CN107117301B - Charging system for electric automobile - Google Patents
Charging system for electric automobile Download PDFInfo
- Publication number
- CN107117301B CN107117301B CN201710489021.8A CN201710489021A CN107117301B CN 107117301 B CN107117301 B CN 107117301B CN 201710489021 A CN201710489021 A CN 201710489021A CN 107117301 B CN107117301 B CN 107117301B
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- CN
- China
- Prior art keywords
- vane
- fan
- aircraft
- mounting portion
- electric automobile
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- 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
- B60L5/00—Current collectors for power supply lines of electrically-propelled vehicles
- B60L5/38—Current collectors for power supply lines of electrically-propelled vehicles for collecting current from conductor rails
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/20—Operating mechanisms mechanical
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses a kind of electric automobile electric power system, include the multiple power transmission rods for being fixedly mounted on both sides of the road, transmission guide rail between each power transmission rod of road homonymy, can be close to the aircraft of flight below transmission guide rail, and be connected between electric automobile and aircraft electric energy to be transferred to the conducting wire on electric automobile from transmission guide rail；The transmission guide rail includes two to be arranged in parallel, and the aircraft upper end is connected with slides the trolley pole electrically connected with two transmission guide rails respectively, and the trolley pole is electrically connected with described conducting wire one end；The present invention is close to transmission guide rail by aircraft and flies, by trolley pole by electric energy through on wire transmission to electric automobile, electric automobile is realized without stopping the function that can be charged, and electric automobile aircraft in the case of fully charged or other can fly away from transmission guide rail at any time, freely travelling for electric automobile will not be caused to limit.
Description
Technical field
The invention belongs to electric automobile corollary system field, and in particular to a kind of charging system for electric automobile.
Background technology
With the popularization of electric automobile, electric automobile charging inconvenience the problem of also increasingly highlight；Purchase electric automobile 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 travels, user is also required to pay attention to very much the remaining capacity of electric automobile, otherwise easily occurs on the way
Situation about casting anchor without electricity.And what similar two-wheeled battery truck was taken sets the scheme of charging equipment in roadside, 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 may cause traffic congestion, and on the other hand, electric automobile 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.
The content of the invention
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, provide a kind of charging conveniently, and
The electric automobile electric power system of user hours underway is not delayed.
To realize the purpose of the present invention, it is achieved using following technical scheme：A kind of charging system for electric automobile, including
There are the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail between each power transmission rod of road homonymy, energy
Enough be close to the aircraft of flight below transmission guide rail, and be connected between electric automobile and aircraft to by electric energy from defeated
Conductance rail is transferred to the conducting wire on electric automobile；
The transmission guide rail includes two to be arranged in parallel, and the aircraft upper end is connected with leads with two transmissions of electricity respectively
Rail slides the trolley pole electrically connected, and the trolley pole is electrically connected with described conducting wire one end.
Preferably：The side in the power transmission rod top towards direction among road is fixedly connected with horizontally disposed
Cross bar, the cross bar lower end are connected with insulator, and the transmission guide rail is connected to insulator lower end；The lower end of the transmission guide rail
Face is arc-shaped in middle fovea superior.
Preferably：The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes one
The Wiinding cartridge of a upper end opening, the wire spool being rotatably installed in Wiinding cartridge, and it is connected to the magnetic material of Wiinding cartridge upper end
Box 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
The rotor of motor is fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower face of the wire spool is provided with
The annular electrode b electrically connected, the storage battery Electricity Federation of the annular electrode a and electric automobile are slided with two annular electrode a
Connect, the conducting wire is electrically connected with annular electrode b；
The Wiinding cartridge side is offered crosses line mouth for what conducting wire passed through.
Preferably：The aircraft includes main part, and the main part includes the fan installation of tubular
Portion, is connected to the connecting tube of fan mounting portion periphery and four equidistant arrangements being connected with fan mounting portion, and is connected to
Each connecting tube outer end and go out vane with what correspondence position connecting tube was connected；
Upper bracket is connected with above connecting tube in the fan mounting portion, driving is installed on the upper bracket
Fan；Lower carriage is connected with below connecting tube in the fan mounting portion, lower driving wind is installed on the lower carriage
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, is located at upper driving fan in the fan mounting portion
Wind pressure superatmospheric between lower driving fan so that go out and wind pressure is formed in vane；
It is described go out vane include the vane upper shell and vane lower housing shell of sealed connection, in the vane lower housing shell inner circumferential
End forms 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 by multiple dowels
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 bottom width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing shell 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 angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane produces
Rotation direction is opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane outlet air speed, the tune in each connecting tube
Section component includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected 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 above-below direction in connecting tube；The company
Adapter internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd 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；Lower part is connected with a upper end court 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 3rd motor are electrically connected with control board respectively；
The main part is tightly connected and forms for upper shell and lower housing shell；The trolley pole lower end is fixedly connected on described
Close to the position for going out vane on housing；
The main part upper end is connected with the air intake cover of a semiellipse spherical shape, and strip is uniformly formed on air intake cover
Air inlet.
Preferably：The lower, outer perimeter of the fan mounting portion is storage battery mounting portion, is connected on storage battery mounting portion
It is connected to the storage battery being electrically connected with control board；The upper end of the aircraft is provided with camera, the camera and control
Circuit board electrical connection.
Preferably：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
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
Holder joint of rising and falling is with going 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 away from Holder joint one end of rising and falling inhaling close to the supporting rod for Holder joint one end rotation connection of rising and falling
Tightly in the second electromagnet of automobile top, and the connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of 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 slip pipe outer wall medium position is connected with
Articulated joint, described connecting rod one end are rotatablely connected with articulated joint, side wall shaping of the connection pipe body away 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 away from Holder joint of rising and falling is fixedly connected with sealing cap, seals
The inner of cap is connected with spring positioning bar, and spring is arranged with the spring positioning bar, and the both ends of the spring is against respectively
Between piston and sealing cap the inner；The connecting rod appearance that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod
Groove；
The supporting rod is in unfolded state when the spring is in extended configuration, 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 also provides a kind of charging system for electric automobile, includes the multiple transmissions of electricity for being fixedly mounted on both sides of the road
Bar, the transmission guide rail between each power transmission rod of road homonymy, can be close to the aircraft to fly below transmission guide rail,
And be connected between electric automobile and aircraft electric energy to be transferred to the conducting wire on electric automobile from transmission guide rail；
The transmission guide rail includes two to be arranged in parallel, and the aircraft upper end is connected with leads with two transmissions of electricity respectively
Rail slides the trolley pole electrically connected, and the trolley pole is electrically connected with described conducting wire one end；
The side in the power transmission rod top towards direction among road is fixedly connected with horizontally disposed cross bar, the cross bar
Lower end is connected with insulator, and the transmission guide rail is connected to insulator lower end；The lower face of the transmission guide rail is in middle fovea superior
It is arc-shaped；
The electromobile at top is provided with a wire-winding unit, the wire-winding unit include upper end opening around
Wire box, the wire spool being rotatably installed in Wiinding cartridge, and it is connected to the box 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
The rotor of motor is fixedly connected with wire spool；
The Wiinding cartridge bottom is provided with two annular electrode being arranged concentrically a, and the lower face of the wire spool is provided with
The annular electrode b electrically connected, the storage battery Electricity Federation of the annular electrode a and electric automobile are slided with two annular electrode a
Connect, the conducting wire is electrically connected with annular electrode b；
The Wiinding cartridge side is offered crosses line mouth for what conducting wire passed through；
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 for 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 correspondence position connecting tube was connected；
Upper bracket is connected with above connecting tube in the fan mounting portion, driving is installed on the upper bracket
Fan；Lower carriage is connected with below connecting tube in the fan mounting portion, lower driving wind is installed on the lower carriage
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, is located at upper driving fan in the fan mounting portion
Wind pressure superatmospheric between lower driving fan so that go out and wind pressure is formed in vane；
It is described go out vane include the vane upper shell and vane lower housing shell of sealed connection, in the vane lower housing shell inner circumferential
End forms 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 by multiple dowels
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 bottom width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing shell 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 angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane produces
Rotation direction is opposite；
It is provided with to adjust the adjusting part that correspondence position goes out vane outlet air speed, the tune in each connecting tube
Section component includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected 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 above-below direction in connecting tube；The company
Adapter internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd 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；Lower part is connected with a upper end court 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 3rd motor are electrically connected with control board respectively；
The main part is tightly connected and forms for upper shell and lower housing shell；The trolley pole lower end is fixedly connected on described
Close to the position for going out vane on housing；
The main part upper end is connected with the air intake cover of a semiellipse spherical shape, and strip is uniformly formed on air intake cover
Air inlet；
The lower, outer perimeter of the fan mounting portion is storage battery mounting portion, is connected with storage battery mounting portion and control circuit
The storage battery that plate is electrically connected；The upper end of the aircraft is provided with camera, and the camera is electrically connected with control board；
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, each Holder joint of rising and falling
On be respectively 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
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 away from Holder joint one end of rising and falling sucking in automobile top
Second electromagnet, and the connecting rod with being rotatablely connected in the middle part of sliding tube, in the middle part of 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 slip pipe outer wall medium position is connected with
Articulated joint, described connecting rod one end are rotatablely connected with articulated joint, side wall shaping of the connection pipe body away 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 away from Holder joint of rising and falling is fixedly connected with sealing cap, seals
The inner of cap is connected with spring positioning bar, and spring is arranged with the spring positioning bar, and the both ends of the spring is against respectively
Between piston and sealing cap the inner；The connecting rod appearance that the connecting rod is accommodated in supporting rod collapsed state is formed on the supporting rod
Groove；
The supporting rod is in unfolded state when the spring is in extended configuration, 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.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention is close to transmission guide rail by aircraft and flies,
By trolley pole by electric energy through on wire transmission to electric automobile, realizing electric automobile without stopping the work(that can be charged
Can, and electric automobile aircraft in the case of fully charged or other can fly away from transmission guide rail at any time, and will not be to electronic vapour
Freely travelling for car causes to limit.
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 box lid of component, when aircraft works, the energization of the second electromagnet, which produces the magnetic field reverse with the box lid of magnetic material, to be made
Aircraft departs from electric automobile.
When electric automobile needs charging, the control system of electric automobile sends signal to aircraft, flies to aircraft
Below transmission guide rail, trolley pole is formed with transmission guide rail sliding contact and electrically connect；The process of electric automobile is flown away from aircraft
In, control system controls the coiling electric motor of wire-winding unit to rotate at the same time makes conducting wire be released from wire spool；Electric automobile has charged
Bi Hou, aircraft fly back to electromobile at top, while coiling electric motor is rotated backward and made on conducting wire wraparound wire spool.
The aircraft provides driving force, the part that upper driving fan produces by the upper driving fan in fan mounting portion
Air-flow from it is each go out vane outlet air gap downwards blow out, and combine adjusting part adjustment and each go out vane and go out wind velocity, from
And realize the horizontal flight or steering of aircraft, due to positioned at aircraft periphery it is each go out vane only play adjustment aircraft
The effect of posture, without the fan for being provided with power, go out not easily leading to when vane produces touching with foreign object aircraft it is out of control or
Injury is produced to human or animal, security is good.Similar to four-axle aircraft, four go out vane and only play adjusting appearance the aircraft appearance
The function of state, therefore the present invention substantially should be single shaft 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 in the lump, so fly
When the part in outlet air gap is stopped in row device flight course, the overall 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 angle of 5-20 degree is formed square between, and the horizontal wind-force that produces of the wind for going out the outlet air gap blowout of vane and upper driving wind
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
Driving fan, or reaction force caused by upper driving fan and the rotation of lower driving fan；Also, by adjusting each tune at the same time
Section component change vane go out wind velocity, it can be achieved that the overall forward or reverse of aircraft.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 can so drive generally in heeling condition
Dynamic aircraft flies in the horizontal direction.
The undercarriage is packed up or is unfolded as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out
Wind pressure in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drives connecting rod one end to sealing cap
Direction is moved, so that supporting rod lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft
During landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved together with piston toward hinged seat direction, so that sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, so that supporting rod lower end turns to extreme position to hinged seat one end, so that
Undercarriage is set to be in unfolded state.
Brief description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is the C portions schematic enlarged-scale view of Fig. 1.
Fig. 3 is structure diagram when aircraft is rested on electric automobile.
Fig. 4 is the decomposition texture schematic diagram of wire-winding unit.
Fig. 5 is the structure diagram of aircraft shutdown status.
Fig. 6 is the structure diagram of aircraft flight state.
Fig. 7 is the schematic cross-sectional view of aircraft.
Fig. 8 is the A portions schematic enlarged-scale view of Fig. 7.
Fig. 9 is the B portions schematic enlarged-scale view of Fig. 7.
The structure diagram of each component that Figure 10 is upper shell and is connected with upper shell.
Figure 11 is the structure 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.
1st, power transmission rod；11st, cross bar；12nd, insulator；2nd, transmission guide rail；5th, electric automobile；5a, wire-winding unit；51st, coiling
Box；511st, line mouth is crossed；52nd, coiling electric motor；53rd, wire spool；54th, box lid；6th, conducting wire；9th, aircraft；91st, main part；91a, on
Housing；91b, lower housing shell；910th, fan mounting portion；9101st, upper bracket；9102nd, lower carriage；9103rd, storage battery mounting portion；
9104th, circuit board installation cavity；9105th, air inlet hole；9106th, vent；911st, vane is gone out；9110th, rise and fall Holder joint；9111st, wind
Ring upper shell；9112nd, vane lower housing shell；91121st, interior curved wall；91122nd, dowel；91123rd, air outlet guard board；91124th, water conservancy diversion
Wall；912nd, connecting tube；9121st, the 3rd motor mounting plate；9122nd, valve plate guide rod；9123rd, baffle；913rd, the first cover board；92nd, store
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 positioning bar；934th, connecting rod；935th, supporting rod；9351st, connecting rod tank；936、
Second electromagnet；937th, spring；94th, air intake cover；941st, camera；951st, upper driving fan；952nd, lower driving fan；96th, adjust
Save component；961st, the 3rd motor；962nd, screw rod；963rd, valve plate；97th, control board；98th, trolley pole.
Embodiment
Embodiment 1
According to Fig. 1 to 5, the present embodiment is a kind of charging system for electric automobile, includes and is fixedly mounted on road two
Multiple power transmission rods 1 of side, the transmission guide rail 2 between each power transmission rod of road homonymy, can be close under transmission guide rail
The aircraft 9 of Fang Feihang, and be connected between electric automobile and aircraft electric energy is transferred to electricity from transmission guide rail
Conducting wire 6 on electrical automobile.The transmission guide rail is connected with power supply network.
The transmission guide rail includes two to be arranged in parallel, and the aircraft upper end is connected with leads with two transmissions of electricity respectively
Rail slides the trolley pole 98 electrically connected, and the trolley pole is electrically connected with described conducting wire one end.
The side in the power transmission rod top towards direction among road is fixedly connected with horizontally disposed cross bar 11, the horizontal stroke
Bar lower end is connected with insulator 12, and the transmission guide rail is connected to insulator lower end；The lower face of the transmission guide rail is in centre
Fovea superior it is arc-shaped.
The electromobile at top is provided with a wire-winding unit 5a, and the wire-winding unit includes upper end opening
Wiinding cartridge 51, the wire spool 53 being rotatably installed in Wiinding cartridge, and it is connected to the box 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 face of the wire spool is provided with
Slide the annular electrode b electrically connected with two annular electrode a, the storage battery of the annular electrode a and electric automobile or
Charge controller electrically connects, and the conducting wire is electrically connected with annular electrode b.
The Wiinding cartridge side is offered crosses line mouth 511 for what conducting wire passed through.
In addition, the aircraft is also powered by transmission guide rail.
The present invention is close to transmission guide rail by aircraft and flies, by trolley pole by electric energy through wire transmission to electric automobile
On, electric automobile is realized without stopping the function that can be charged, and electric automobile is in fully charged or other situations
Lower aircraft can fly away from transmission guide rail at any time, and freely travelling for electric automobile will not be caused to limit.
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 box lid of component, when aircraft works, the energization of the second electromagnet, which produces the magnetic field reverse with the box lid of magnetic material, to be made
Aircraft departs from electric automobile.
When electric automobile needs charging, the control system of electric automobile sends signal to aircraft, flies to aircraft
Below transmission guide rail, trolley pole is formed with transmission guide rail sliding contact and electrically connect；The process of electric automobile is flown away from aircraft
In, control system controls the coiling electric motor of wire-winding unit to rotate at the same time makes conducting wire be released from wire spool；Electric automobile has charged
Bi Hou, aircraft fly back to electromobile at top, while coiling electric motor is rotated backward and made on conducting wire wraparound wire spool.
Embodiment 2
With reference to shown in Fig. 6 to Figure 12, the present embodiment makes following improvement on the basis of embodiment 1：The aircraft bag
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 912 for four equidistant arrangements that fan mounting portion is connected, and it is connected to each connecting tube outer end and and correspondence position
What connecting tube was connected goes out vane 911.
Upper bracket 9101 is connected with above connecting tube in the fan mounting portion, is provided with the upper bracket
Driving fan 951；Lower carriage 9102 is connected with below connecting tube in the fan mounting portion, is installed on the lower carriage
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 wind pressure is formed in vane.
It is described go out vane include the vane upper shell 9111 and vane lower housing shell 9112 of sealed connection, the vane lower casing
Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board by multiple dowels 91122,
Air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end；Shape between the interior curved wall 91121 and air outlet guard board 91123
Into outlet air gap wide at the top and narrow at the bottom, the bottom width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower housing shell 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 angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind for going out the outlet air gap blowout of vane produces
Rotation direction is opposite.
It is provided with to adjust the adjusting part 96 that correspondence position goes out vane outlet air speed in each 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；For the valve plate upper periphery close to connection inside pipe wall, 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
Lower part is connected with a upper end 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 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 housing shell 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, and bar is uniformly formed on air intake cover
The air inlet of shape.
The lower, outer perimeter of the fan mounting portion is storage battery mounting portion 9103, is connected with and controls on storage battery mounting portion
The storage battery 92 of circuit board electrical connection；The upper end of the aircraft is provided with camera 941, the camera and control board
It is electrically connected.
The camera shooting obtains aircraft with respect to the position of transmission guide rail, can be by manual operation remote control aircraft
Fly, can also be flown automatically along transmission guide rail by aircraft by machine vision technique along transmission guide rail.
Top on the fan mounting portion positioned at storage battery mounting portion is a circuit board installation cavity 9104, the control
Circuit board is installed in circuit board installation cavity, and the circuit board installation cavity lower end is connected with a first annular cover board 913；Institute
The upper surface for stating circuit board installation cavity uniformly forms the air inlet hole 9105 connected with 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 the upper driving fan in fan mounting portion, lower driving fan
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, so as to fulfill 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, without the fan for being provided with power, goes out when vane produces touching with foreign object and does not easily lead to aircraft
It is out of control or good to human or animal's generation injury, security.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 single shaft
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 in the lump, so fly
When the part in outlet air gap is stopped in row device flight course, the overall 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 angle of 5-20 degree is formed square between, and the horizontal wind-force that produces of the wind for going out the outlet air gap blowout of vane and upper driving wind
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
Reaction force caused by driving fan and the rotation of lower driving fan；Also, change by adjusting each adjusting part at the same time
Vane goes out wind velocity, it can be achieved that the overall forward or reverse of aircraft.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 can so drive aircraft in water generally in heeling condition
Square to flight.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, control board is played scattered
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 undercarriage
A undercarriage 93 is respectively connected with connector；The undercarriage is equipped 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 box lid.
Embodiment 3
With reference to 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 away from connecting tube forms Holder joint 9110 of rising and falling, and being respectively connected with one in each Holder joint of rising and falling rises and falls
Frame 93；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 what is be connected inside vane
Connection pipe body 931, the sliding tube 932 being slidably mounted in connection pipe body, rotates with connection pipe body close to Holder joint one end of rising and falling
The supporting rod 935 of connection, be connected on supporting rod away from Holder joint one end of rising and falling sucking the of electromobile at top
Two electromagnet 936, and the connecting rod 934 with being rotatablely connected in the middle part of sliding tube, in the middle part of 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, the slip pipe outer wall middle part position close to Holder joint one end of rising and falling
Put and be connected with articulated joint 9322, described connecting rod one end is rotatablely connected with articulated joint, and 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 912 body of connecting tube away from Holder joint of rising and falling is consolidated
Surely sealing cap 933 is connected with, the inner of sealing cap is connected with spring positioning bar 9331, is arranged with the spring positioning bar
Spring 937, the both ends of the spring are against between piston and sealing cap the inner respectively；Form on the supporting rod and received in supporting rod
The connecting rod tank 9351 of the connecting rod is accommodated during the state of rising.
The supporting rod is in unfolded state when the spring is in extended configuration, 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 is packed up or is unfolded as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out
Wind pressure in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drives connecting rod one end to sealing cap
Direction is moved, so that supporting rod lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft
During landing, the wind pressure gone out in vane reduces, and spring drives sliding tube to be moved together with piston toward hinged seat direction, so that sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, so that supporting rod lower end turns to extreme position to hinged seat one end, so that
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 causes spring to stretch
After length, supporting rod turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each supporting rod is equal
In stable state.
Claims (2)
- A kind of 1. charging system for electric automobile, it is characterised in that：Include the multiple power transmission rods for being fixedly mounted on both sides of the road, pacify Transmission guide rail between each power transmission rod of road homonymy, can be close to the aircraft of flight below transmission guide rail, and Be connected between electric automobile and aircraft electric energy to be transferred to the conducting wire on electric automobile from transmission guide rail；The transmission guide rail includes two to be arranged in parallel, and the aircraft upper end is connected with to be slided with two transmission guide rails respectively The dynamic trolley pole electrically connected, the trolley pole are electrically connected with described conducting wire one end；The side in the power transmission rod top towards direction among road is fixedly connected with horizontally disposed cross bar, the cross bar lower end Insulator is connected with, the transmission guide rail is connected to insulator lower end；The lower face of the transmission guide rail is in the circle of middle fovea superior Arc；The electromobile at top is provided with a wire-winding unit, and the wire-winding unit includes the coiling of a upper end opening Box, the wire spool being rotatably installed in Wiinding cartridge, and it is connected to the box 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 face of the wire spool is provided with and two A annular electrode a slides the annular electrode b electrically connected, and the storage battery of the annular electrode a and electric automobile electrically connect, institute Conducting wire is stated to electrically connect with annular electrode b；The Wiinding cartridge side is offered crosses line mouth for what conducting wire passed through；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 for four equidistant arrangements being connected with fan mounting portion, and be connected to each connecting tube outer end and with What correspondence position connecting tube was connected goes out vane；Upper bracket is connected with above connecting tube in the fan mounting portion, driving wind is installed on the upper bracket Fan；Lower carriage is connected with below connecting tube in the fan mounting portion, lower driving fan is installed on the lower carriage； The upper driving fan is turned on the contrary, and installing the interior of driving fan part in the fan mounting portion with lower driving fan More than the internal diameter of the lower driving fan part of the interior installation of fan mounting portion, the fan mounting portion is interior to be located at upper driving fan with in footpath Wind pressure superatmospheric between driving fan so that go out and wind pressure is formed in vane；It is described go out vane include the vane upper shell and vane lower housing shell of sealed connection, the vane lower housing shell 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；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 bottom width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower housing shell 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 provided with to adjust the adjusting part that correspondence position goes out vane outlet air speed, the adjusting group in each 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 For valve plate upper periphery close to connection inside pipe wall, 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；Lower part is connected with upper end towards going out 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 3rd motor are electrically connected with control board respectively；The main part is tightly connected and forms for upper shell and lower housing shell；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 of a semiellipse spherical shape, uniformly formed on air intake cover strip into Air port.
- A kind of 2. charging system for electric automobile as claimed in claim 1, it is characterised in that：Outside the lower part of the fan mounting portion Week is storage battery mounting portion, and the storage battery being electrically connected with control board is connected with storage battery mounting portion；The aircraft Upper end is provided with camera, and the camera is electrically connected with control board.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810102346.0A CN108248850B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201710489021.8A CN107117301B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201810102350.7A CN108216609B (en) | 2017-06-23 | 2017-06-23 | Electric automobile charging system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710489021.8A CN107117301B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Related Child Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810102350.7A Division CN108216609B (en) | 2017-06-23 | 2017-06-23 | Electric automobile charging system |
| CN201810102346.0A Division CN108248850B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
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| Publication Number | Publication Date |
|---|---|
| CN107117301A CN107117301A (en) | 2017-09-01 |
| CN107117301B true CN107117301B (en) | 2018-05-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710489021.8A Active CN107117301B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
| CN201810102350.7A Active CN108216609B (en) | 2017-06-23 | 2017-06-23 | Electric automobile charging system |
| CN201810102346.0A Active CN108248850B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810102350.7A Active CN108216609B (en) | 2017-06-23 | 2017-06-23 | Electric automobile charging system |
| CN201810102346.0A Active CN108248850B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
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| DE102020208406A1 (en) | 2020-07-06 | 2022-01-13 | Volkswagen Aktiengesellschaft | Docking system and motor vehicle with docking system |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US7802755B2 (en) * | 2004-03-10 | 2010-09-28 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor guide-ring |
| CN201268234Y (en) * | 2008-01-17 | 2009-07-08 | 杨钧泰 | Power receiving multi-energy automobile |
| CN102306421B (en) * | 2011-06-30 | 2014-02-19 | 华北电力大学 | Motorway charging system of EV (electric vehicle) |
| CN102593899B (en) * | 2012-02-21 | 2014-03-12 | 北京联合大学 | Midway charging system for electric vehicle |
| US9475589B2 (en) * | 2013-12-20 | 2016-10-25 | Google Inc. | Systems and apparatus for winch drum mechanism |
| US20150180186A1 (en) * | 2013-12-20 | 2015-06-25 | Google Inc. | Systems and Apparatus for Cable Management |
| CN104999927A (en) * | 2014-04-21 | 2015-10-28 | 张利明 | Electrified road traffic route design method |
| CN105099003A (en) * | 2015-07-28 | 2015-11-25 | 联想(北京)有限公司 | Wireless charging method and corresponding device |
| CN106427596A (en) * | 2015-08-07 | 2017-02-22 | 姚舜 | Method for instantaneously supplying electricity for electric vehicle on highway |
| 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 |
| CN205178538U (en) * | 2015-10-12 | 2016-04-20 | 上海中科深江电动车辆有限公司 | Electric vehicle removes wireless charging system |
| CN205304274U (en) * | 2015-10-12 | 2016-06-08 | 上海中科深江电动车辆有限公司 | Wireless charging system of electric vehicle with remove high -altitude flight operation |
| US20170136887A1 (en) * | 2015-11-13 | 2017-05-18 | NextEv USA, Inc. | Electric vehicle aerial vehicle charging system and method of use |
| 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 |
| CN106314777B (en) * | 2016-08-29 | 2019-12-24 | 英华达（上海）科技有限公司 | Unmanned aerial vehicle |
| CN206050060U (en) * | 2016-09-14 | 2017-03-29 | 西北工业大学 | A kind of roller type Multi-stage damping reed pipe unmanned plane Shatter-resistant device |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN107117301A (en) | 2017-09-01 |
| CN108248850A (en) | 2018-07-06 |
| CN108248850B (en) | 2019-11-08 |
| CN108216609A (en) | 2018-06-29 |
| CN108216609B (en) | 2021-06-29 |
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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: Jiang Jiahui Address before: 310051 1, -10 5, No. 11, Ju Gong Road, Binjiang District Xi Xing street, Hangzhou, Zhejiang. Patentee before: HANGZHOU LIPU TECHNOLOGY Co.,Ltd. |
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