CN107176052A - Electric car electric energy shared system and sharing method - Google Patents
Electric car electric energy shared system and sharing method Download PDFInfo
- Publication number
- CN107176052A CN107176052A CN201710488489.5A CN201710488489A CN107176052A CN 107176052 A CN107176052 A CN 107176052A CN 201710488489 A CN201710488489 A CN 201710488489A CN 107176052 A CN107176052 A CN 107176052A
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- China
- Prior art keywords
- vane
- electric automobile
- aircraft
- fan
- electric
- Prior art date
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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
- B60L53/10—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
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2240/00—Control parameters of input or output; Target parameters
- B60L2240/70—Interactions with external data bases, e.g. traffic centres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The invention discloses a kind of electric car electric energy shared system and sharing method, the system includes electric automobile, the aircraft being mounted on electric automobile and the wire being connected between electric automobile and aircraft；It is provided between two electrodes, two aircraft and is electrically connected by electrode on each aircraft；Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is electrically connected with carry-on electrode；When two electric automobiles share electric energy, the aircraft that two electric automobiles are each carried overhead of position between two electric automobiles is relatively fixed and electrically connects the electrode between two aircraft.The aircraft that the present invention is each carried by two electric automobiles electrically connects the charging electric vehicle realized and the electric energy of the sufficient electric automobile of electricity is shared to not enough power supply, the problem of solving electric automobile during traveling process midway not enough power supply in the air.
Description
Technical field
The invention belongs to electric automobile corollary system field, and in particular to a kind of electric car electric energy shared system.
Background technology
With the popularization of electric automobile, the problem of charging electric vehicle is inconvenient is also increasingly highlighted；Electric automobile is bought at present
User be typically limited to only that city is on and off duty to be used, it is necessary to which outgoing user then still tends to use fuel oil at a distance for a long time
Car.And even city short distance is travelled, user is also required to note very much the dump energy of electric automobile, otherwise easily occurs on the way
Situation about being cast anchor without electricity.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric automobile
Speech is not just most suitable, and the floor space of one side electric automobile is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills
Electricity is likely to result in traffic congestion, on the other hand, the big many of battery truck of the electric automobile power consumption also than two-wheeled, in current battery charging
In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
The content of the invention
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, provide a kind of charging conveniently, and
The electric car electric energy shared 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 electric car electric energy shared system,
Include electric automobile, the aircraft being mounted on electric automobile and the wire being connected between electric automobile and aircraft；
The aircraft upper end or lower end are provided with two electrodes that concentric setting is provided with permanent magnet a, the permanent magnet
a；The aircraft lower end or upper end are provided with two electrode b that concentric setting is provided with electromagnet, the electromagnet；Two
Electrically connected between individual aircraft by electrode a, electrode b；
Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is with being arranged on carry-on liter
The input of die block is electrically connected, and the electrode a, input, output ends of the electrode b respectively with boost module are electrically connected.In order to
Electrode a can be aligned with electrode b, and the electromagnet should be that diameter is close or identical is cylindric with permanent magnet a.
Preferably：The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes one
The Wiinding cartridge of individual upper end open, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the magnetic material of Wiinding cartridge upper end
Lid；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor
Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two
The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute
Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through.
Preferably：The aircraft includes main part, and the fan that the main part includes tubular is installed
Portion, is connected to the connecting tube of fan installation portion periphery and four equidistant arrangements being connected with fan installation portion, and is connected to
Each connecting tube outer end and with correspondence position connecting tube is connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper
Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
To opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described
Valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube
Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube
The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port.
Preferably：The lower, outer perimeter of the fan installation portion is to connect on battery installation portion, battery installation portion
It is connected to the battery electrically connected with control board；The main part upper end of the aircraft is provided with camera, main part
End is provided with lower camera, and the upper camera, lower camera are electrically connected with control board respectively.
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 automobile 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.
Preferably：The electromagnet is arranged at the top of air intake cover, and the electrode b is arranged on electromagnet upper end, institute
Electromagnet is stated to electrically connect with control board；The lower carriage lower end is connected with charging rod, and the permanent magnet a is arranged on charging rod
Bottom, the electrode a is arranged on permanent magnet a lower ends；
Between two aircraft by permanent magnet a sucked with cold electromagnet together with and realize electrode a and electrode b electricity
Connection；Produced when the electromagnet is powered makes two aircraft disengagings with the reverse magnetic field of permanent magnet.
The present invention also provides a kind of electric car electric energy shared system, includes electric automobile, is mounted on electric automobile
Aircraft and the wire that is connected between electric automobile and aircraft；
The aircraft upper end or lower end are provided with two electrodes that concentric setting is provided with permanent magnet a, the permanent magnet
a；The aircraft lower end or upper end are provided with two electrode b that concentric setting is provided with electromagnet, the electromagnet；Two
Electrically connected between individual aircraft by electrode a, electrode b；
Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is with being arranged on carry-on liter
The input of die block is electrically connected, and the electrode a, input, output ends of the electrode b respectively with boost module are electrically connected；
The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes the coiling of a upper end open
Box, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor
Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two
The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute
Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through；
The aircraft includes main part, and the main part includes the fan installation portion of tubular, is connected to fan installation
Portion periphery and the connecting tube for four equidistant arrangements being connected with fan installation portion, and be connected to each connecting tube outer end and with
What correspondence position connecting tube was connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper
Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
To opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described
Valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube
Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube
The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port；
The lower, outer perimeter of the fan installation portion is to be connected with battery installation portion, battery installation portion and control board electricity
The battery of connection；The main part upper end of the aircraft is provided with camera, and main part lower end is provided with lower camera, institute
Camera, lower camera is stated to electrically connect with control board respectively；
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 the second of automobile top
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.
Present invention offer is a kind of to realize the shared method of electric car electric energy using above-mentioned electric car electric energy shared system,
When electric automobile a electricity is less than setting value, electric automobile sends charging automatically or in the case where user manually operates to server
Request, server sends charge request to each electric automobile b close to electric automobile a, while server is by electric automobile a's
Positional information and driving path are sent to electric automobile b, and whether electric automobile b provides electric energy by its corresponding user's artificial selection
It is shared；First confirms that provide the shared electric automobile b of electric energy travels close to electric automobile a, in electric automobile b and electric automobile
When the distance between a is less than setting value, the aircraft on electric automobile a and electric automobile b flies to electric automobile a and electric automobile
The top of position between b, and the electrode b of the electric automobile b aircraft and electrode a of electric automobile a aircraft electrically connects.
The electric automobile a is needs the electric automobile charged, and electric automobile b is the shared electric automobile of offer electricity,
A, b limit only for the purposes of distinguishing without substantial.
Preferably；When the distance between electric automobile a and electric automobile b exceed setting value, electric automobile a and
The aircraft that electric automobile b is each carried mutually is disengaged.
The present invention provides a kind of electric car electric energy shared system, includes electric automobile, is mounted on electric automobile
Aircraft and the wire being connected between electric automobile and aircraft；
It is provided between two electrodes, two aircraft and is electrically connected by electrode on each aircraft；
Described wire one end couples with the storage battery of electric automobile, the other end of the wire and carry-on electrode Electricity Federation
Connect；
When two electric automobiles share electric energy, the aircraft that two electric automobiles are each carried position between two electric automobiles
Overhead be relatively fixed and electrically connect the electrode between two aircraft.
Compared with prior art, the beneficial effects of the invention are as follows：What the present invention was each carried by two electric automobiles
Aircraft electrically connects the charging electric vehicle realized and the electric energy of the sufficient electric automobile of electricity is shared to not enough power supply in the air,
The problem of solving electric automobile during traveling process midway not enough power supply.
Pass through electromagnet between two aircraft（Iron core）With permanent magnet a realize be relatively fixed, while realize electrode a with
Electrode b contact is electrically connected；When electric automobile a chargings are finished or electric automobile a is different from electric automobile b driving paths,
The aircraft of two cars departs from, and electromagnet is powered to producing when two aircraft depart from makes two flights with magnetic field reverse permanent magnet a
Device is disengaged.
When aircraft does not work, the aircraft passes through the second electromagnet（Iron core）Suck in electromobile at top coiling
The upper end of the lid of component, when aircraft works, the energization of the second electromagnet, which produces the magnetic field reverse with the lid of magnetic material, to be made
Aircraft departs from electric automobile.
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.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2 is that aircraft rests in structural representation when on electric automobile.
Fig. 3 is the decomposition texture schematic diagram of wire-winding unit.
Fig. 4 is the structural representation of aircraft stopped status.
Fig. 5 is the structural representation of aircraft flight state.
Fig. 6 is the cross section structure diagram of aircraft.
Fig. 7 is Fig. 6 A portions schematic enlarged-scale view.
Fig. 8 is Fig. 6 B portions schematic enlarged-scale view.
The structural representation of each part that Fig. 9 is upper shell and is connected with upper shell.
Figure 10 is the structural representation of lower housing section.
Figure 11 is the cross section structure diagram of lower housing section.
Figure 12 is the decomposition texture schematic diagram of undercarriage part.
Figure 13 is the cross section structure diagram of undercarriage part.
5th, electric automobile；5a, wire-winding unit；51st, Wiinding cartridge；511st, line mouthful is crossed；52nd, coiling electric motor；53rd, wire spool；54、
Lid；6th, wire；9th, aircraft；91st, main part；91a, upper shell；91b, lower house；910th, fan installation portion；9101st, upper branch
Frame；9102nd, lower carriage；9103rd, battery installation portion；9104th, circuit board installation cavity；9105th, fresh air inlet；9106th, vent；
911st, vane is gone out；9110th, rise and fall Holder joint；9111st, vane upper shell；9112nd, vane lower house；91121st, interior curved wall；
91122nd, dowel；91123rd, air outlet guard board；91124th, training wall；912nd, connecting tube；9121st, the 3rd motor mounting plate；9122、
Valve plate guide rod；9123rd, baffle plate；913rd, the first cover plate；92nd, battery；93rd, undercarriage；931st, connection pipe body；9311st, hinged seat；
9312nd, strip shape gob；932nd, sliding tube；9321st, piston；9322nd, articulated joint；933rd, sealing cap；9331st, spring locating rod；934、
Connecting rod；935th, support bar；9351st, connecting rod tank；936th, the second electromagnet；937th, spring；94th, air intake cover；941st, electromagnet；
951st, upper driving fan；952nd, lower driving fan；96th, adjusting part；961st, the 3rd motor；962nd, screw rod；963rd, valve plate；97、
Control board；98th, charging rod；981st, permanent magnet.
Embodiment
Embodiment 1
According to Fig. 1 to 3, the present embodiment is a kind of electric car electric energy shared system, includes electric automobile 5, is mounted in
Aircraft on electric automobile and the wire 6 being connected between electric automobile and aircraft.
The aircraft upper end or lower end, which are provided with, is provided with concentric setting on permanent magnet a981, the permanent magnet a
Two electrode a；The aircraft lower end or upper end, which are provided with, is provided with two that concentric is set on electromagnet, the electromagnet
Electrode b；Electrically connected between two aircraft by electrode a, electrode b.
Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is with installing on board the aircraft
The input of boost module electrically connect, the electrode a, input, output ends of the electrode b respectively with boost module are electrically connected.
The boost module is brought the voltage up to the rated voltage of charging to charge to the electric automobile for needing to charge.
Describe for convenience, following electric automobile a is need the electric automobile charged, and electric automobile b is total to provide electricity
The electric automobile enjoyed, a, b limit only for the purposes of distinguishing without substantial.
When electric automobile a electricity is less than setting value, electric automobile it is automatic or in the case where user manually operates to server
Charge request is sent, server sends charge request to each electric automobile b close to electric automobile a, while server is by electricity
Electrical automobile a positional information and driving path is sent to electric automobile b, and electric automobile b is by its corresponding user's artificial selection
No offer electric energy is shared；First confirms that provide the shared electric automobile b of electric energy travels close to electric automobile a, in electric automobile b
When being less than setting value with the distance between electric automobile a, the aircraft on electric automobile a and electric automobile b flies to electric automobile a
The top of position between electric automobile b, and the electricity of the electrode b and electric automobile a of electric automobile b aircraft aircraft
Pole a is electrically connected.
When the distance between electric automobile a and electric automobile b exceedes setting value, electric automobile a and electric automobile b are each
The aircraft of carrying is mutually disengaged.
The touch-screen electrically connected with the control system of electric automobile is provided with the electric automobile, charging is sent to artificial
Request, receives charge request, display driving path etc..Control system, touch-screen as electric automobile etc. are prior art,
And be not emphasis of the present invention, it will not be repeated here.
The electromobile at top is provided with a wire-winding unit 5a, and the wire-winding unit includes upper end open
Wiinding cartridge 51, is rotatably installed in the wire spool 53 in Wiinding cartridge, and be connected to the lid 54 of the magnetic material of Wiinding cartridge upper end.
Centre position is provided with a coiling electric motor 52 in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, it is described around
The rotor of line motor is fixedly connected with wire spool.
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with
Slide the annular electrode b electrically connected with two annular electrode a, the battery of the annular electrode a and electric automobile or
Charge controller is electrically connected, and the wire is electrically connected with annular electrode b.
The Wiinding cartridge side offers and crosses line mouthful 511 for what wire was passed through.
Embodiment 2
With reference to shown in Fig. 4 to Figure 11, 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 912 for four equidistant arrangements that dress portion is connected, and be connected to each connecting tube outer end and be connected with correspondence position
What pipe was 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 91121, and the inner circumferential of the interior curved wall is connected with an air-out by multiple dowels 91122
Baffle plate, air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；The interior curved wall 91121 and air outlet guard board 91123
Between form 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 vane lower house it is interior
Week is training wall 91124 wide at the top and narrow at the bottom positioned at the lower section in air-out gap, 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 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 is connected with the air intake cover 94 of a semiellipse spherical shape, air intake cover and uniformly forms bar
The air inlet of shape.
The lower, outer perimeter of the fan installation portion is to be connected with and control on battery installation portion 9103, battery installation portion
The battery 92 of circuit board electrical connection；The main part upper end of the aircraft is provided with camera, and main part lower end is provided with
Lower camera, the upper camera, lower camera are electrically connected with control board respectively.
The upper camera, lower camera are used to that between the state of real-time monitored aircraft, two aircraft people can be passed through
Work manipulation is achieved a butt joint in the air, and the aerial automatic butt of two aircraft can also be realized by machine vision technique.
It is a circuit board installation cavity 9104, the control to be located at the top of battery installation portion on the fan installation portion
Circuit board is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with a first annular cover plate 913；Institute
The upper surface for stating circuit board installation cavity uniformly forms the fresh air inlet 9105 connected with fan installation portion, and the circuit board is installed
The lateral wall of chamber uniformly forms vent 9106.
The electromagnet is arranged at the top of air intake cover, and the electrode b is arranged on electromagnet upper end, the electromagnet and control
Circuit board is electrically connected；The lower carriage lower end is connected with charging rod 98, and the permanent magnet a is arranged on charging rod bottom, described
Electrode a is arranged on permanent magnet a981 lower ends.
Between two aircraft by permanent magnet a sucked with cold electromagnet together with and realize electrode a and electrode b
Electrically connect；Produced when the electromagnet is powered makes two aircraft disengagings with magnetic field reverse permanent magnet a.
Aircraft provides driving force, upper driving fan production by the upper driving fan in fan installation portion, lower driving fan
Raw fraction is blown out downwards from each air-out gap for going out vane, and combines the air-out that adjusting part adjustment each goes out vane
Speed, so as to realize the horizontal flight or steering of aircraft, due to going out vane positioned at each of aircraft periphery and only play tune
The effect of whole attitude of flight vehicle, without the fan for being provided with power, goes out when vane produces touching with foreign object and is not easily caused aircraft
Out of control or produce injury to human or animal, security is good.The similar four-axle aircraft of aircraft outward appearance, therefore with four-axle aircraft
It is named, four go out the function that vane i.e. so-called " four axles " only plays regulation posture, therefore this aircraft substantially should be single shaft
Aircraft.
Further, it is described go out vane air-out gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward in the lump, so fly
When the part in air-out gap is stopped in row device flight course, the overall airflow influence that air-out gap is formed is small, is conducive to flying
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out axial direction and the level of vane
The angle of 5-20 degree is formed between direction, and goes out horizontal wind-force and upper driving fan that the wind of the air-out gap blowout of vane is produced
Fan blade rotation direction it is opposite.Pass through such design so that the wind energy for going out the air-out gap blowout of vane enough offsets drive
The reaction force produced when dynamic fan and the rotation of lower driving fan；Also, change air-out by adjusting each adjusting part simultaneously
Ring goes out wind velocity, and the overall forward or reverse of aircraft can be achieved.Make one by adjusting one or two adjusting part
Or two go out vane go out wind velocity, aircraft can be achieved generally in heeling condition, aircraft can be so driven in level
Fly in direction.
A small amount of air-flow of the fan installation portion enters from fresh air inlet and from vent discharge, plays scattered to control board
Heat effect.
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint 9110 of rising and falling, each described undercarriage
A undercarriage 93 is respectively connected with joint；The undercarriage is provided with to suck the second electromagnet in electromobile at top
936。
When aircraft does not work, aircraft is sucked in electromobile at top by the second electromagnet of undercarriage lower end
On lid.
Embodiment 3
With reference to Figure 12 to Figure 13, 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.
Embodiment 4
The present embodiment is a kind of electric car electric energy shared system, includes electric automobile, is mounted in the flight on electric automobile
Device and the wire being connected between electric automobile and aircraft.
It is provided between two electrodes, two aircraft and is electrically connected by electrode on each aircraft.
Described wire one end couples with the storage battery of electric automobile, the other end of the wire and carry-on electrode
Electrically connect.
When two electric automobiles share electric energy, the aircraft that two electric automobiles are each carried is between two electric automobiles
The overhead of position is relatively fixed and electrically connects the electrode between two aircraft.
Electrode described in the present embodiment can be the metal electrode film that is electrically connected by contact or by wireless
Charging technique carries out the wireless charging transmitting of electric energy transmission, receiving module.
Claims (10)
1. a kind of electric car electric energy shared system, it is characterised in that：Include electric automobile, be mounted in flying on electric automobile
Row device and the wire being connected between electric automobile and aircraft；
The aircraft upper end or lower end are provided with two electrodes that concentric setting is provided with permanent magnet a, the permanent magnet a
a；The aircraft lower end or upper end are provided with two electrode b that concentric setting is provided with electromagnet, the electromagnet；Two
Electrically connected between individual aircraft by electrode a, electrode b；
Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is with being arranged on carry-on liter
The input of die block is electrically connected, and the electrode a, input, output ends of the electrode b respectively with boost module are electrically connected.
2. a kind of electric car electric energy shared system as claimed in claim 1, it is characterised in that：The electromobile at top peace
Equipped with a wire-winding unit, the wire-winding unit includes the Wiinding cartridge of a upper end open, is rotatably installed in Wiinding cartridge
Wire spool, and it is connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor
Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two
The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute
Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through.
3. a kind of electric car electric energy shared system as claimed in claim 1, it is characterised in that：The aircraft includes master
Body portion, the main part includes the fan installation portion of tubular, be connected to fan installation portion periphery and with fan installation portion phase
The connecting tube of four equidistant arrangements of connection, and be connected to each connecting tube outer end and be connected with correspondence position connecting tube
Go out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper
Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
To opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described
Valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube
Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube
The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port.
4. a kind of electric car electric energy shared system as claimed in claim 3, it is characterised in that：Under the fan installation portion
Portion periphery is to be connected with the battery electrically connected with control board on battery installation portion, battery installation portion；The flight
The main part upper end of device is provided with camera, and main part lower end is provided with lower camera, the upper camera, lower camera point
Do not electrically connected with control board.
5. a kind of electric car electric energy shared system as claimed in claim 3, it is characterised in that：Go out vane inner circumferential described in each
Holder joint 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；It is described
Undercarriage 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,
The sliding tube in connection pipe body is slidably mounted on, the support bar being connected is rotated close to Holder joint one end of rising and falling with connection pipe body, even
Be connected on support bar away from Holder joint one end of rising and falling sucking the second electromagnet in automobile top, 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.
6. a kind of electric car electric energy shared system as claimed in claim 3, it is characterised in that：The electromagnet be arranged on into
At the top of fan housing, the electrode b is arranged on electromagnet upper end, and the electromagnet is electrically connected with control board；Under the lower carriage
End is connected with charging rod, and the permanent magnet a is arranged on charging rod bottom, and the electrode a is arranged on permanent magnet a lower ends；
Between two aircraft by permanent magnet a sucked with cold electromagnet together with and realize electrode a and electrode b electricity
Connection；Produced when the electromagnet is powered makes two aircraft disengagings with magnetic field reverse permanent magnet a.
7. a kind of electric car electric energy shared system, it is characterised in that：Include electric automobile, be mounted in flying on electric automobile
Row device and the wire being connected between electric automobile and aircraft；
The aircraft upper end or lower end are provided with two electrodes that concentric setting is provided with permanent magnet a, the permanent magnet a
a；The aircraft lower end or upper end are provided with two electrode b that concentric setting is provided with electromagnet, the electromagnet；Two
Electrically connected between individual aircraft by electrode a, electrode b；
Described wire one end couples with the storage battery of electric automobile, and the other end of the wire is with being arranged on carry-on liter
The input of die block is electrically connected, and the electrode a, input, output ends of the electrode b respectively with boost module are electrically connected；
The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes the coiling of a upper end open
Box, is rotatably installed in the wire spool in Wiinding cartridge, and be connected to the lid of the magnetic material of Wiinding cartridge upper end；
Centre position is provided with a coiling electric motor in the Wiinding cartridge, and coiling electric motor is external rotor electric machine, the coiling electric motor
Rotor be fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower surface of the wire spool is provided with and two
The individual annular electrode a slides the annular electrode b electrically connected, and the annular electrode a couples with the storage battery of electric automobile, institute
Wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers and crosses line mouthful for what wire was passed through；
The aircraft includes main part, and the main part includes the fan installation portion of tubular, is connected to fan installation
Portion periphery and the connecting tube for four equidistant arrangements being connected with fan installation portion, and be connected to each connecting tube outer end and with
What correspondence position connecting tube was connected goes out vane；
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan；It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed；
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper
Drive the blast superatmospheric between fan so that go out and blast is formed in vane；
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected；Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree；
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
To opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight；It is described
Valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube；The connecting tube
Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate；Bottom is connected with upper end towards going out in the connecting tube
The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate；
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively；
The main part is that upper shell and lower house are tightly connected composition；
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port；
The lower, outer perimeter of the fan installation portion is to be connected with battery installation portion, battery installation portion and control board electricity
The battery of connection；The main part upper end of the aircraft is provided with camera, and main part lower end is provided with lower camera, institute
Camera, lower camera is stated to electrically connect with control board respectively；
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 the second of automobile top
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.
8. one kind realizes that electric car electric energy is shared using any one of claim 1 to the 7 electric car electric energy shared system
Method, it is characterised in that：When electric automobile a electricity is less than setting value, electric automobile is automatic or is manually operated in user
Lower to send charge request to server, server sends charge request to each electric automobile b close to electric automobile a, simultaneously
Electric automobile a positional information and driving path are sent to electric automobile b by server, and electric automobile b is by its corresponding user
Whether artificial selection, which provides electric energy, is shared；First confirms that provide the shared electric automobile b of electric energy travels close to electric automobile a,
When distance between electric automobile b and electric automobile a is less than setting value, the aircraft on electric automobile a and electric automobile b flies
To the top of the position between electric automobile a and electric automobile b, and the electrode b and electric automobile a of electric automobile b aircraft
The electrode a of aircraft electrically connect.
9. electric car electric energy sharing method as claimed in claim 8, it is characterised in that：As electric automobile a and electric automobile b
The distance between exceed setting value when, the aircraft that electric automobile a and electric automobile b are each carried mutually is disengaged.
10. a kind of electric car electric energy shared system, it is characterised in that：Include electric automobile, be mounted on electric automobile
Aircraft and the wire being connected between electric automobile and aircraft；
It is provided between two electrodes, two aircraft and is electrically connected by electrode on each aircraft；
Described wire one end couples with the storage battery of electric automobile, the other end of the wire and carry-on electrode Electricity Federation
Connect；
When two electric automobiles share electric energy, the aircraft that two electric automobiles are each carried position between two electric automobiles
Overhead be relatively fixed and electrically connect the electrode between two aircraft.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
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Cited By (3)
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| CN108608874A (en) * | 2018-04-03 | 2018-10-02 | 徐东云 | A kind of electric vehicle autonomous contact synchronous charging device between advancing |
| 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 |
| DE102019131194A1 (en) * | 2019-11-19 | 2021-05-20 | Bayerische Motoren Werke Aktiengesellschaft | Method for charging an accumulator of a motor vehicle |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112406583B (en) * | 2020-11-12 | 2022-05-31 | 观典防务技术股份有限公司 | Charging equipment special for unmanned aerial vehicle and use method |
| CN114347825B (en) * | 2021-12-29 | 2024-02-02 | 为梦充电(重庆)科技发展有限公司 | Shared charging pile capable of realizing shared charging and server |
| CN117485198B (en) * | 2023-12-29 | 2024-03-15 | 南京轶诺科技有限公司 | Energy storage sharing and distributing method and system based on vehicle-mounted power battery |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN108146287B (en) | 2020-06-09 |
| CN107176052B (en) | 2018-08-14 |
| CN108146287A (en) | 2018-06-12 |
| CN108297726B (en) | 2020-06-09 |
| CN108297726A (en) | 2018-07-20 |
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