CN108248850B - Charging system for electric automobile - Google Patents
Charging system for electric automobile Download PDFInfo
- Publication number
- CN108248850B CN108248850B CN201810102346.0A CN201810102346A CN108248850B CN 108248850 B CN108248850 B CN 108248850B CN 201810102346 A CN201810102346 A CN 201810102346A CN 108248850 B CN108248850 B CN 108248850B
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- China
- Prior art keywords
- vane
- fan
- aircraft
- mounting portion
- guide rail
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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
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- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Wind Motors (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a kind of electric car power supply systems, it include the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail being mounted between the ipsilateral each power transmission rod of road, can be close to the aircraft to fly below transmission guide rail, and be connected between electric car and aircraft to the conducting wire that is transferred to electric energy from transmission guide rail on electric car；The transmission guide rail includes two disposed in parallel, and the aircraft upper end, which 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 flight by aircraft, by trolley pole by electric energy through on wire transmission to electric car, electric car is realized without stopping the function that can be charged, and electric car aircraft in fully charged or other situations can fly away from transmission guide rail at any time, will not cause to limit to being traveled freely for electric car.
Description
Technical field
The invention belongs to electric car corollary system fields, and in particular to a kind of charging system for electric automobile.
Background technique
With popularizing for electric car, the inconvenient problem of electric car charging is also increasingly highlighted；Purchase electric car at present
User be typically limited to only city use on and off duty, need for a long time at a distance outgoing user then still tend to using fuel oil
Vehicle.Even and city short distance traveling, user are also required to pay attention to very much the remaining capacity of electric car, are otherwise easy to appear on the way
The case where no electricity casts anchor.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric car
Say it is not just most suitable, the occupied area of one side electric car is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fill
Electricity may cause traffic congestion, and on the other hand, electric car 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.
Summary of the invention
The technical problems to be solved by the present invention are: in view of the deficienciess of the prior art, to provide a kind of charging convenient, and
The electric car power supply system of user hours underway is not delayed.
Purpose to realize the present invention, 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 being mounted between the ipsilateral each power transmission rod of road, energy
Enough be close to the aircraft to fly below transmission guide rail, and be connected between electric car and aircraft to by electric energy from defeated
Conductance rail is transferred to the conducting wire on electric car；
The transmission guide rail includes two disposed 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.
As a preferred solution: the side in the power transmission rod top towards direction among road be fixedly connected with it is 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 intermediate fovea superior.
As a preferred solution: the electromobile at top is equipped with a wire-winding unit, 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 cover；
Middle position is equipped 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；
There are two the annular electrode a being arranged concentrically, the lower end surface of the wire spool is equipped with for the Wiinding cartridge bottom installation
The annular electrode b electrically connected, the battery Electricity Federation of the annular electrode a and electric car are slided with two annular electrode a
It connects, the conducting wire is electrically connected with annular electrode b；
The Wiinding cartridge side offers the thread passing port passed through for conducting wire.
As a preferred solution: the aircraft includes main part, the main part includes the fan installation of tubular
Portion, the connecting tube of four equidistant arrangements for being connected to fan mounting portion periphery and being connected with fan mounting portion, and be connected to
Each connecting tube outer end and the vane out being connected with corresponding position connecting tube；
It is located above connecting tube in the fan mounting portion and is connected with upper bracket, driving is installed on the upper bracket
Fan；It is located at below connecting tube in the fan mounting portion and is connected with lower bracket, lower driving wind is installed on the lower bracket
Fan；The steering of the upper driving fan and lower driving fan is on the contrary, and install driving fan part in the fan mounting portion
Internal diameter be greater than the internal diameter that lower driving fan part is installed in fan mounting portion, be located at upper driving fan in the fan mounting portion
Wind pressure between lower driving fan is higher than atmospheric pressure, so that forming wind pressure in vane out；
It is described go out vane include sealed connection vane upper housing and vane lower case, in the vane lower case 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 housing inner circumferential lower end；Outlet air gap wide at the top and narrow at the bottom is formed between the interior curved wall and air outlet guard board,
The lower end width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower case is located at outlet air gap is upper width
Under narrow training wall, the cone angle size of tapered surface locating for the training wall is 20-30 degree；
The axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and out between the axial direction and horizontal direction of vane
The angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind of the outlet air gap blowout of vane generates out
Rotation direction is opposite；
The adjusting component for going out vane outlet air speed to adjust corresponding position, the tune are installed in each connecting tube
Saving component includes third motor, the coaxially connected screw rod with third motor output shaft, and the valve plate connecting 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 up and down direction in connecting tube；The company
Adapter tube internal upper part forms the third motor mounting plate to install the third motor, and the third motor mounting plate direction goes out
The side of vane is connected with the valve plate guide rod being slidably connected with the valve plate；Lower part is connected with a upper end court in the connecting tube
The conducting adjustable air passage of area is formed to the inclined baffle in vane direction out, between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively；
The main part is that upper housing and lower case are tightly connected and constitute；The trolley pole lower end is fixedly connected on described
Close to the position for going out vane on shell；
The main part upper end is connected with the air intake cover of a semiellipse spherical shape, uniformly forms strip on air intake cover
Air inlet.
As a preferred solution: the lower, outer perimeter of the fan mounting portion is battery mounting portion, connect on battery mounting portion
It is connected to the battery being electrically connected with control circuit board；The upper end of the aircraft is equipped with camera, the camera and control
Circuit board electrical connection.
As a preferred solution: each vane inner circumferential out forms Holder joint of rising and falling far from the position of connecting tube, it is each
A undercarriage is respectively connected in the Holder joint of rising and falling；The undercarriage includes to be fixedly connected and pass through with Holder joint of rising and falling
Holder joint of rising and falling and the connection pipe body being connected inside vane out, are slidably mounted on the intracorporal sliding tube of connecting tube, with connecting tube
Body is connected on support rod far from Holder joint one end of rising and falling close to the support rod for Holder joint one end rotation connection of rising and falling to inhale
Tightly in the second electromagnet of automobile top, and the connecting rod with rotation connection in the middle part of sliding tube middle part, support rod respectively；
The connection pipe body forms hinged seat, described support rod one end and hinged seat close to the Holder joint one end wall that rises and falls
Rotation connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the sliding pipe outer wall medium position is connected with
Articulated joint, described connecting rod one end and articulated joint are rotatablely connected, side wall molding of the connection pipe body far from Holder joint one end of rising and falling
There is the strip shape gob passed through for articulated joint；The connection pipe body is fixedly connected with sealing cap far from the one end for Holder joint of rising and falling, and seals
The inner end of cap is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against respectively
Between piston and sealing cap inner end；The connecting rod appearance that the connecting rod is accommodated in support rod collapsed state is formed on the support rod
Slot；
The spring is in support rod when extended state and is in unfolded state, and the upper driving fan is in work shape
After state, the air pressure driving piston in vane makes support rod be in collapsed state together with sliding tube movement out.
It include the multiple transmissions of electricity for being fixedly mounted on both sides of the road the present invention also provides a kind of charging system for electric automobile
Bar, the transmission guide rail being mounted between the ipsilateral each power transmission rod of road can be close to the aircraft to fly below transmission guide rail,
And be connected between electric car and aircraft to the conducting wire that is transferred to electric energy from transmission guide rail on electric car；
The transmission guide rail includes two disposed 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 end surface of the transmission guide rail is in intermediate fovea superior
It is arc-shaped；
The electromobile at top is equipped with a wire-winding unit, the wire-winding unit include a upper end opening around
Wire box, the wire spool being rotatably installed in Wiinding cartridge, and it is connected to the box cover of the magnetic material of Wiinding cartridge upper end；
Middle position is equipped 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；
There are two the annular electrode a being arranged concentrically, the lower end surface of the wire spool is equipped with for the Wiinding cartridge bottom installation
The annular electrode b electrically connected, the battery Electricity Federation of the annular electrode a and electric car are slided with two annular electrode a
It connects, the conducting wire is electrically connected with annular electrode b；
The Wiinding cartridge side offers the thread passing port passed through for conducting wire；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan
The connecting tube of mounting portion periphery and four equidistant arrangements being connected with fan mounting portion, and it is connected to each connecting tube outer end
And what is be connected with corresponding position connecting tube goes out vane；
It is located above connecting tube in the fan mounting portion and is connected with upper bracket, driving is installed on the upper bracket
Fan；It is located at below connecting tube in the fan mounting portion and is connected with lower bracket, lower driving wind is installed on the lower bracket
Fan；The steering of the upper driving fan and lower driving fan is on the contrary, and install driving fan part in the fan mounting portion
Internal diameter be greater than the internal diameter that lower driving fan part is installed in fan mounting portion, be located at upper driving fan in the fan mounting portion
Wind pressure between lower driving fan is higher than atmospheric pressure, so that forming wind pressure in vane out；
It is described go out vane include sealed connection vane upper housing and vane lower case, in the vane lower case 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 housing inner circumferential lower end；Outlet air gap wide at the top and narrow at the bottom is formed between the interior curved wall and air outlet guard board,
The lower end width in outlet air gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower case is located at outlet air gap is upper width
Under narrow training wall, the cone angle size of tapered surface locating for the training wall is 20-30 degree；
The axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and out between the axial direction and horizontal direction of vane
The angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind of the outlet air gap blowout of vane generates out
Rotation direction is opposite；
The adjusting component for going out vane outlet air speed to adjust corresponding position, the tune are installed in each connecting tube
Saving component includes third motor, the coaxially connected screw rod with third motor output shaft, and the valve plate connecting 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 up and down direction in connecting tube；The company
Adapter tube internal upper part forms the third motor mounting plate to install the third motor, and the third motor mounting plate direction goes out
The side of vane is connected with the valve plate guide rod being slidably connected with the valve plate；Lower part is connected with a upper end court in the connecting tube
The conducting adjustable air passage of area is formed to the inclined baffle in vane direction out, between the baffle and valve plate；
The upper driving fan, lower driving fan and each third motor are electrically connected with control circuit board respectively；
The main part is that upper housing and lower case are tightly connected and constitute；The trolley pole lower end is fixedly connected on described
Close to the position for going out vane on shell；
The main part upper end is connected with the air intake cover of a semiellipse spherical shape, uniformly forms strip on air intake cover
Air inlet；
The lower, outer perimeter of the fan mounting portion is battery mounting portion, is connected on battery mounting portion and control circuit
The battery of plate electrical connection；The upper end of the aircraft is equipped with camera, and the camera is electrically connected with control circuit board；
Each vane inner circumferential out forms Holder joint of rising and falling, each Holder joint of rising and falling far from the position of connecting tube
On be respectively connected with a undercarriage；The undercarriage include be fixedly connected with Holder joint of rising and falling and by rise and fall Holder joint with go out
The connection pipe body being connected inside vane is slidably mounted on the intracorporal sliding tube of connecting tube, with connection pipe body close to the bridge joint that rises and falls
The support rod of first end rotation connection, is connected on support rod far from Holder joint one end of rising and falling to suck in automobile top
Second electromagnet, and the connecting rod with rotation connection in the middle part of sliding tube middle part, support rod respectively；
The connection pipe body forms hinged seat, described support rod one end and hinged seat close to the Holder joint one end wall that rises and falls
Rotation connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the sliding pipe outer wall medium position is connected with
Articulated joint, described connecting rod one end and articulated joint are rotatablely connected, side wall molding of the connection pipe body far from Holder joint one end of rising and falling
There is the strip shape gob passed through for articulated joint；The connection pipe body is fixedly connected with sealing cap far from the one end for Holder joint of rising and falling, and seals
The inner end of cap is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against respectively
Between piston and sealing cap inner end；The connecting rod appearance that the connecting rod is accommodated in support rod collapsed state is formed on the support rod
Slot；
The spring is in support rod when extended state and is in unfolded state, and the upper driving fan is in work shape
After state, the air pressure driving piston in vane makes support rod be in collapsed state together with sliding tube movement out.
Compared with prior art, the beneficial effects of the present invention are: the present invention is close to transmission guide rail flight by aircraft,
By trolley pole by electric energy through on wire transmission to electric car, realizing electric car without stopping the function that can be charged
Can, and electric car aircraft in fully charged or other situations can fly away from transmission guide rail at any time, and it will not be to electronic vapour
Being traveled freely for vehicle causes to limit.
When aircraft does not work, the aircraft is sucked by the second electromagnet (iron core) in electromobile at top coiling
The upper end of the box cover of component, when aircraft works, the energization of the second electromagnet, which generates the magnetic field reversed with the box cover of magnetic material, to be made
Aircraft and electric car are detached from.
When electric car needs to charge, the control system of electric car sends signal to aircraft, flies to aircraft
Below transmission guide rail, forms trolley pole with transmission guide rail sliding contact and electrically connect；The process of electric car is flown away from aircraft
In, the coiling electric motor rotation that control system controls wire-winding unit simultaneously releases conducting wire from wire spool；Electric car has charged
Bi Hou, aircraft fly back to electromobile at top, while coiling electric motor rotates backward and makes on conducting wire wraparound wire spool.
The aircraft provides driving force, the part that upper driving fan generates by the upper driving fan in fan mounting portion
Air-flow is blown out downwards from the outlet air gap of each vane out, and combination adjusts the wind velocity out of each vane out of component adjustment, from
And realize the horizontal flight or steering of aircraft, each vane out due to being located at aircraft periphery only plays adjustment aircraft
The effect of posture, without the fan for being provided with power, do not easily led to when vane and foreign object generate touching out aircraft it is out of control or
Injury is generated to human or animal, safety 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 uniaxial aircraft.
Further, the air-flow that the outlet air gap of the vane out sprays can be along training wall stream according to Coanda principle
It is dynamic, form the wind film an of taper, and the wind film of taper will drive out the air of vane inner circumferential and flow downward together, fly in this way
When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly
The stabilization of row device flight attitude.
Further, the axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and the axial direction and water of vane out
The angle of 5-20 degree is formed square between, and the horizontal wind-force and upper driving wind that the wind of the outlet air gap blowout of vane generates out
The rotation direction of the fan blade of fan is opposite.Design in this way enables the wind of the outlet air gap blowout of vane out to offset
The reaction force that driving fan or upper driving fan and lower driving fan generate when rotating；Also, passes through while adjusting each tune
Section component change vane out go out wind velocity, it can be achieved that aircraft it is whole forward or reverse.By adjusting one or two
Adjusting component makes one or two go out the wind velocity out of vane, it can be achieved that aircraft generally in heeling condition, can drive in this way
Dynamic aircraft flies in the horizontal direction.
The undercarriage with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, out
It is mobile to sealing cap one end together with sliding tube that wind pressure in vane makes piston, so that sliding tube be made to drive connecting rod one end to sealing cap
Direction is mobile, to make support rod lower end also rotate to sealing cap one end, so that undercarriage be made to be in collapsed state.Work as aircraft
When landing, the wind pressure in vane reduces out, and spring drives sliding tube mobile toward hinged seat direction together with piston, to make sliding tube
It is mobile to hinged seat direction to drive connecting rod one end, so that support rod lower end is made to turn to extreme position to hinged seat one end, thus
Undercarriage is set to be in unfolded state.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention.
Fig. 2 is the portion the C schematic enlarged-scale view of Fig. 1.
Fig. 3 is structural schematic diagram when aircraft rests on electric car.
Fig. 4 is the decomposition texture schematic diagram of wire-winding unit.
Fig. 5 is the structural schematic diagram of aircraft shutdown status.
Fig. 6 is the structural schematic diagram of aircraft flight state.
Fig. 7 is the schematic cross-sectional view of aircraft.
Fig. 8 is the portion the A schematic enlarged-scale view of Fig. 7.
Fig. 9 is the portion the B schematic enlarged-scale view of Fig. 7.
The structural schematic diagram of each component that Figure 10 is upper housing and connect with upper housing.
Figure 11 is the structural schematic diagram of lower housing section.
Figure 12 is the schematic cross-sectional view of lower housing section.
Figure 13 is the decomposition texture schematic diagram of undercarriage part.
Figure 14 is the schematic cross-sectional view of undercarriage part.
1, power transmission rod；11, cross bar；12, insulator；2, transmission guide rail；5, electric car；5a, wire-winding unit；51, coiling
Box；511, thread passing port；52, coiling electric motor；53, wire spool；54, box cover；6, conducting wire；9, aircraft；91, main part；91a, on
Shell；91b, lower case；910, fan mounting portion；9101, upper bracket；9102, lower bracket；9103, battery mounting portion；
9104, circuit board installation cavity；9105, air inlet hole；9106, vent；911, go out vane；9110, it rises and falls Holder joint；9111, wind
Ring upper housing；9112, vane lower case；91121, interior curved wall；91122, dowel；91123, air outlet guard board；91124, water conservancy diversion
Wall；912, connecting tube；9121, third motor mounting plate；9122, valve plate guide rod；9123, baffle；913, the first cover board；92, it stores
Battery；93, undercarriage；931, connection pipe body；9311, hinged seat；9312, strip shape gob；932, sliding tube；9321, piston；
9322, articulated joint；933, sealing cap；9331, spring positioning bar；934, connecting rod；935, support rod；9351, connecting rod tank；936,
Second electromagnet；937, spring；94, air intake cover；941, camera；951, upper driving fan；952, lower driving fan；96, it adjusts
Save component；961, third motor；962, screw rod；963, valve plate；97, control circuit board；98, trolley pole.
Specific embodiment
Embodiment 1
According to Fig. 1 to 5, the present embodiment is a kind of charging system for electric automobile, includes to be fixedly mounted on road two
Multiple power transmission rods 1 of side, the transmission guide rail 2 being mounted between the ipsilateral each power transmission rod of road, can be close under transmission guide rail
The aircraft 9 of Fang Feihang, and be connected between electric car 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 disposed 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 cross
Bar lower end is connected with insulator 12, and the transmission guide rail is connected to insulator lower end；The lower end surface of the transmission guide rail is in centre
Fovea superior it is arc-shaped.
The electromobile at top is equipped with a wire-winding unit 5a, and the wire-winding unit includes a upper end opening
Wiinding cartridge 51, the wire spool 53 being rotatably installed in Wiinding cartridge, and it is connected to the box cover 54 of the magnetic material of Wiinding cartridge upper end.
Middle position is equipped 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.
There are two the annular electrode a being arranged concentrically, the lower end surface of the wire spool is equipped with for the Wiinding cartridge bottom installation
The battery of the annular electrode b, the annular electrode a and electric car that are electrically connected with two annular electrode a slidings or
Charge controller electrically connects, and the conducting wire is electrically connected with annular electrode b.
The Wiinding cartridge side offers the thread passing port 511 passed through for conducting wire.
In addition, the aircraft is also powered by transmission guide rail.
The present invention is close to transmission guide rail flight by aircraft, by trolley pole by electric energy through wire transmission to electric car
On, electric car is realized without stopping the function that can be charged, and electric car is in fully charged or other situations
Lower aircraft can fly away from transmission guide rail at any time, will not cause to limit to being traveled freely for electric car.
When aircraft does not work, the aircraft is sucked by the second electromagnet (iron core) in electromobile at top coiling
The upper end of the box cover of component, when aircraft works, the energization of the second electromagnet, which generates the magnetic field reversed with the box cover of magnetic material, to be made
Aircraft and electric car are detached from.
When electric car needs to charge, the control system of electric car sends signal to aircraft, flies to aircraft
Below transmission guide rail, forms trolley pole with transmission guide rail sliding contact and electrically connect；The process of electric car is flown away from aircraft
In, the coiling electric motor rotation that control system controls wire-winding unit simultaneously releases conducting wire from wire spool；Electric car has charged
Bi Hou, aircraft fly back to electromobile at top, while coiling electric motor rotates backward and makes on conducting wire wraparound wire spool.
Embodiment 2
In conjunction with shown in Fig. 6 to Figure 12, the present embodiment makes following improvement on the basis of embodiment 1: the aircraft packet
Main part 91 is included, the main part includes the fan mounting portion 910 of tubular, is connected to fan mounting portion periphery and and wind
The connecting tube 912 for four equidistant arrangements that fan mounting portion is connected, and it is connected to each connecting tube outer end and and corresponding position
What connecting tube was connected goes out vane 911.
It is located above connecting tube in the fan mounting portion and is connected with upper bracket 9101, is equipped on the upper bracket
Driving fan 951；It is located at below connecting tube in the fan mounting portion and is connected with lower bracket 9102, is installed on the lower bracket
There is lower driving fan 952；The steering of the upper driving fan and lower driving fan in the fan mounting portion on the contrary, and install
The internal diameter of driving fan part is greater than the internal diameter that lower driving fan part is installed in fan mounting portion, position in the fan mounting portion
Wind pressure between upper driving fan and lower driving fan is higher than atmospheric pressure, so that forming wind pressure in vane out.
The vane out includes the vane upper housing 9111 and vane lower case 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 and vane upper housing inner circumferential lower end are tightly connected；Shape between the interior curved wall 91121 and air outlet guard board 91123
At outlet air gap wide at the top and narrow at the bottom, the lower end width in outlet air gap is 0.8-1.5mm；The inner circumferential of the vane lower case 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 tapered surface locating for the training wall is 20-30
Degree.
The axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and out between the axial direction and horizontal direction of vane
The angle of 5-20 degree is formed, and the horizontal wind-force and the fan blade of upper driving fan that the wind of the outlet air gap blowout of vane generates out
Rotation direction is opposite.
The adjusting component 96 for going out vane outlet air speed to adjust corresponding position is installed in each connecting tube, it is described
Adjusting component includes third motor 961, the screw rod 962 coaxially connected with third motor output shaft, and is connected with screw flight
The valve plate 963 connect；For the valve plate upper periphery close to connection inside pipe wall, valve plate lower end is located at the middle part of up and down direction in connecting tube
Position；The connecting tube internal upper part forms the third motor mounting plate to install the third motor, the third motor
The side of mounting plate 9121 towards vane out is connected with the valve plate guide rod 9122 being slidably connected with the valve plate；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 third motor are electrically connected with control circuit board 97 respectively.Institute
Stating main part is that upper housing 91a and lower case 91b is tightly connected composition；The trolley pole lower end is fixedly connected on the upper housing
The upper position close to vane out；.
The main part upper end is connected with the air intake cover 94 of a semiellipse spherical shape, uniformly forms item on air intake cover
The air inlet of shape.
The lower, outer perimeter of the fan mounting portion is battery mounting portion 9103, is connected with and controls on battery mounting portion
The battery 92 of circuit board electrical connection；The upper end of the aircraft is equipped with camera 941, the camera and control circuit board
Electrical connection.
The camera shooting acquisition aircraft, can be by manual operation remote control aircraft with respect to the position of transmission guide rail
It flies, can also be flown automatically along transmission guide rail by aircraft by machine vision technique along transmission guide rail.
The top for being located at battery mounting portion on the fan mounting portion is a circuit board installation cavity 9104, the control
Circuit board is mounted in circuit board installation cavity, and 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 being connected to in fan mounting portion, the circuit board installation
The lateral wall of chamber uniformly forms vent 9106.
Aircraft provides driving force by upper driving fan, the lower driving fan in fan mounting portion, and upper driving fan produces
Raw fraction is blown out downwards from the outlet air gap of each vane out, and combines the outlet air for adjusting each vane out of component adjustment
Speed, to realize the horizontal flight or steering of aircraft, each vane out due to being located at aircraft periphery only plays tune
The effect of whole attitude of flight vehicle does not easily lead to aircraft when vane and foreign object generate touching out without the fan for being provided with power
Out of control or generate injury to human or animal, safety is good.The aircraft appearance is similar to four-axle aircraft, therefore with four-axle aircraft
It is named, four go out vane, that is, so-called " four axis " and only play the function of adjusting posture, therefore this aircraft substantially should be uniaxial
Aircraft.
Further, the air-flow that the outlet air gap of the vane out sprays can be along training wall stream according to Coanda principle
It is dynamic, form the wind film an of taper, and the wind film of taper will drive out the air of vane inner circumferential and flow downward together, fly in this way
When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly
The stabilization of row device flight attitude.
Further, the axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and the axial direction and water of vane out
The angle of 5-20 degree is formed square between, and the horizontal wind-force and upper driving wind that the wind of the outlet air gap blowout of vane generates out
The rotation direction of the fan blade of fan is opposite.Design in this way enables the wind of the outlet air gap blowout of vane out to offset
The reaction force that driving fan and lower driving fan generate when rotating；Also, passes through while adjusting each adjusting component and change out
Vane go out wind velocity, it can be achieved that aircraft it is whole forward or reverse.Adjusting component by adjusting one or two makes one
It is a or two go out vane go out wind velocity, it can be achieved that aircraft generally in heeling condition, can be driven in water in aircraft in this way
Square to flight.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, plays to control circuit board scattered
Heat effect.
Each vane inner circumferential out forms Holder joint 9110 of rising and falling, each undercarriage far from the position of connecting tube
A undercarriage 93 is respectively connected on connector；The undercarriage is equipped with to suck the second electromagnet in electromobile at top
936。
When aircraft does not work, aircraft is sucked by the second electromagnet of undercarriage lower end in electromobile at top
On box cover.
Embodiment 3
In conjunction with Figure 13 to Figure 14, the present embodiment also makes following improvement on the basis of embodiment 2: each vane out
Inner circumferential forms Holder joint 9110 of rising and falling far from the position of connecting tube, is respectively connected with one in each Holder joint of rising and falling and rises and falls
Frame 93；The undercarriage includes to be fixedly connected with Holder joint of rising and falling and by being connected inside rise and fall Holder joint and vane out
Connection pipe body 931 is slidably mounted on the intracorporal sliding tube 932 of connecting tube, with connection pipe body close to Holder joint one end rotation of rising and falling
The support rod 935 of connection, be connected on support rod far from Holder joint one end of rising and falling to suck the in electromobile at top
Two electromagnet 936, and the connecting rod 934 with rotation connection in the middle part of sliding tube middle part, support rod respectively.
The connection pipe body forms hinged seat 9311, described support rod one end and hinge close to the Holder joint one end wall that rises and falls
Joint chair rotation connection；The sliding tube is connected with piston 9321, position in the middle part of the sliding pipe outer wall close to Holder joint one end of rising and falling
It sets and is connected with articulated joint 9322, described connecting rod one end and articulated joint are rotatablely connected, and the connection pipe body is far from Holder joint one of rising and falling
The side wall at end forms the strip shape gob 9312 passed through for articulated joint；The one end of 912 body of connecting tube far from Holder joint of rising and falling is solid
Surely it is connected with sealing cap 933, the inner end of sealing cap is connected with spring positioning bar 9331, is arranged on the spring positioning bar
Spring 937, the both ends of the spring are against respectively between piston and sealing cap inner end；It forms on the support rod and is received in support rod
The connecting rod tank 9351 of the connecting rod is accommodated when the state of rising.
The spring is in support rod when extended state and is in unfolded state, and the upper driving fan is in work shape
After state, the air pressure driving piston in vane makes support rod be in collapsed state together with sliding tube movement out.
The undercarriage with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, out
It is mobile to sealing cap one end together with sliding tube that wind pressure in vane makes piston, so that sliding tube be made to drive connecting rod one end to sealing cap
Direction is mobile, to make support rod lower end also rotate to sealing cap one end, so that undercarriage be made to be in collapsed state.Work as aircraft
When landing, the wind pressure in vane reduces out, and spring drives sliding tube mobile toward hinged seat direction together with piston, to make sliding tube
It is mobile to hinged seat direction to drive connecting rod one end, so that support rod lower end is made to turn to extreme position to hinged seat one end, thus
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 stretches spring
After length, support rod turn to it is vertical with horizontal direction after continue to rotate 3-10 degree so that aircraft landing after, each support rod is equal
In stable state.
Claims (1)
1. a kind of charging system for electric automobile, it is characterised in that: it include the multiple power transmission rods for being fixedly mounted on both sides of the road, peace
Transmission guide rail between each power transmission rod ipsilateral mounted in road can be close to the aircraft to fly below transmission guide rail, and
Be connected between electric car and aircraft to the conducting wire that is transferred to electric energy from transmission guide rail on electric car；
The transmission guide rail includes two disposed in parallel, and the aircraft upper end is connected with sliding 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
It is connected with insulator, the transmission guide rail is connected to insulator lower end；The lower end surface of the transmission guide rail is in the circle of intermediate fovea superior
Arc；
The electromobile at top is equipped 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 cover of the magnetic material of Wiinding cartridge upper end；
Middle position is equipped 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；
There are two the annular electrode a being arranged concentrically, the lower end surface of the wire spool is equipped with and two for the Wiinding cartridge bottom installation
The battery of annular electrode b, the annular electrode a and electric car that a annular electrode a sliding electrically connects electrically connect, institute
Conducting wire is stated to electrically connect with annular electrode b；
The Wiinding cartridge side offers the thread passing port passed through for conducting wire；
The aircraft includes main part, and the main part includes the fan mounting portion of tubular, is connected to fan installation
The connecting tube of portion periphery and four equidistant arrangements being connected with fan mounting portion, and be connected to each connecting tube outer end and with
What corresponding position connecting tube was connected goes out vane；
It is located above connecting tube in the fan mounting portion and is connected with upper bracket, driving wind is installed on the upper bracket
Fan；It is located at below connecting tube in the fan mounting portion and is connected with lower bracket, lower driving fan is installed on the lower bracket；
The upper driving fan is turned to lower driving fan on the contrary, and installing the interior of driving fan part in the fan mounting portion
Diameter is greater than the interior internal diameter for installing lower driving fan part of fan mounting portion, is located at upper driving fan under in the fan mounting portion
Wind pressure between driving fan is higher than atmospheric pressure, so that forming wind pressure in vane out；
It is described go out vane include sealed connection vane upper housing and vane lower case, the vane lower case inner circumferential upper end at
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 housing inner circumferential lower end is tightly connected；Outlet air gap wide at the top and narrow at the bottom, outlet air are formed between the interior curved wall and air outlet guard board
The lower end width in gap is 0.8-1.5mm；The lower section that the inner circumferential of the vane lower case is located at outlet air gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of tapered surface locating for the training wall is 20-30 degree；
The axial direction of vane out and the radial direction of fan mounting portion are perpendicular, and are formed between the axial direction and horizontal direction of vane out
The angle of 5-20 degree, and the rotation of the fan blade of the wind horizontal wind-force generated and upper driving fan of the outlet air gap blowout of vane out
It is contrary；
The adjusting component for going out vane outlet air speed to adjust corresponding position, the adjusting group are installed in each connecting tube
Part includes motor, the coaxially connected screw rod with motor output shaft, and the valve plate connecting with screw flight；The valve plate top
Close to connection inside pipe wall, valve plate lower end is located at the medium position of up and down direction in connecting tube for periphery；The connecting tube internal upper part at
Type has the motor mounting plate to install the motor, and the motor mounting plate is connected with and the valve towards the side for going out vane
The valve plate guide rod that plate is slidably connected；Lower part is connected with a upper end direction inclined baffle in vane direction out in the connecting tube,
The conducting adjustable air passage of area is formed between the baffle and valve plate；
The upper driving fan, lower driving fan and each motor are electrically connected with control circuit board respectively；
The main part is that upper housing and lower case are tightly connected and constitute；The trolley pole lower end is fixedly connected on the upper housing
The upper position close to vane out；
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；
The lower, outer perimeter of the fan mounting portion is battery mounting portion, is connected on battery mounting portion and control circuit board electricity
The battery of connection；The upper end of the aircraft is equipped with camera, and the camera is electrically connected with control circuit board；
It is each it is described go out vane inner circumferential far from the position of connecting tube form Holder joint of rising and falling, it is each in each Holder joint of rising and falling
It is connected with a undercarriage；The undercarriage includes to be fixedly connected with Holder joint of rising and falling and by Holder joint and the vane out of rising and falling
The connection pipe body that inside is connected is slidably mounted on the intracorporal sliding tube of connecting tube, with connection pipe body close to Holder joint one of rising and falling
The support rod for holding rotation connection is connected on support rod far from Holder joint one end of rising and falling to suck the electromagnetism in automobile top
Iron, and the connecting rod with rotation connection in the middle part of sliding tube middle part, support rod respectively；
The connection pipe body forms hinged seat close to the Holder joint one end wall that rises and falls, and described support rod one end and hinged seat rotate
Connection；The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the sliding pipe outer wall medium position is connected with hingedly
Head, described connecting rod one end and articulated joint are rotatablely connected, and the connection pipe body forms confession far from the side wall of Holder joint one end of rising and falling
The strip shape gob that articulated joint passes through；The connection pipe body is fixedly connected with sealing cap far from the one end for Holder joint of rising and falling, sealing cap
Inner end is connected with spring positioning bar, and spring is arranged on the spring positioning bar, and the both ends of the spring is against piston respectively
Between sealing cap inner end；The connecting rod tank that the connecting rod is accommodated in support rod collapsed state is formed on the support rod；
The spring is in support rod when extended state and is in unfolded state, and the upper driving fan is in running order
Afterwards, the air pressure driving piston out in vane makes support rod be in collapsed state together with sliding tube movement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810102346.0A CN108248850B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Applications Claiming Priority (2)
| 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 |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710489021.8A Division CN107117301B (en) | 2017-06-23 | 2017-06-23 | Charging system for electric automobile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108248850A CN108248850A (en) | 2018-07-06 |
| CN108248850B true CN108248850B (en) | 2019-11-08 |
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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 |
| CN201810102346.0A Active CN108248850B (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 |
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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 |
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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 |
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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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Also Published As
| Publication number | Publication date |
|---|---|
| CN107117301A (en) | 2017-09-01 |
| CN107117301B (en) | 2018-05-04 |
| CN108216609A (en) | 2018-06-29 |
| CN108248850A (en) | 2018-07-06 |
| CN108216609B (en) | 2021-06-29 |
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Effective date of registration: 20220713 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. |