CN107139767B - A kind of electric car electric energy shared system and sharing method - Google Patents

A kind of electric car electric energy shared system and sharing method Download PDF

Info

Publication number
CN107139767B
CN107139767B CN201710489017.1A CN201710489017A CN107139767B CN 107139767 B CN107139767 B CN 107139767B CN 201710489017 A CN201710489017 A CN 201710489017A CN 107139767 B CN107139767 B CN 107139767B
Authority
CN
China
Prior art keywords
aircraft
vane
fan
electricity
electric
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.)
Active
Application number
CN201710489017.1A
Other languages
Chinese (zh)
Other versions
CN107139767A (en
Inventor
江佳辉
虞丽丽
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.)
Lin Weixin
Original Assignee
Hangzhou Power Spectrum 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 Hangzhou Power Spectrum Technology Co Ltd filed Critical Hangzhou Power Spectrum Technology Co Ltd
Priority to CN201710489017.1A priority Critical patent/CN107139767B/en
Priority to CN201810101785.XA priority patent/CN108312869B/en
Priority to CN201810101355.8A priority patent/CN108248435B/en
Priority to CN201810101354.3A priority patent/CN108312868B/en
Publication of CN107139767A publication Critical patent/CN107139767A/en
Application granted granted Critical
Publication of CN107139767B publication Critical patent/CN107139767B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • B60L53/10—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
    • B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • 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
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/028—Micro-sized aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2240/00—Control parameters of input or output; Target parameters
    • B60L2240/70—Interactions with external data bases, e.g. traffic centres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • 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
    • 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
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles
    • Y02T90/167—Systems integrating technologies related to power network operation and communication or information technologies for supporting the interoperability of electric or hybrid vehicles, i.e. smartgrids as interface for battery charging of electric vehicles [EV] or hybrid vehicles [HEV]
    • 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
    • Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
    • Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
    • Y04S30/00—Systems supporting specific end-user applications in the sector of transportation
    • Y04S30/10—Systems supporting the interoperability of electric or hybrid vehicles
    • Y04S30/12—Remote or cooperative charging

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention discloses a kind of electric car electric energy shared system and sharing methods, the system comprises there are two the aircraft that can be rested in respectively on two electric vehicles, and be connected between two aircraft to the conducting wire by the electrical energy transportation of an electric vehicle to another electric vehicle；The aircraft is equipped with the transmission of electricity connector electrically connected with conducting wire；Further include being mounted on electric vehicle to connect electric connection socket with what transmission of electricity connector electrically connected, the accumulator of wiring connecting seat and electric vehicle electrically connects.The electric vehicle that the electric energy of the electric vehicle of electricity abundance is shared with not enough power supply by least two aircraft by the present invention charges, and solves the problems, such as electric automobile during traveling process midway not enough power supply.

Description

A kind of electric car electric energy shared system and sharing method
Technical field
The invention belongs to electric vehicle corollary system fields, and in particular to a kind of electric car electric energy shared system.
Background technology
With popularizing for electric vehicle, the inconvenient problem of electric vehicle charging also increasingly highlights；Purchase electric vehicle at present User be typically limited to only city use on and off duty, need for a long time at a distance outgoing user then still tend to use fuel oil Vehicle.Even and city short distance traveling, user are also required to pay attention to very much the remaining capacity of electric vehicle, are otherwise susceptible on the way The case where no electricity casts anchor.And what similar two-wheeled battery truck was taken is arranged the scheme of charging equipment in roadside, for electric vehicle Speech is not just most suitable, and the floor space of one side electric vehicle is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills Electricity may cause traffic congestion, and on the other hand, electric vehicle power consumption also many bigger than the battery truck of two-wheeled charges in current battery In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
Invention content
The technical problem to be solved by the present invention is to：In view of the deficienciess of the prior art, a kind of charging of offer is convenient, and The electric car electric energy shared system of user hours underway is not delayed.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of electric car electric energy shared system, Include that there are two the aircraft that can be rested in respectively on two electric vehicles, and be connected between two aircraft to The electrical energy transportation of one electric vehicle is given to the conducting wire of another electric vehicle；The aircraft is equipped with and electrically connects with conducting wire Transmission of electricity connector；Further include being mounted on electric vehicle to connect electric connection socket, wiring connecting seat and electricity with what transmission of electricity connector electrically connected The accumulator of electrical automobile electrically connects.
Preferably：Further include that there are one supporting the hanging wire aircraft of conducting wire, hanging wire aircraft lower end There are one winding mechanisms for connection；The winding mechanism include there are one bobbin winder bracket and be rotatably installed on bobbin winder bracket rolling up Around the wire spool of the conducting wire, the coiling electric motor for driving wire spool to rotate is installed on the bobbin winder bracket.
Preferably：Two aircraft are respectively to rest in the first transmission of electricity on the electric vehicle for providing electric energy Aircraft and to rest on the electric vehicle that need to be charged second transmission of electricity aircraft, first transmission of electricity aircraft and second transmission of electricity Electricity Federation is connected to boost module between carry-on transmission of electricity connector；The carry-on transmission of electricity connector of first transmission of electricity and boost module Input terminal electrically connects, and the output end of the carry-on transmission of electricity connector of the second transmission of electricity and boost module electrically connects.
Preferably：The shaft of the wire spool is horizontally disposed, and the centre position of wire spool is equipped with partition board, wire spool The upper winding space that two same sizes are formed positioned at partition board both sides, the centre of the conducting wire is fixed on wire spool.
Preferably：There are two conductive electrode a, the conducting wire and conductive electrode a for the both ends installation of the wire spool It electrically connects；The position that wire spool both ends are corresponded on the bobbin winder bracket is equipped with and electrically connects with two conductive electrode a sliding contacts To the conductive electrode b to power for hanging wire aircraft, conductive electrode b is coupled by soft wire with hanging wire aircraft electrical.
Preferably：The aircraft includes main part, and the main part includes the fan installation of tubular Portion, the connecting tube of four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion, and be connected to Each connecting tube outer end and go out vane with what corresponding position connecting tube was connected；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving is installed on the upper bracket Fan；It is located in the fan mounting portion below connecting tube and is connected with lower bracket, lower driving wind is installed on the lower bracket Fan；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install driving fan part Internal diameter be more than the internal diameter of the lower driving fan part of installation in fan mounting portion, be located at upper driving fan in the fan mounting portion Wind pressure superatmospheric between lower driving fan so that go out and form wind pressure in vane；
It is described go out vane include sealed connection vane upper shell and vane lower housing, in the vane lower housing inner circumferential End forms interior curved wall, and there are one air outlet guard board, air outlet guard board upper ends by the connection of multiple dowels for the inner circumferential of the interior curved wall It is tightly connected with vane upper shell inner circumferential lower end；Outlet air gap wide at the top and narrow at the bottom is formed between the interior curved wall and air outlet guard board, The lower end width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is upper width Under narrow training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction The horizontal wind-force and the fan blade of upper driving fan that the wind for forming the angle of 5-20 degree, and going out the outlet air gap blowout of vane generates Rotation direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the tune in each connecting tube It includes third motor to save component, the coaxially connected screw rod with third motor output shaft, and the valve plate being connect with screw flight； For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；The company Take over internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out The side of vane is connected with the valve plate guide rod being slidably connected with the valve plate；There are one upper end courts for lower part connection in the connecting tube To the inclined baffle in vane direction is gone out, the conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively；
The main part is that upper shell and lower housing are tightly connected and constitute；
The main part upper end connects the air intake cover there are one semiellipse spherical shape, and strip is uniformly formed on air intake cover Air inlet.
Preferably：Go out position of the vane inner circumferential far from connecting tube described in each and forms Holder joint of rising and falling, it is each Respectively there are one undercarriages for connection in the Holder joint of rising and falling；The undercarriage includes to be fixedly connected and pass through with Holder joint of rising and falling Holder joint of rising and falling with go out the connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connecting tube Body is connected on supporting rod far from Holder joint one end of rising and falling close to the supporting rod for Holder joint one end rotation connection of rising and falling inhaling Tightly in the second electromagnet of automobile top, and the connecting rod with rotation connection in the middle part of sliding tube middle part, supporting rod respectively；
The connection pipe body forms hinged seat, described supporting rod one end and hinged seat close to the Holder joint one end wall that rises and falls Rotation connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the sliding pipe outer wall medium position is connected with Articulated joint, described connecting rod one end are rotatablely connected with articulated joint, side wall molding of the connection pipe body far from Holder joint one end of rising and falling There is the strip shape gob passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, seals The inner end of cap is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against respectively Between piston and sealing cap inner end；The connecting rod appearance that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod Slot；
The spring is in supporting rod when extended configuration and is in unfolded state, and the upper driving fan is in work shape After state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The present invention provides a kind of electric car electric energy shared system, it is characterised in that：Including there are two can stop respectively Aircraft on two electric vehicles, and be connected between two aircraft to the electric energy of an electric vehicle is defeated Give the conducting wire of another electric vehicle；The aircraft is equipped with the transmission of electricity connector electrically connected with conducting wire, is set on electric vehicle Have and connect electric connection socket with what transmission of electricity connector electrically connected, the accumulator of wiring connecting seat and electric vehicle electrically connects；
Further include there are one to support the hanging wire aircraft of conducting wire, there are one coilings for the connection of hanging wire aircraft lower end Mechanism；The winding mechanism include there are one bobbin winder bracket and be rotatably installed on bobbin winder bracket to wind the conducting wire around Drum is equipped with the coiling electric motor for driving wire spool to rotate on the bobbin winder bracket；
Two aircraft be respectively to rest in the first transmission of electricity aircraft on the electric vehicle that electric energy is provided and to The second transmission of electricity aircraft on the electric vehicle that need to be charged is rested in, the first transmission of electricity aircraft and the second transmission of electricity are carry-on defeated Electricity Federation is connected to boost module between electric connection；The input terminal Electricity Federation of the carry-on transmission of electricity connector and boost module of first transmission of electricity It connects, the output end of the carry-on transmission of electricity connector of the second transmission of electricity and boost module electrically connects；
The shaft of the wire spool is horizontally disposed, and the centre position of wire spool is equipped with partition board, is located at partition board two on wire spool Side forms the winding space of two same sizes, and the centre of the conducting wire is fixed on wire spool；
There are two conductive electrode a, the conducting wire is electrically connected with conductive electrode a for the both ends installation of the wire spool；It is described around Corresponded on coil holder wire spool both ends position be equipped with two conductive electrode a sliding contacts electrically connect to for hanging wire fly The conductive electrode b of device power supply, conductive electrode b are coupled by soft wire with hanging wire aircraft electrical；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan Mounting portion periphery and the connecting tube of four equidistant arrangements being connected with fan mounting portion, and it is connected to each connecting tube outer end And go out vane with what corresponding position connecting tube was connected；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving is installed on the upper bracket Fan；It is located in the fan mounting portion below connecting tube and is connected with lower bracket, lower driving wind is installed on the lower bracket Fan；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install driving fan part Internal diameter be more than the internal diameter of the lower driving fan part of installation in fan mounting portion, be located at upper driving fan in the fan mounting portion Wind pressure superatmospheric between lower driving fan so that go out and form wind pressure in vane；
It is described go out vane include sealed connection vane upper shell and vane lower housing, in the vane lower housing inner circumferential End forms interior curved wall, and there are one air outlet guard board, air outlet guard board upper ends by the connection of multiple dowels for the inner circumferential of the interior curved wall It is tightly connected with vane upper shell inner circumferential lower end；Outlet air gap wide at the top and narrow at the bottom is formed between the interior curved wall and air outlet guard board, The lower end width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is upper width Under narrow training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction The horizontal wind-force and the fan blade of upper driving fan that the wind for forming the angle of 5-20 degree, and going out the outlet air gap blowout of vane generates Rotation direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the tune in each connecting tube It includes third motor to save component, the coaxially connected screw rod with third motor output shaft, and the valve plate being connect with screw flight； For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；The company Take over internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out The side of vane is connected with the valve plate guide rod being slidably connected with the valve plate；There are one upper end courts for lower part connection in the connecting tube To the inclined baffle in vane direction is gone out, the conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively；
The main part is that upper shell and lower housing are tightly connected and constitute；
The main part upper end connects the air intake cover there are one semiellipse spherical shape, and strip is uniformly formed on air intake cover Air inlet；
Go out position of the vane inner circumferential far from connecting tube described in each and forms Holder joint of rising and falling, each Holder joint of rising and falling There are one undercarriages for upper each connection；The undercarriage include be fixedly connected with Holder joint of rising and falling and by rise and fall Holder joint with go out The connection pipe body being connected inside vane, the sliding tube being slidably mounted in connection pipe body, with connection pipe body close to the bridge joint that rises and falls The supporting rod of first end rotation connection is connected on supporting rod far from Holder joint one end of rising and falling sucking in automobile top Second electromagnet, and the connecting rod with rotation connection in the middle part of sliding tube middle part, supporting rod respectively；
The connection pipe body forms hinged seat, described supporting rod one end and hinged seat close to the Holder joint one end wall that rises and falls Rotation connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the sliding pipe outer wall medium position is connected with Articulated joint, described connecting rod one end are rotatablely connected with articulated joint, side wall molding of the connection pipe body far from Holder joint one end of rising and falling There is the strip shape gob passed through for articulated joint；The one end of the connection pipe body far from Holder joint of rising and falling is fixedly connected with sealing cap, seals The inner end of cap is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against respectively Between piston and sealing cap inner end；The connecting rod appearance that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod Slot；
The spring is in supporting rod when extended configuration and is in unfolded state, and the upper driving fan is in work shape After state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The present invention provides a kind of method for realizing that electric car electric energy is shared using above-mentioned electric car electric energy shared system, When the electricity of electric vehicle a is less than setting value, electric vehicle is automatic or sends charging to server under user's manual operation Request, server sends charge request to each electric vehicle b close to electric vehicle a, while server is by electric vehicle a's Location information and driving path are sent to electric vehicle b, and whether electric vehicle b provides electric energy by its corresponding user's artificial selection It is shared；First confirms that provide the shared electric vehicle b of electric energy travels close to electric vehicle a, while server controls are by one Two connected aircraft of conducting wire are respectively flown on electric vehicle a and electric vehicle b, make transmission of electricity connector on corresponding electric vehicle The electric connection socket that connects electrically connect.
Preferably：It is at least one to fly when the distance between electric vehicle a and electric vehicle b are more than setting value Row device is detached from electric vehicle.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is filled electricity by least two aircraft The electric energy of the electric vehicle of foot is shared with the electric vehicle charging of not enough power supply, solves electric automobile during traveling process midway electricity Insufficient problem.
The hanging wire aircraft is used to support the middle part of conducting wire, and conducting wire is made not cause shadow to the normally travel of electric vehicle It rings, in addition, the Wire-wound, on the winding mechanism below hanging wire aircraft, winding mechanism can be according to the distance between two vehicles The effective length of conducting wire is adjusted flexibly.
The aircraft, hanging wire aircraft provide driving force, upper driving wind by the upper driving fan in fan mounting portion Fan the fraction that generates from it is each go out vane outlet air gap downwards blow out, and adjusting part adjustment is combined each to go out vane Go out wind velocity, to realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only rise It is not easily led to when going out vane with foreign object generation touching winged without the fan for being provided with power to the effect of adjustment attitude of flight vehicle Row device is out of control or generates injury to human or animal, and safety is good.For the aircraft appearance similar to four-axle aircraft, four go out vane The function of adjusting posture is only played, therefore the present invention substantially should be uniaxial aircraft.
Further, it is described go out vane outlet air gap spray air-flow can be along training wall stream according to Coanda principle It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward together, flown in this way When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly The stabilization of row device flight attitude.
Further, it is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction and water of vane The horizontal wind-force and upper driving wind that the wind for forming the angle of 5-20 degree square between, and going out the outlet air gap blowout of vane generates The rotation direction of the fan blade of fan is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset The reaction force that driving fan or upper driving fan and lower driving fan generate when rotating；Also, by adjusting each tune simultaneously Section component change vane go out wind velocity, it can be achieved that aircraft whole forward or reverse.By adjusting one or two Adjusting part makes what one or two went out vane to go out wind velocity, it can be achieved that aircraft is generally in heeling condition, can drive in this way Dynamic aircraft flies in the horizontal direction.
Description of the drawings
Fig. 1 is the use state diagram of the present invention.
Fig. 2 is the structural schematic diagram of electric vehicle.
Fig. 3 is the decomposition texture schematic diagram for connecing electric connection socket.
Fig. 4 is the structural schematic diagram of winding mechanism.
Fig. 5 is the structural schematic diagram of aircraft shutdown status.
Fig. 6 is the structural schematic diagram of aircraft flight state.
Fig. 7 is the schematic cross-sectional view of aircraft.
Fig. 8 is the portions the A schematic enlarged-scale view of Fig. 7.
Fig. 9 is the portions the B schematic enlarged-scale view of Fig. 7.
The structural schematic diagram of each component that Figure 10 is upper shell and is connect with upper shell.
Figure 11 is the structural schematic diagram of lower housing section.
Figure 12 is the schematic cross-sectional view of lower housing section.
Figure 13 is the decomposition texture schematic diagram of undercarriage part.
Figure 14 is the schematic cross-sectional view of undercarriage part.
4, winding mechanism；41, bobbin winder bracket；42, wire spool；421, partition board；43, coiling electric motor；44, connecting rope；
5, electric vehicle；5a, electric connection socket is connect；51, powered electrode plate；52, insulation sleeve；53, powered electrode seat；54, magnetic Ferropexy seat；
6, conducting wire；
9a, hanging wire aircraft；9b, the first transmission of electricity aircraft；9c, the second transmission of electricity aircraft；91, main part；91a, upper casing Body；91b, lower housing；
910, fan mounting portion；9101, upper bracket；9102, lower bracket；9103, accumulator mounting portion；9104, circuit board Installation cavity；9105, air inlet hole；9106, vent；9107, trolley pole；91071, powered electrode a；91072, powered electrode b；
911, go out vane；9110, it rises and falls Holder joint；9111, vane upper shell；9112, vane lower housing；91121, interior curved Wall；91122, dowel；91123, air outlet guard board；91124, training wall；
912, connecting tube；9121, third motor mounting plate；9122, valve plate guide rod；9123, baffle；913, the first cover board；
92, accumulator；
93, undercarriage；931, connection pipe body；9311, hinged seat；9312, strip shape gob；932, sliding tube；9321, piston； 9322, articulated joint；933, sealing cap；9331, spring positioning bar；934, connecting rod；935, supporting rod；9351, connecting rod tank；936、 Second electromagnet；937, spring；
94, air intake cover；
951, upper driving fan；952, lower driving fan；
96, adjusting part；961, third motor；962, screw rod；963, valve plate；
97, control circuit board.
Specific implementation mode
Embodiment 1
According to Fig. 1 to 4, the present embodiment is a kind of electric car electric energy shared system, including there are two can distinguish Rest in the aircraft on two electric vehicles, and be connected between two aircraft to by the electricity of an electric vehicle The conducting wire 6 of another electric vehicle can be conveyed to；The aircraft is equipped with the transmission of electricity connector electrically connected with conducting wire；It further include peace On electric vehicle electric connection socket 5a, the accumulator electricity of wiring connecting seat and electric vehicle are connect with what transmission of electricity connector electrically connected Connection.
Two aircraft are respectively to rest in the first transmission of electricity aircraft 9b and the use on the electric vehicle for providing electric energy To rest in the second transmission of electricity aircraft 9c on the electric vehicle that need to be charged, the first transmission of electricity aircraft and second is transmitted electricity on aircraft Transmission of electricity connector between Electricity Federation be connected to boost module；The input terminal electricity of the carry-on transmission of electricity connector of first transmission of electricity and boost module The output end of connection, the carry-on transmission of electricity connector of the second transmission of electricity and boost module electrically connects.
The electric vehicle that the boost module charges to needs after bringing the voltage up to the rated voltage of charging charges.
Further include there are one to support the hanging wire aircraft 9a of conducting wire, the connection of hanging wire aircraft lower end there are one around Line mechanism 4；The winding mechanism include there are one bobbin winder bracket 41 and be rotatably installed on bobbin winder bracket winding described lead The wire spool 42 of line is equipped with the coiling electric motor 43 for driving wire spool to rotate on the bobbin winder bracket.
The shaft of the wire spool is horizontally disposed, and the centre position of wire spool is equipped with partition board 421, is located at partition board on wire spool Both sides form the winding space of two same sizes, and the centre of the conducting wire is fixed on wire spool.The conducting wire is with intermediate point For boundary two parts respectively on two winding spaces.
There are two conductive electrode a, the conducting wire is electrically connected with conductive electrode a for the both ends installation of the wire spool；It is described around Corresponded on coil holder wire spool both ends position be equipped with two conductive electrode a sliding contacts electrically connect to for hanging wire fly The conductive electrode b of device power supply, conductive electrode b are coupled by soft wire with hanging wire aircraft electrical.
The electric connection socket that connects includes sequentially connected magnet fixed seat 54, powered electrode seat 53, insulation from bottom to top Plate 52 and powered electrode plate 51.
Powered electrode seat upper end uniformly forms the convex cavity of multiple circular groove shapes, and the powered electrode seat is non-ferric The metal of magnetic material is made.
The position that magnet fixed seat upper end corresponds to each convex cavity is connected with permanent magnet a, and permanent magnet a stretches into correspondence In the convex cavity of position.The position that the upper end of the insulation board corresponds to each convex cavity forms the convex cavity that insulate The insulation sleeve of lateral wall.The position that each insulation sleeve is corresponded on the powered electrode plate forms appearance hole.The powered electrode plate And current electrode seat is connected with the accumulator of electric vehicle or charging control circuit.
There are one charging rod 9107, charging rod lower end is equipped with logical with permanent magnet a for connection among the lower end of the aircraft The iron block that magnetic force sucks is crossed, the iron block is simultaneously as the powered electrode a91071 with the electric shock connection of powered electrode seated connection；It is described The periphery that aircraft lower end is located at iron block is connected with 3 elastic rods, and the lower end of elastic rod is connected with contacts electricity with powered electrode plate The powered electrode b91072 of connection.The powered electrode a, powered electrode b are electrically connected with conducting wire respectively.Meanwhile the storage of aircraft The electric energy that battery is also provided by conducting wire is powered.
When the electricity of electric vehicle a is less than setting value, electric vehicle it is automatic or under user's manual operation to server Charge request is sent, server sends charge request to each electric vehicle b close to electric vehicle a, while server will be electric The location information and driving path of electrical automobile a is sent to electric vehicle b, and electric vehicle b is by its corresponding user's artificial selection No offer electric energy is shared；First confirms that provide the shared electric vehicle b of electric energy travels close to electric vehicle a, while server Control by a conducting wire be connected two aircraft respectively fly on electric vehicle a and electric vehicle b, make transmission of electricity connector with it is corresponding The electric connection socket that connects on electric vehicle electrically connects.
When the distance between electric vehicle a and electric vehicle b are more than setting value, at least one aircraft and electric vehicle It is detached from.
Above-mentioned electric vehicle a is the electric vehicle for needing to charge, and electric vehicle b is to provide electricity shared electric vehicle, A, b is only for the purposes of distinguishing, and the restriction of unsubstantiality.
The touch screen electrically connected with the control system of electric vehicle is equipped in the electric vehicle, manually to send charging Request receives charge request, display driving path etc..Control system, touch screen etc. as electric vehicle are the prior art, And be not emphasis of the present invention, details are not described herein.
Embodiment 2
The present embodiment and embodiment 1 difference lies in：The connect electric connection socket and transmission of electricity connector is to pass through wireless charging Power technology realizes the coil of electric energy transmission.
Embodiment 3
In conjunction with shown in Figure 13 to Figure 14, the present embodiment makes following improvement on the basis of embodiment 1：The aircraft packet Main part 91 is included, the main part includes the fan mounting portion 910 of tubular, is connected to fan mounting portion periphery and and wind The connecting tube for four equidistant arrangements that fan mounting portion is connected, and be connected to each connecting tube outer end and connect with corresponding position What pipe was connected goes out vane 911.
It is located in the fan mounting portion above connecting tube and is connected with upper bracket 9101, is equipped on the upper bracket Driving fan 951；It is located in the fan mounting portion below connecting tube and is connected with lower bracket 9102, is installed on the lower bracket There is lower driving fan 952；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install The internal diameter of driving fan part is more than the internal diameter of the lower driving fan part of installation in fan mounting portion, position in the fan mounting portion Wind pressure superatmospheric between upper driving fan and lower driving fan so that go out and form wind pressure in vane.
It is described go out vane include sealed connection vane upper shell 9111 and vane lower housing 9112, the vane lower casing Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected by multiple dowels 91122 there are one air outlet guard board, Air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；Shape between the interior curved wall 91121 and air outlet guard board 91123 At outlet air gap wide at the top and narrow at the bottom, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing is located at The lower section in outlet air gap is training wall 91124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface residing for the training wall is 20-30 Degree.
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction The horizontal wind-force and the fan blade of upper driving fan that the wind for forming the angle of 5-20 degree, and going out the outlet air gap blowout of vane generates Rotation direction is opposite.
It is equipped with to adjust the adjusting part 96 that corresponding position goes out vane outlet air speed in each connecting tube, it is described Adjusting part includes third motor 961, the screw rod 962 coaxially connected with third motor output shaft, and is connected with screw flight The valve plate 963 connect；For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the middle part of upper and lower directions in connecting tube Position；The connecting tube internal upper part forms to install the third motor mounting plate of the third motor, the third motor Mounting plate 9121 is connected with the valve plate guide rod 9122 being slidably connected with the valve plate towards the side for going out vane；In the connecting tube There are one upper ends for lower part connection towards the inclined baffle 9123 in vane direction is gone out, and conducting area is formed between the baffle and valve plate Adjustable air passage.
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board 97 respectively.Institute It is upper shell 91a and lower housing 91b sealed connection compositions to state main part；The trolley pole lower end is fixedly connected on the upper shell Above close to the position for going out vane；.
The main part upper end connects the air intake cover 94 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover The air inlet of shape.
The lower, outer perimeter of the fan mounting portion is accumulator mounting portion 9103, is connected with and controls on accumulator mounting portion The accumulator 92 of circuit board electrical connection；Camera, the camera and control circuit are installed on the main part of the aircraft Plate is electrically connected.
State of the camera for observing aircraft in real time, aircraft can be accommodated to electric vehicle by manual control On, the automatic stop of aircraft can also be realized by machine vision technique.
The top for being located at accumulator mounting portion on the fan mounting portion is a circuit board installation cavity 9104, the control Circuit board is mounted in circuit board installation cavity, and there are one the first cover boards 913 of annular for the connection of circuit board installation cavity lower end；Institute The upper surface for stating circuit board installation cavity uniformly forms the air inlet hole 9105 being connected to in fan mounting portion, the circuit board installation The lateral wall of chamber uniformly forms vent 9106.
Aircraft provides driving force, upper driving fan production by upper driving fan, the lower driving fan in fan mounting portion Raw fraction from it is each go out vane outlet air gap blow out downwards, and combine adjusting part adjustment each go out vane outlet air Speed, to realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only play tune The effect of whole attitude of flight vehicle goes out when vane generates touching with foreign object without the fan for being provided with power and does not easily lead to aircraft Out of control or generate injury to human or animal, safety is good.The aircraft appearance is similar to four-axle aircraft, therefore with four-axle aircraft It is named, four go out vane i.e. so-called " four axis " and only play the function of adjusting posture, therefore this aircraft substantially should be uniaxial Aircraft.
Further, it is described go out vane outlet air gap spray air-flow can be along training wall stream according to Coanda principle It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward together, flown in this way When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly The stabilization of row device flight attitude.
Further, it is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out the axial direction and water of vane The horizontal wind-force and upper driving wind that the wind for forming the angle of 5-20 degree square between, and going out the outlet air gap blowout of vane generates The rotation direction of the fan blade of fan is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane is enough offset The reaction force that driving fan and lower driving fan generate when rotating；Also, change by adjusting each adjusting part simultaneously Vane go out wind velocity, it can be achieved that aircraft whole forward or reverse.Make one by adjusting one or two adjusting part It is a or two go out vane go out wind velocity, it can be achieved that aircraft is generally in heeling condition, can be driven aircraft in this way in water Square to flight.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, is played to control circuit board scattered Heat effect.
Go out position of the vane inner circumferential far from connecting tube described in each and forms Holder joint 9110 of rising and falling, each undercarriage Respectively there are one undercarriages 93 for connection on connector；The undercarriage is equipped with to suck the second electromagnet in electromobile at top 936。
The hanging wire Flight Vehicle Structure is identical as aircraft.
Embodiment 4
In conjunction with Figure 13 to Figure 14, the present embodiment also makes following improvement on the basis of embodiment 2：Go out vane described in each Position of the inner circumferential far from connecting tube forms Holder joint 9110 of rising and falling, and respectively there are one rise and fall for connection in each Holder joint of rising and falling Frame 93；The undercarriage include be fixedly connected with Holder joint of rising and falling and by rise and fall Holder joint with go out inside vane to be connected Connection pipe body 931, the sliding tube 932 being slidably mounted in connection pipe body, with connection pipe body close to Holder joint one end rotation of rising and falling The supporting rod 935 of connection, be connected on supporting rod far from Holder joint one end of rising and falling sucking the in electromobile at top Two electromagnet 936, and the connecting rod 934 with rotation connection in the middle part of sliding tube middle part, supporting rod respectively.
The connection pipe body forms hinged seat 9311, described supporting rod one end and hinge close to the Holder joint one end wall that rises and falls Joint chair is rotatablely connected；The sliding tube is connected with piston 9321, sliding pipe outer wall middle part position close to Holder joint one end of rising and falling It sets and is connected with articulated joint 9322, described connecting rod one end is rotatablely connected with articulated joint, and the connection pipe body is far from Holder joint one of rising and falling The side wall at end forms the strip shape gob 9312 passed through for articulated joint；The one end of 912 body of the connecting tube far from Holder joint of rising and falling is solid Surely it is connected with sealing cap 933, the inner end of sealing cap is connected with spring positioning bar 9331, is arranged on the spring positioning bar Spring 937, the both ends of the spring are against respectively between piston and sealing cap inner end；It forms on the supporting rod and is received in supporting rod The connecting rod tank 9351 of the connecting rod is accommodated when the state of rising.
The spring is in supporting rod when extended configuration and is in unfolded state, and the upper driving fan is in work shape After state, the air pressure driving piston gone out in vane makes supporting rod be in collapsed state together with sliding tube movement.
The undercarriage with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, go out Wind pressure in vane makes piston be moved to sealing cap one end together with sliding tube, to make sliding tube drive connecting rod one end to sealing cap Direction is moved, to make supporting rod lower end also be rotated to sealing cap one end, to make undercarriage be in collapsed state.Work as aircraft When landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved toward hinged seat direction together with piston, to make sliding tube Connecting rod one end is driven to be moved to hinged seat direction, to make supporting rod lower end turn to extreme position to hinged seat one end, to Undercarriage is set to be in unfolded state.
The strip shape gob plays the role of articulated joint on limit slippage pipe, and the position of strip shape gob end just makes spring stretch After length, supporting rod turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each supporting rod is equal In stable state.

Claims (5)

1. a kind of electric car electric energy shared system, it is characterised in that：Including there are two can rest in two electronic vapour respectively Aircraft on vehicle, and be connected between two aircraft giving the electrical energy transportation of an electric vehicle to another electricity The conducting wire of electrical automobile；The aircraft is equipped with the transmission of electricity connector electrically connected with conducting wire；Further include being mounted on electric vehicle Electric connection socket is connect with what transmission of electricity connector electrically connected, and the accumulator of wiring connecting seat and electric vehicle electrically connects；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan installation Portion periphery and the connecting tube of four equidistant arrangements being connected with fan mounting portion, and be connected to each connecting tube outer end and with What corresponding position connecting tube was connected goes out vane；
It is located in the fan mounting portion above connecting tube and is connected with upper bracket, driving wind is installed on the upper bracket Fan；It is located in the fan mounting portion below connecting tube and is connected with lower bracket, lower driving fan is installed on the lower bracket； The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion Diameter is more than the internal diameter of the lower driving fan part of the interior installation of fan mounting portion, is located at upper driving fan under in the fan mounting portion Wind pressure superatmospheric between driving fan so that go out and form wind pressure in vane；
It is described go out vane include sealed connection vane upper shell and vane lower housing, the vane lower housing inner circumferential upper end at Type has interior curved wall, and there are one air outlet guard board, air outlet guard board upper end and wind by the connection of multiple dowels for the inner circumferential of the interior curved wall Ring upper shell inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing is located at outlet air gap is wide at the top and narrow at the bottom Training wall, the cone angle size of the taper surface residing for the training wall is 20-30 degree；
It is described go out vane axial direction and the radial direction of fan mounting portion it is perpendicular, and go out between the axial direction of vane and horizontal direction and formed The angle of 5-20 degree, and go out the rotation of the horizontal wind-force and the fan blade of upper driving fan of the wind generation of the outlet air gap blowout of vane Direction is opposite；
It is equipped with to adjust the adjusting part that corresponding position goes out vane outlet air speed, the adjusting group in each connecting tube Part includes third motor, the coaxially connected screw rod with third motor output shaft, and the valve plate being connect with screw flight；It is described For valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the medium position of upper and lower directions in connecting tube；The connecting tube Internal upper part forms to install the third motor mounting plate of the third motor, and the third motor mounting plate direction goes out vane Side be connected with the valve plate guide rod being slidably connected with the valve plate；There are one upper end directions to go out for lower part connection in the connecting tube The inclined baffle in vane direction forms the conducting adjustable air passage of area between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively；
The main part is that upper shell and lower housing are tightly connected and constitute；
Main part upper end connection there are one the air intake cover of semiellipse spherical shape, uniformly formed on air intake cover strip into Air port.
2. a kind of electric car electric energy shared system as described in claim 1, it is characterised in that：Further include that there are one propping up The hanging wire aircraft of conducting wire is supportted, there are one winding mechanisms for the connection of hanging wire aircraft lower end；The winding mechanism includes one A bobbin winder bracket and be rotatably installed on bobbin winder bracket to wind the wire spool of the conducting wire, installed on the bobbin winder bracket useful With the coiling electric motor for driving wire spool to rotate.
3. a kind of electric car electric energy shared system as described in claim 1, it is characterised in that：Two aircraft are respectively to use To rest in the first transmission of electricity aircraft and to rest on the electric vehicle that need to be charged on the electric vehicle for providing electric energy Second transmission of electricity aircraft, Electricity Federation is connected to boosting mould between the first transmission of electricity aircraft and the second carry-on transmission of electricity connector of transmission of electricity Block；The input terminal of the carry-on transmission of electricity connector of first transmission of electricity and boost module electrically connects, the second carry-on transmission of electricity of transmission of electricity The output end of connector and boost module electrically connects.
4. a kind of electric car electric energy shared system as claimed in claim 2, it is characterised in that：The shaft water of the wire spool The centre position of flat setting, wire spool is equipped with partition board, and the coiling that formation two same sizes in partition board both sides are located on wire spool is empty Between, the centre of the conducting wire is fixed on wire spool.
5. a kind of electric car electric energy shared system as claimed in claim 2, it is characterised in that：Pacify at the both ends of the wire spool There are two conductive electrode a, the conducting wires to be electrically connected with conductive electrode a for dress；The position at wire spool both ends is corresponded on the bobbin winder bracket Be equipped with two conductive electrode a sliding contacts electrically connect to the conductive electrode b that powers for hanging wire aircraft, conductive electrode B is coupled by soft wire with hanging wire aircraft electrical.
CN201710489017.1A 2017-06-23 2017-06-23 A kind of electric car electric energy shared system and sharing method Active CN107139767B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CN201710489017.1A CN107139767B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system and sharing method
CN201810101785.XA CN108312869B (en) 2017-06-23 2017-06-23 Electric vehicle electric energy sharing method
CN201810101355.8A CN108248435B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system
CN201810101354.3A CN108312868B (en) 2017-06-23 2017-06-23 Electric automobile electric energy sharing system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710489017.1A CN107139767B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system and sharing method

Related Child Applications (3)

Application Number Title Priority Date Filing Date
CN201810101354.3A Division CN108312868B (en) 2017-06-23 2017-06-23 Electric automobile electric energy sharing system
CN201810101785.XA Division CN108312869B (en) 2017-06-23 2017-06-23 Electric vehicle electric energy sharing method
CN201810101355.8A Division CN108248435B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system

Publications (2)

Publication Number Publication Date
CN107139767A CN107139767A (en) 2017-09-08
CN107139767B true CN107139767B (en) 2018-08-14

Family

ID=59782982

Family Applications (4)

Application Number Title Priority Date Filing Date
CN201710489017.1A Active CN107139767B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system and sharing method
CN201810101785.XA Active CN108312869B (en) 2017-06-23 2017-06-23 Electric vehicle electric energy sharing method
CN201810101355.8A Active CN108248435B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system
CN201810101354.3A Active CN108312868B (en) 2017-06-23 2017-06-23 Electric automobile electric energy sharing system

Family Applications After (3)

Application Number Title Priority Date Filing Date
CN201810101785.XA Active CN108312869B (en) 2017-06-23 2017-06-23 Electric vehicle electric energy sharing method
CN201810101355.8A Active CN108248435B (en) 2017-06-23 2017-06-23 A kind of electric car electric energy shared system
CN201810101354.3A Active CN108312868B (en) 2017-06-23 2017-06-23 Electric automobile electric energy sharing system

Country Status (1)

Country Link
CN (4) CN107139767B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109228898A (en) * 2018-09-26 2019-01-18 广州华跃电力工程设计有限公司 A kind of charging system for electric automobile, charging method, device and storage medium
CN109547627A (en) * 2018-09-29 2019-03-29 东莞市趣电智能科技有限公司 Charging demand for electric vehicles matches service system, computer readable storage medium
JP6763596B1 (en) * 2019-01-16 2020-09-30 株式会社ナイルワークス Drone system, drone, moving object, compartment member, drone system control method, and drone system control program

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104253464B (en) * 2013-06-28 2017-05-03 比亚迪股份有限公司 System for mutual charging of electric vehicles and charging connector
CN113232547B (en) * 2014-08-08 2023-07-18 深圳市大疆创新科技有限公司 Unmanned aerial vehicle battery replacement system and method
CN104192017B (en) * 2014-08-18 2016-09-07 中国矿业大学(北京) A kind of autonomous formula electric motor car electric power system and method for supplying power to thereof
CN204279932U (en) * 2014-10-28 2015-04-22 深圳九星智能航空科技有限公司 Bottom is provided with the unmanned vehicle of wireless charging current-collecting device
CN205304342U (en) * 2015-10-12 2016-06-08 上海中科深江电动车辆有限公司 Electric vehicle removes wireless benefit electric system
US10753761B2 (en) * 2015-11-13 2020-08-25 Nio Usa, Inc. Universal battery and modular power system
CN106549433B (en) * 2015-11-30 2020-03-06 深圳北斗应用技术研究院有限公司 Mobile charging control method and system for electric vehicle to be charged
CN105825713B (en) * 2016-04-08 2018-07-24 重庆大学 The method of operation of vehicle-mounted unmanned aerial vehicle DAS (Driver Assistant System)
CN205882819U (en) * 2016-06-24 2017-01-11 上海蓝幻航空科技有限公司 On -vehicle solar charging system of wired electronic unmanned aerial vehicle
CN106160134A (en) * 2016-09-30 2016-11-23 安徽翼讯飞行安全技术有限公司 A kind of aerial charging device of unmanned plane

Also Published As

Publication number Publication date
CN108248435A (en) 2018-07-06
CN108248435B (en) 2019-10-15
CN107139767A (en) 2017-09-08
CN108312868B (en) 2020-09-22
CN108312869A (en) 2018-07-24
CN108312868A (en) 2018-07-24
CN108312869B (en) 2020-07-03

Similar Documents

Publication Publication Date Title
CN107176052B (en) Electric car electric energy shared system and sharing method
CN107139767B (en) A kind of electric car electric energy shared system and sharing method
CN107215231B (en) A kind of electric vehicle and charging system
CN107244253B (en) Charging system for electric automobile
CN107215232B (en) A kind of New-energy electric vehicle charging system
CN107176062B (en) A kind of electric vehicle power supply system
CN107244238B (en) New-energy electric vehicle charging system
CN108312875A (en) A kind of charging system for electric automobile to be charged by transmission guide rail
CN107215230B (en) A kind of charging system for electric automobile
CN107117301B (en) Charging system for electric automobile
CN206812832U (en) A kind of electric car electric energy shared system
CN108556649A (en) A kind of power supply system for electric vehicle charging
CN206841203U (en) Electric car electric energy shared system
CN206841714U (en) Charging system for electric automobile

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20220706

Address after: 310051 1, -10 5, No. 11, Ju Gong Road, Binjiang District Xi Xing street, Hangzhou, Zhejiang.

Patentee after: Lin Weixin

Address before: 310051 1, -10 5, No. 11, Ju Gong Road, Binjiang District Xi Xing street, Hangzhou, Zhejiang.

Patentee before: HANGZHOU LIPU TECHNOLOGY Co.,Ltd.