidably mounted on the transmission guide rail and and transmission guide rail The guide rail car of electrical connection, the aircraft that can be rested on electric automobile and be electrically connected with electric automobile, and it is connected to guide rail Between car and aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The guide rail car lower end is rotatably connected to a winding mechanism that can be horizontally rotated；The winding mechanism includes one Bobbin winder bracket, the wire spool for the horizontally disposed non-metallic material of rotating shaft being rotatably connected on bobbin winder bracket, and installed in bobbin winder bracket Side and the coiling electric motor being connected with wire spool one end；
The wire spool both sides are provided with electrode a, and the both sides of the bobbin winder bracket are provided with the electrode a sliding contacts Electricity Federation with homonymy The electrode b connect, described wire one end is electrically connected with two electrode a；
The bobbin winder bracket lower end is connected with an aircraft and stops plate, and the aircraft stops the both sides of plate upper end correspondence bobbin winder bracket It is fixedly connected with the defeated line for being provided with two intermeshing transmissions between two defeated line plates, two defeated line plates by axis of rotation Wheel, two line-transmitting wheel periphery symmetrical moldings have the driving concave surface for rolling the circular arc being connected by stiction between wire, The wire passes through between two driving concave surfaces；
The line-transmitting wheel includes the driving wheel and driven pulley connected by meshed transmission gear；It is provided between two defeated line plates One and drive shaft are installed with the outside of one polygonal drive shaft for being slidably connected with driving wheel, a defeated line plate The defeated line motor that one end is fixedly connected；One cylinder for rotating and being slidably connected with driven pulley is installed between two defeated line plates Rotating shaft；The both sides of the driven pulley form two limiting plates, and the driving wheel both sides are limited between two limiting plates；
The coiling electric motor, defeated line motor are electrically connected by wire with the controller on guide rail car respectively, the coiling Frame upper end forms a lower limit projection, and the guide rail car lower end is fixedly connected with one and rotates what is be connected with the bobbin winder bracket Mounting seat, the lower end of the mounting seat forms two with lower limit male cooperation to limit the upper limit of bobbin winder bracket slewing area It is raised；
The guide rail car includes sweep, and is fixedly connected on the lower sweep below sweep；The upper sweep upper left side Front and rear portions are installed with two the first motors, and the upper upper right side front and rear portions of sweep are provided with two can be left along guide rail car Second motor of right direction movement；First motor, the second motor lower end have been respectively fixedly connected with to be rolled with both sides transmission guide rail The driving wheel of dynamic connection；
The bar shaped perforation slided for the second motor is formed on the upper sweep along upper sweep left and right directions；Pacify on the upper sweep Equipped with to drive the second motor close to the pushing meanss of transmission guide rail；
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at slip In seat and horizontally disposed sliding bar, and it is fixedly connected on what is be fixedly connected on the outside of the second motor and with two sliding bar one end Motor fixing seat；Compression spring is installed between the sliding bar and sliding seat；
The lower sweep both sides are connected with by axis of rotation and roll the roller that electrically connect with transmission guide rail so that the rotating shaft and The transmission guide rail electrical connection of homonymy, while rotating shaft is electrically connected with the electrode b on bobbin winder bracket；
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；
It is provided with the top of the air intake cover of the aircraft at the top of the first electromagnet, first electromagnet and shooting is installed Head；
The upper camera and the first electromagnet are electrically connected with control board respectively；
The aircraft stops plate lower end and is provided with cross telltale mark；The aircraft stops plate at least its underpart The permanent magnet that one electromagnet is sucked by magnetic force；
The lower, outer perimeter of the fan installation portion for charging transmitter module installation portion, charging transmitter module installation portion on be connected with The charging transmitter module of control board electrical connection；
The lower carriage bottom of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board；
The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module；
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；
The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board installation cavity, the control electricity Road plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with a first annular cover plate；The electricity The upper surface of road plate installation cavity uniformly forms the fresh air inlet connected with fan installation portion, the outside of the circuit board installation cavity Wall uniformly forms vent.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention on transmission guide rail by travelling and keeping With the guide rail car of electric automobile identical travel speed, the aircraft being connected with guide rail car wire is coordinated to come to be electronic in traveling Automobile charges, and realizes electric automobile and coordinates guide rail car to realize without stopping the function that can be charged, and by aircraft Electric energy on transmission guide rail is transferred on electric automobile, such electric automobile can be at any time in the case of fully charged or other Depart from aircraft, limitation will not be caused to freely travelling for electric automobile.With existing in the electronic of roof setting pantograph Bus is compared, and the present invention need to only set a charging receiving module in electromobile at top（Such as the common contact of prior art Electrode or wireless charging receiving module that formula is electrically connected）, the outward appearance of not too large influence electric automobile, and be easy to existing electricity Electrical automobile is transformed.
The aircraft passes through the first electromagnet in off working state（Iron core）Suck and stopped in aircraft below plate Permanent magnet on, aircraft work when, the first electromagnet be powered produce with the reverse magnetic field of permanent magnet make aircraft and aircraft Plate is stopped to depart from.
When there is electric automobile to need charging, coiling electric motor driving wire spool, which is rotated, releases wire, while defeated line motor drives Dynamic line-transmitting wheel, which is rotated, ensures that wire can be released quick smoothly, it is to avoid wire is wrapped on bobbin winder bracket during releasing；Then Aircraft departs from guide rail car and flown on electric automobile, and aircraft is sucked in electronic vapour by the second electromagnet of undercarriage lower end On the metal car shell of roof.After charging electric vehicle is finished, aircraft flies back to aircraft and stopped below plate, while coiling is electric Machine and defeated line motor, which are rotated backward, to be made on wire wraparound wire spool.Because two line-transmitting wheels can turn along drive shaft, cylinder respectively Axle is moved axially, and so when wire is significantly greater than opposite side in the thickness that the side of wire spool is wound, wire can be towards another Slideslip, now line-transmitting wheel can produce the movement of adaptability, it is ensured that it is more uniform that wire is wound on wire spool.
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.
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.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2, Fig. 3 are the structural representations of aircraft and guide rail car.
Fig. 4, Fig. 5 are the decomposition texture schematic diagrams of guide rail car.
Fig. 6 is the structural representation of aircraft stopped status.
Fig. 7 is the structural representation of aircraft flight state.
Fig. 8 is the cross section structure diagram of aircraft.
Fig. 9 is Fig. 8 A portions schematic enlarged-scale view.
Figure 10 is Fig. 8 B portions schematic enlarged-scale view.
The structural representation of each part that Figure 11 is upper shell and is connected with upper shell.
Figure 12 is the structural representation of lower housing section.
Figure 13 is the cross section structure diagram of lower housing section.
Figure 14 is the structural representation of air intake cover.
Figure 15 is the decomposition texture schematic diagram of undercarriage part.
Figure 16 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；5th, wire；9th, aircraft；41st, upper sweep； 411st, bar shaped is perforated；412nd, driving wheel；414th, the first motor；415th, the second motor；416th, motor fixing seat；417th, sliding seat； 418th, sliding bar；42nd, lower sweep；422nd, roller；423rd, mounting seat；43rd, bobbin winder bracket；44th, wire spool；441st, coiling electric motor； 45th, aircraft stops plate；46th, line-transmitting wheel；461st, driving wheel；462nd, driven pulley；463rd, defeated line motor；464th, drive shaft；465、 Cylinder-shaped shaft；466th, defeated line plate；91st, main part；91a, upper shell；91b, lower house；910th, fan installation portion；9101st, on Support；9102nd, lower carriage；9103rd, charge transmitter module installation portion；9104th, circuit board installation cavity；9105th, fresh air inlet；9106、 Vent；9107th, lower camera；911st, vane is gone out；9110th, rise and fall Holder joint；9111st, vane upper shell；9112nd, vane lower casing Body；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；92nd, charge transmitter module；93rd, undercarriage； 931st, connection pipe body；9311st, hinged seat；9312nd, strip shape gob；932nd, sliding tube；9321st, piston；9322nd, articulated joint；933rd, seal Mouth cap；9331st, spring locating rod；934th, connecting rod；935th, support bar；9351st, connecting rod tank；936th, the second electromagnet；937th, bullet Spring；94th, air intake cover；941st, the first electromagnet；942nd, upper camera；951st, upper driving fan；952nd, lower driving fan；96th, adjust Save component；961st, the 3rd motor；962nd, screw rod；963rd, valve plate；97th, control board.
Embodiment
Embodiment 1
According to Fig. 1 to 5, the present embodiment is a kind of charging system for electric automobile, includes and is fixedly mounted on both sides of the road Multiple power transmission rods 1, the transmission guide rail 2 between each power transmission rod, roll or be slidably mounted on the transmission guide rail and The guide rail car 4 electrically connected with transmission guide rail, the aircraft 9 that can be rested on electric automobile and be electrically connected with electric automobile, with And be connected between guide rail car and aircraft to the wire 5 that is transferred to electric energy from transmission guide rail on electric automobile.
Two groups are at least connected between two groups of transmission guide rails of both sides of the road is used for the commutation guide rail that guide rail car commutates 3；The transmission guide rail, commutation guide rail include two tracks be arrangeding in parallel respectively, and each track at least includes a use In guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part phase between two tracks To setting.
The guide rail car lower end is rotatably connected to a winding mechanism that can be horizontally rotated；The winding mechanism includes One bobbin winder bracket 43, the wire spool 44 for the horizontally disposed non-metallic material of rotating shaft being rotatably connected on bobbin winder bracket, and install Bobbin winder bracket side and with wire spool one end be connected coiling electric motor 441.
Because the speed during electric automobile during traveling between guide rail car has differences unavoidably, especially add in electric automobile Speed, in moderating process, therefore the mode that the bobbin winder bracket is designed as horizontally rotating, it is ensured that wire and winding mechanism contact position by To pull that degree is smaller, the service life of extension lead.
The wire spool both sides are provided with electrode a, and the both sides of the bobbin winder bracket are provided with the electrode a sliding contacts with homonymy The electrode b electrically connected, described wire one end is electrically connected with two electrode a.The wire refers to including 2 in whole line, wire Root electric wire.
The bobbin winder bracket lower end is connected with an aircraft and stops plate 45, and the aircraft stops plate upper end correspondence bobbin winder bracket Both sides be fixedly connected between two defeated line plates 466, two defeated line plates by axis of rotation be provided with two intermeshing biography Dynamic line-transmitting wheel 46, two line-transmitting wheel periphery symmetrical moldings have rolls the circular arc being connected between wire by stiction Concave surface is driven, the wire passes through between two driving concave surfaces.
The line-transmitting wheel includes the driving wheel 461 and driven pulley 462 connected by meshed transmission gear；Two defeated line plates Between a polygonal drive shaft 464 being slidably connected with driving wheel is installed, be fixedly mounted on the outside of a defeated line plate There is a defeated line motor 463 being fixedly connected with drive shaft one end；One is provided between two defeated line plates to rotate with driven pulley And the cylinder-shaped shaft 465 being slidably connected；The both sides of the driven pulley form two limiting plates, the driving wheel both sides limitation Between two limiting plates.
When there is electric automobile to need charging, coiling electric motor driving wire spool, which is rotated, releases wire, while defeated line motor drives Dynamic line-transmitting wheel, which is rotated, ensures that wire can be released quick smoothly, it is to avoid wire is wrapped on bobbin winder bracket during releasing；Then Aircraft departs from guide rail car and flown on electric automobile, and aircraft is sucked in electronic vapour by the second electromagnet of undercarriage lower end On the metal car shell of roof.After charging electric vehicle is finished, aircraft flies back to aircraft and stopped below plate, while coiling is electric Machine and defeated line motor, which are rotated backward, to be made on wire wraparound wire spool.Because two line-transmitting wheels can turn along drive shaft, cylinder respectively Axle is moved axially, and so when wire is significantly greater than opposite side in the thickness that the side of wire spool is wound, wire can be towards another Slideslip, now line-transmitting wheel can produce the movement of adaptability, it is ensured that it is more uniform that wire is wound on wire spool.
The coiling electric motor, defeated line motor are electrically connected by wire with the controller on guide rail car respectively, described Bobbin winder bracket upper end forms a lower limit projection, and the guide rail car lower end, which is fixedly connected with one and rotated with the bobbin winder bracket, to be connected The mounting seat 423 connect, the lower end of the mounting seat forms two with lower limit male cooperation to limit bobbin winder bracket slewing area Upper limit it is raised.
Because coiling electric motor, defeated line motor are electrically connected by wire with the controller on guide rail car respectively, in order to Avoid wire from being torn, therefore set upper and lower spacing preiection to limit the slewing area of bobbin winder bracket.
The guide rail car includes sweep 41, and is fixedly connected on the lower sweep 42 below sweep；It is described to get on the bus Plate upper left side front and rear portions are installed with two the first motors, and the upper upper right side front and rear portions of sweep are provided with two being capable of edge Second motor of guide rail car left and right directions movement；First motor, the second motor lower end have been respectively fixedly connected with defeated with both sides Conductance rail rolls the driving wheel 412 of connection.
The bar shaped perforation 411 slided for the second motor 415 is formed on the upper sweep along upper sweep left and right directions；It is described The pushing meanss for driving the second motor close to transmission guide rail are installed on upper sweep.
The pushing meanss include being fixedly connected on the sliding seat 417 of the upper both sides of perforating in bar shaped of sweep, the company of slip Be connected in sliding seat and horizontally disposed sliding bar 418, and be fixedly connected on the outside of the second motor and with two sliding bars one Hold the motor fixing seat 416 being fixedly connected；Compression spring is installed between the sliding bar and sliding seat.
The lower sweep both sides are connected with by axis of rotation and roll the roller 422 electrically connected with transmission guide rail so that institute Rotating shaft is stated to electrically connect with the transmission guide rail of homonymy.The lower sweep is non-conducting material, institute at least with the junction of rotating shaft The rotating shaft for stating lower sweep both sides is connected respectively by electric wire with two electrode b of bobbin winder bracket both sides so that the fax of transmission guide rail It is defeated on wire.
The driving wheel coordinates to roll with the vertical plate portion of the track to be connected, the horizontal plate part of the roller then with track Rolling is electrically connected, and the roller is metal wheel, and each side of lower sweep sets 2-3 roller, is so on the one hand beneficial to guide rail car Steady traveling on transmission guide rail, on the other hand ensure that good between roller and transmission guide rail electrically connect.Further Say, can be connected between roller and rotating shaft by bearing, then also form Electricity Federation between metal material inner ring, outer ring and the ball of bearing Connect, and there is lubricant medium between ball and inner ring, outer ring and be likely to result in larger resistance, therefore guide rail car passes through 2-3 per side Roller is rolled with transmission guide rail and is connected, and ensure that the continuity transmitted electricity between guide rail car and transmission guide rail, it is ensured that stable electricity Pressure, electric current.
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 second design of electrical motor of side is on guide rail car It can be moved along guide rail car left and right directions so that when driving into the track of circular arc the driving wheel of both sides can keep guide rail car Keep offseting with two siding tracks.
Embodiment 2
With reference to shown in Fig. 6 to Figure 14, 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.
First electromagnet 941 is installed, the top of first electromagnet is installed at the top of the air intake cover of the aircraft There is upper camera 942.The upper camera and the first electromagnet are electrically connected with control board respectively.
The aircraft stops plate lower end and is provided with cross telltale mark；The aircraft stops plate at least its underpart The permanent magnet sucked with the first electromagnet by magnetic force.
The lower, outer perimeter of the fan installation portion is on charging transmitter module installation portion 9103, charging transmitter module installation portion It is connected with the charging transmitter module 92 electrically connected with control board；
The lower carriage bottom of the aircraft is provided with lower camera 9107, and the lower camera is electrically connected with control board； The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module.
The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board installation cavity 9104, institute Control board is stated in circuit board installation cavity, the circuit board installation cavity lower end is connected with a first annular cover plate 913；The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet 9105 connected with fan installation portion, the circuit The lateral wall of plate installation cavity 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.
First electromagnet 941 is installed, the top of first electromagnet is installed at the top of the air intake cover of the aircraft There is upper camera 942；The upper camera and the first electromagnet are electrically connected with control board respectively；The wire spool is installed Groove lower end is fixedly connected with aircraft and stops plate 44；Aircraft stops plate lower end and forms cross telltale mark 441；It is described The position that aircraft stops plate lower end correspondence telltale mark is connected with the permanent magnet sucked with the first electromagnet by magnetic force.
The aircraft passes through the first electromagnet in off working state（Iron core）Suck and stopped in aircraft below plate Permanent magnet on, aircraft work when, the first electromagnet be powered produce with the reverse magnetic field of permanent magnet make aircraft and aircraft Plate is stopped to depart from.The upper camera is used for the position for judging aircraft opposite rail car, in order to which aircraft can pass through standard Really rest on guide rail car.The upper camera shoots the position for obtaining aircraft opposite rail car, can be long-range by artificial operation Manipulate aircraft be accommodated to by the first electromagnet on corresponding guide rail car, can also by machine vision technique by aircraft from It is dynamic to be accommodated on corresponding guide rail car.
The lower, outer perimeter of the fan installation portion is on charging transmitter module installation portion 9103, charging transmitter module installation portion It is connected with the charging transmitter module 92 electrically connected with control board；The lower carriage bottom of the aircraft is provided with lower camera 9107, the lower camera is electrically connected with control board；The electromobile at top is provided with to be electrically connected with charging transmitter module The charging receiving module connect.
Described charging transmitter module, charging receiving module can be the electrodes of contact or by wireless charging Power technology carries out the coil of power transmission.
The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board installation cavity 9104, institute Control board is stated in circuit board installation cavity, the circuit board installation cavity lower end is connected with a first annular cover plate 913；The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet 9105 connected with fan installation portion, the circuit The lateral wall of plate installation cavity uniformly forms vent 9106.
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 there is electric automobile to need charging, coiling electric motor driving wire spool, which is rotated, releases wire, while aircraft departs from Guide rail car is simultaneously flown on electric automobile, and aircraft sucks the gold in electromobile at top by the second electromagnet of undercarriage lower end Belong on car shell.
Embodiment 3
With reference to Figure 15 to Figure 16, 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 (10)

1. a kind of charging system for electric automobile, it is characterised in that：Include the multiple power transmission rods for being fixedly mounted on both sides of the road, pacify Transmission guide rail between each power transmission rod, rolls or is slidably mounted on the transmission guide rail and electrically connected with transmission guide rail Guide rail car, the aircraft that can be rested on electric automobile and be electrically connected with electric automobile, and be connected to guide rail car with fly Between row device to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The guide rail car lower end is rotatably connected to a winding mechanism that can be horizontally rotated；The winding mechanism includes one Bobbin winder bracket, the wire spool for the horizontally disposed non-metallic material of rotating shaft being rotatably connected on bobbin winder bracket, and installed in bobbin winder bracket Side and the coiling electric motor being connected with wire spool one end；
The wire spool both sides are provided with electrode a, and the both sides of the bobbin winder bracket are provided with the electrode a sliding contacts Electricity Federation with homonymy The electrode b connect, described wire one end is electrically connected with two electrode a.
2. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：The bobbin winder bracket lower end is connected with one Individual aircraft stops plate, and the both sides that the aircraft stops plate upper end correspondence bobbin winder bracket are fixedly connected with two defeated line plates, two The line-transmitting wheel of two intermeshing transmissions is installed by axis of rotation, two line-transmitting wheel periphery symmetrical moldings have between defeated line plate The driving concave surface of circular arc being connected is rolled by stiction between wire, the wire from two driving concave surfaces it Between pass through.
3. a kind of charging system for electric automobile as claimed in claim 2, it is characterised in that：The line-transmitting wheel includes by tooth Take turns the driving wheel and driven pulley being connected by meshing transmission；Be provided between two defeated line plates one with driving wheel be slidably connected it is polygon A defeated line motor being fixedly connected with drive shaft one end is installed with the outside of the drive shaft of shape, a defeated line plate；Two One cylinder-shaped shaft for rotating and being slidably connected with driven pulley is installed between individual defeated line plate；The both sides shaping of the driven pulley There are two limiting plates, the driving wheel both sides are limited between two limiting plates.
4. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：The coiling electric motor, defeated line motor Electrically connected respectively by wire with the controller on guide rail car, it is convex that the bobbin winder bracket upper end forms a lower limit Rise, the guide rail car lower end is fixedly connected with one and rotates the mounting seat being connected, the lower end of the mounting seat with the bobbin winder bracket It is raised to limit the upper limit of bobbin winder bracket slewing area with lower limit male cooperation to form two.
5. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：The guide rail car, which includes, gets on the bus Plate, and it is fixedly connected on the lower sweep below sweep；The upper sweep upper left side front and rear portions are installed with two first Motor, the upper upper right side front and rear portions of sweep are provided with two the second motors that can be moved along guide rail car left and right directions；It is described First motor, the second motor lower end are respectively fixedly connected with rolls the driving wheel being connected with both sides transmission guide rail；
The bar shaped perforation slided for the second motor is formed on the upper sweep along upper sweep left and right directions；Pacify on the upper sweep Equipped with to drive the second motor close to the pushing meanss of transmission guide rail；
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at slip In seat and horizontally disposed sliding bar, and it is fixedly connected on what is be fixedly connected on the outside of the second motor and with two sliding bar one end Motor fixing seat；Compression spring is installed between the sliding bar and sliding seat；
The lower sweep both sides are connected with by axis of rotation and roll the roller that electrically connect with transmission guide rail so that the rotating shaft and The transmission guide rail electrical connection of homonymy, while rotating shaft is electrically connected with the electrode b on bobbin winder bracket.
6. a kind of charging system for electric automobile as claimed in claim 1, it is characterised in that：The aircraft includes main body Portion, the main part includes the fan installation portion of tubular, is connected to fan installation portion periphery and is connected with fan installation portion The connecting tube of four logical equidistant arrangements, and be connected to each connecting tube outer end and with going out that correspondence position connecting tube is connected Vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed； It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior Footpath is more than 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.
7. a kind of charging system for electric automobile as claimed in claim 6, it is characterised in that：The top of the air intake cover of the aircraft Portion is provided with the top of the first electromagnet, first electromagnet and is provided with camera；
The upper camera and the first electromagnet are electrically connected with control board respectively；
The aircraft stops plate lower end and is provided with cross telltale mark；The aircraft stops plate at least its underpart The permanent magnet that one electromagnet is sucked by magnetic force.
8. a kind of charging system for electric automobile as claimed in claim 6, it is characterised in that：Outside the bottom of the fan installation portion Week is that the charging transmitting electrically connected with control board is connected with charging transmitter module installation portion, charging transmitter module installation portion Module；
The lower carriage bottom of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board；
The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module.
9. a kind of charging system for electric automobile as claimed in claim 6, it is characterised in that：Go out vane inner circumferential described in each remote The position of connecting tube forms Holder joint of rising and falling, and a undercarriage is respectively connected with Holder joint of rising and falling described in each；It is described to rise and fall Frame includes the connection pipe body for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling, and slides Sliding tube in connection pipe body, rotates the support bar being connected close to Holder joint one end of rising and falling with connection pipe body, is connected to Away from Holder joint one end of rising and falling sucking the second electromagnet in electromobile at top on support bar, and respectively with slip The connecting rod of connection is rotated in the middle part of pipe, in the middle part of 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.
10. a kind of charging system for electric automobile, it is characterised in that：Include the multiple power transmission rods for being fixedly mounted on both sides of the road, Transmission guide rail between each power transmission rod, rolls or is slidably mounted on the transmission guide rail and be electrically connected with transmission guide rail The guide rail car connect, the aircraft that can be rested on electric automobile and be electrically connected with electric automobile, and be connected to guide rail car with Between aircraft to the wire that is transferred to electric energy from transmission guide rail on electric automobile；
The guide rail car lower end is rotatably connected to a winding mechanism that can be horizontally rotated；The winding mechanism includes one Bobbin winder bracket, the wire spool for the horizontally disposed non-metallic material of rotating shaft being rotatably connected on bobbin winder bracket, and installed in bobbin winder bracket Side and the coiling electric motor being connected with wire spool one end；
The wire spool both sides are provided with electrode a, and the both sides of the bobbin winder bracket are provided with the electrode a sliding contacts Electricity Federation with homonymy The electrode b connect, described wire one end is electrically connected with two electrode a；
The bobbin winder bracket lower end is connected with an aircraft and stops plate, and the aircraft stops the both sides of plate upper end correspondence bobbin winder bracket It is fixedly connected with the defeated line for being provided with two intermeshing transmissions between two defeated line plates, two defeated line plates by axis of rotation Wheel, two line-transmitting wheel periphery symmetrical moldings have the driving concave surface for rolling the circular arc being connected by stiction between wire, The wire passes through between two driving concave surfaces；
The line-transmitting wheel includes the driving wheel and driven pulley connected by meshed transmission gear；It is provided between two defeated line plates One and drive shaft are installed with the outside of one polygonal drive shaft for being slidably connected with driving wheel, a defeated line plate The defeated line motor that one end is fixedly connected；One cylinder for rotating and being slidably connected with driven pulley is installed between two defeated line plates Rotating shaft；The both sides of the driven pulley form two limiting plates, and the driving wheel both sides are limited between two limiting plates；
The coiling electric motor, defeated line motor are electrically connected by wire with the controller on guide rail car respectively, the coiling Frame upper end forms a lower limit projection, and the guide rail car lower end is fixedly connected with one and rotates what is be connected with the bobbin winder bracket Mounting seat, the lower end of the mounting seat forms two with lower limit male cooperation to limit the upper limit of bobbin winder bracket slewing area It is raised；
The guide rail car includes sweep, and is fixedly connected on the lower sweep below sweep；The upper sweep upper left side Front and rear portions are installed with two the first motors, and the upper upper right side front and rear portions of sweep are provided with two can be left along guide rail car Second motor of right direction movement；First motor, the second motor lower end have been respectively fixedly connected with to be rolled with both sides transmission guide rail The driving wheel of dynamic connection；
The bar shaped perforation slided for the second motor is formed on the upper sweep along upper sweep left and right directions；Pacify on the upper sweep Equipped with to drive the second motor close to the pushing meanss of transmission guide rail；
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at slip In seat and horizontally disposed sliding bar, and it is fixedly connected on what is be fixedly connected on the outside of the second motor and with two sliding bar one end Motor fixing seat；Compression spring is installed between the sliding bar and sliding seat；
The lower sweep both sides are connected with by axis of rotation and roll the roller that electrically connect with transmission guide rail so that the rotating shaft and The transmission guide rail electrical connection of homonymy, while rotating shaft is electrically connected with the electrode b on bobbin winder bracket；
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；
It is provided with the top of the air intake cover of the aircraft at the top of the first electromagnet, first electromagnet and shooting is installed Head；
The upper camera and the first electromagnet are electrically connected with control board respectively；
The aircraft stops plate lower end and is provided with cross telltale mark；The aircraft stops plate at least its underpart The permanent magnet that one electromagnet is sucked by magnetic force；
The lower, outer perimeter of the fan installation portion for charging transmitter module installation portion, charging transmitter module installation portion on be connected with The charging transmitter module of control board electrical connection；
The lower carriage bottom of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board；
The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module；
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；
The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board installation cavity, the control electricity Road plate is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with a first annular cover plate；The electricity The upper surface of road plate installation cavity uniformly forms the fresh air inlet connected with fan installation portion, the outside of the circuit board installation cavity Wall uniformly forms vent.
CN201710488146.9A 2017-06-23 2017-06-23 A kind of charging system for electric automobile Active CN107215230B (en)

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CN201711348760.1A CN108081987A (en) 2017-06-23 2017-06-23 A kind of charging system for electric automobile
CN201711351795.0A CN108099657A (en) 2017-06-23 2017-06-23 A kind of charging system for electric automobile
CN201711351805.0A CN107972518A (en) 2017-06-23 2017-06-23 A kind of charging system for electric automobile
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109229389A (en) * 2018-08-30 2019-01-18 西安三翼航空科技有限公司 A kind of multi-functional mission payload hanger of unmanned plane
CN114180062A (en) * 2021-12-31 2022-03-15 山东省物化探勘查院 Multifunctional surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information
EP4292866A1 (en) * 2022-06-14 2023-12-20 Solér, Ola Vehicle power adaptor
CN118124431A (en) * 2024-04-07 2024-06-04 苏州华仕通科技有限公司 New energy automobile charging station

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1156098A (en) * 1996-02-02 1997-08-06 张凯文 Power supply system for trolley bus
CN102490619A (en) * 2011-12-14 2012-06-13 西南交通大学 Charging system in driving state of electric cars
CN202737496U (en) * 2012-06-11 2013-02-13 叶明旭 Automatic charging system for electric automobile
KR20130050003A (en) * 2011-11-07 2013-05-15 현대자동차주식회사 Vehicle charging system for complex building
CN103935266A (en) * 2014-04-08 2014-07-23 杨有岳 Traveling vehicle power supply device
CN105244971A (en) * 2015-11-10 2016-01-13 蔡淑彬 Electric vehicle automatic charging system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1156098A (en) * 1996-02-02 1997-08-06 张凯文 Power supply system for trolley bus
KR20130050003A (en) * 2011-11-07 2013-05-15 현대자동차주식회사 Vehicle charging system for complex building
CN102490619A (en) * 2011-12-14 2012-06-13 西南交通大学 Charging system in driving state of electric cars
CN202737496U (en) * 2012-06-11 2013-02-13 叶明旭 Automatic charging system for electric automobile
CN103935266A (en) * 2014-04-08 2014-07-23 杨有岳 Traveling vehicle power supply device
CN105244971A (en) * 2015-11-10 2016-01-13 蔡淑彬 Electric vehicle automatic charging system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109229389A (en) * 2018-08-30 2019-01-18 西安三翼航空科技有限公司 A kind of multi-functional mission payload hanger of unmanned plane
CN114180062A (en) * 2021-12-31 2022-03-15 山东省物化探勘查院 Multifunctional surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information
CN114180062B (en) * 2021-12-31 2022-08-26 山东省物化探勘查院 Multifunctional surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information
EP4292866A1 (en) * 2022-06-14 2023-12-20 Solér, Ola Vehicle power adaptor
CN118124431A (en) * 2024-04-07 2024-06-04 苏州华仕通科技有限公司 New energy automobile charging station

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CN107972518A (en) 2018-05-01

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Effective date of registration: 20211118

Address after: 236600 38, Jianyi village, yuanqiang Town, Taihe County, Fuyang City, Anhui Province

Patentee after: Ruan Fang

Address before: 325000 building 3, area a, 329 Jinhai Third Road, Wenzhou Economic and Technological Development Zone, Zhejiang Province

Patentee before: WENZHOU RUICHU TECHNOLOGY Co.,Ltd.