CN107487218B - A kind of electric automobile charging pile - Google Patents
A kind of electric automobile charging pile Download PDFInfo
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- CN107487218B CN107487218B CN201710663810.9A CN201710663810A CN107487218B CN 107487218 B CN107487218 B CN 107487218B CN 201710663810 A CN201710663810 A CN 201710663810A CN 107487218 B CN107487218 B CN 107487218B
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- battery unit
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- 239000000725 suspension Substances 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 11
- 230000008569 process Effects 0.000 claims description 11
- 238000000465 moulding Methods 0.000 claims description 7
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- 230000009471 action Effects 0.000 claims description 3
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- 239000004020 conductor Substances 0.000 claims description 3
- 238000011068 loading method Methods 0.000 abstract description 2
- 230000000630 rising effect Effects 0.000 description 11
- 238000010586 diagram Methods 0.000 description 9
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- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052744 lithium Inorganic materials 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/31—Charging columns specially adapted for electric vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
- B60S5/00—Servicing, maintaining, repairing, or refitting of vehicles
- B60S5/06—Supplying batteries to, or removing batteries from, vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
The invention discloses a kind of electric automobile charging piles, include the housing of rectangular shape, side and the multiple cell support framves being placed equidistant with along longitudinal direction in housing, it is placed on the battery unit to charge on each cell support frame, battery disassembly and assembly seat mounted on case top and above cell support frame and the conveying mechanism for the conveying battery unit between each cell support frame and battery disassembly and assembly seat in housing；By loading multiple battery units in charging pile housing, and battery unit can on battery disassembly and assembly seat assembled integrated battery module, institute's electricity demand can substantially be estimated according to the distance of different electric vehicle institutes predicted travel to determine required battery unit number in this way, then providing one or more battery unit transportation to electric vehicle position to electricity for electric vehicle by aircraft feeds.
Description
Technical field
The invention belongs to electric vehicle corollary equipment fields, and in particular to a kind of electric automobile charging pile.
Background technology
Universal with electric vehicle, the problem of electric vehicle charging is inconvenient, also increasingly highlights；Purchase electric vehicle at present
User be typically limited to only city use on and off duty, need for a long time at a distance outgoing user then still tend to use fuel oil
Vehicle.And even city short distance traveling, user are also required to pay attention to very much the remaining capacity of electric vehicle, are otherwise susceptible on the way
Situation about casting anchor without electricity.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric vehicle
Speech is not just most suitable, and the floor space of one side electric vehicle is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills
Electricity may cause traffic congestion, and on the other hand, electric vehicle power consumption also many bigger than the battery truck of two-wheeled charges in current battery
In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
Invention content
The technical problems to be solved by the invention are：In view of the deficienciess of the prior art, provide a kind of structure novel, energy
Enough electric vehicles in traveling provide the electric automobile charging pile of electricity supply.
Purpose to realize the present invention, is achieved using following technical scheme：A kind of electric automobile charging pile, includes
The housing of rectangular shape, side and the multiple cell support framves being placed equidistant with along longitudinal direction, are placed on each in housing
The battery unit to charge on cell support frame, the battery disassembly and assembly mounted on case top and above cell support frame
Seat and the conveyer for the conveying battery unit between each cell support frame and battery disassembly and assembly seat in housing
Structure；
The upper part of the housing is stepped, and the case top is located at cell support frame upper section for the first top plate, institute
It is the second top plate, and the position of the second top plate is higher than the first top plate that case top, which is stated, different from the part of the first top plate；The housing
There are one the side openings for battery unit disengaging for tool between the first top plate and the second top plate；
The conveying mechanism includes longitudinal translating device associated and horizontal transport agency；The longitudinal translating device associated includes perpendicular
It is straight to be mounted in housing different from the leading screw and lifting guide pillar of cell support frame side, it is connect with leading screw by screw-driven, with rising
The lifting seat and be fixedly mounted on housing bottom and the lifting motor being connect with lead screw transmission that drop guide rod is slidably connected；
The horizontal transport agency includes there are one the battery Mobile base of square and is connected to battery Mobile base with rising
Horizontally disposed horizontal push between seat drops；It is fixedly connected on the lifting seat towards the side of battery Mobile base there are two water
The horizontal guide of setting is equalled, the sliding seat being slidably connected with two with horizontal guide is connected on the battery Mobile base；It is described
4 electromagnet that battery unit is sucked by magnetic force are installed close to four vertex positions on Mobile base；
The battery unit is integrally square, and close four vertex positions form wide at the top and narrow at the bottom on the battery unit
Step through-hole, the fastening screw of the magnetic conductive material being packed into from top to bottom is slidably fitted in each step through-hole,
The spacing collar for being plugged with to stop that fastening screw is detached from step through-hole is fixed on the step through-hole top；The positioning is inserted
There are one outer flange collars for the medium position periphery molding of pin length direction, are equipped between the outer flange collar upper end and spacing collar lower end
To the spring a for pushing down on fastening screw；The electromagnet is sucked by magnetic field force and fastening screw thus by battery unit
Lift；
There are one splicing convex block, the periphery for splicing convex block is equidistantly molded battery unit upper end centre position integrally connected
There are multiple bayonet parts that are screwed on, there are two the upper output electrodes of the annular of concentric setting for splicing convex block upper end installation；It is described
The molding of battery unit lower end centre position to form and the bayonet part that is screwed on there are one recess, the splicing recess inner circumferential is spliced
The convex block that is screwed on being connected, the lower output electrode for splicing annular of the bottom installation there are two concentric setting in recess；
Connected between neighbouring two battery units by the bayonet part that is screwed on the convex block that is screwed on, and when be screwed on bayonet part and
When the convex block that is screwed on is connected in place, the fastening screw for the battery unit being located above is inserted into the step of underlying battery unit
Through-hole top；It is connected in parallel between neighbouring two battery units by the realization that offsets of upper output electrode and lower output electrode；
Each lateral wall of the battery unit is equipped with charging electrode；The inner walls are located at each cell support frame
Top position is equipped with the cradle for charging for battery unit, the charging output electrode on cradle just with battery unit
On charging electrode offset and electrically connect；
The battery disassembly and assembly seat include the guide sleeve that is fixedly connected on the first top plate lower end and across the first top plate with
The battery tray of guide sleeve sliding connection；
The positioning projection seat that there are one battery tray upper end integrally connecteds with the splicing recess grafting of battery unit lower end,
The periphery of the positioning projection seat forms the rotation stop male part for being plugged on position between the two neighboring convex block that is screwed in splicing recess,
The sliding bar that the guide sleeve is slidably connected is connected among the battery tray lower end, the sliding bar outer wall forms
More than two guide heads being distributed with circumference array；
The guide sleeve inner wall forms the guide groove of quantity identical with guide head, and the guide head is slidably connected to described
In guide groove；The guide groove includes helical groove portion and is connected to the longitudinal slot portion of helical groove portion lower end；
Be arranged with spring outside the sliding bar, the both ends of the spring be located in battery tray lower end and the first top plate upper end it
Between；The sliding bar lower end is fixedly connected with damping piston, and being equipped with below damping piston in the housing can be with resistance
The damping piston cylinder that Buddhist nun's piston is connected；The damping piston cylinder is in the groove body of upper end opening, the damping piston cylinder lower end
Connection is there are one the check valve by damping piston cylinder Inside To Outside one-way conduction, and the damping piston cylinder lower end is different from unidirectional
The position of valve offers air admission hole, and the internal diameter of air admission hole is 1-2mm；
The lifting motor, horizontal push, each electromagnet and each cradle respectively in housing
Controller electrically connect；
When having more than one battery unit on battery disassembly and assembly seat, and needing to load another battery unit, lifting
Motor work makes lifting seat be moved to a fully charged battery unit top position in housing together with battery Mobile base, then water
Flat-pushing bar elongation makes battery Mobile base be moved to the surface of battery unit, and then electromagnet energization, which is sucked on battery unit, determines
Position bolt battery unit lifts；
Then horizontal push, which is retracted, makes battery unit be detached from cell support frame region, and then lifting motor work drives battery
Unit is moved upward to above the battery unit loaded on battery disassembly and assembly seat, and then horizontal push elongation makes battery to be loaded
Unit is moved to right over the battery unit loaded；
Then lifting motor driving battery Mobile base and the battery unit of below to be loaded move down and oppress electricity
Pond pallet to guide head reaches the lower end position of guide sleeve inside spin groove portion, and in the process, the battery unit loaded connects
It is moved down with battery tray while generates rotation, the convex block that is screwed on of battery unit lower end finally to be loaded is caught in what is loaded
Position between the two neighboring bayonet part that is screwed on of battery unit upper end；
The battery unit for driving battery Mobile base and below to be loaded followed by lifting motor moves up, battery tray
Disk and the battery unit loaded are moved up and are turned round under the restoring force effect of spring, so as to make battery unit to be loaded
The convex block that is screwed on be caught in and loaded being screwed among bayonet part of corresponding position on battery unit；Then the electromagnetism on battery Mobile base
Iron power-off makes fastening screw disengage and be inserted into the step through-hole for the battery unit being disposed below with electromagnet；
When being disassembled on battery disassembly and assembly seat there are two above battery unit, lifting motor work drives battery
Mobile base is moved to the top position of battery unit to be dismantled on battery disassembly and assembly seat；Then horizontal push elongation moves battery
Seat is moved to right over battery unit to be dismantled, and the battery unit positioned at the top is sucked in then electromagnet energization, makes simultaneously
The step through-hole of fastening screw and battery unit adjacent below for obtaining the battery unit positioned at the top is detached from；
Then lifting motor driving battery Mobile base moves down compressing battery unit and battery tray to guide head reaches
The lower position of longitudinal slot portion in guide sleeve；In the process, other batteries other than the battery unit for being located at the top
Unit generates rotation with battery tray；When guide head reaches the lower end position of guide sleeve inside spin groove portion, positioned at the top
Battery unit lower end be screwed on convex block and the bayonet part disengagement that is screwed on of adjacent battery unit upper end below；It is reached in guide head
In to guide sleeve during the lower position of longitudinal slot portion, damping piston is slipped into the damping piston cylinder, the sky in damping piston cylinder
Gas is discharged from check valve and air admission hole；
Battery Mobile base and battery unit positioned at the top is driven to move up followed by lifting motor, battery tray with
And the battery unit do not disassembled is slowly mobile upwards under the restoring force of spring and the force action of damping piston and turns round, herein
It is separated from the process positioned at the battery unit of the top and adjacent battery unit below；
Final level push rod retracts the top that the battery unit under having disassembled is made to be detached from battery disassembly and assembly seat, then lifting motor
Battery unit under driving battery Mobile base and having disassembled is moved to above unloaded cell support rack position, then horizontal push
Elongation makes the battery unit under disassembling be moved to right over cell support frame, and then electromagnet power-off makes the battery unit under disassembling
It is detached from battery Mobile base.
Preferably：It has further included to convey more than one battery between battery disassembly and assembly seat and electric vehicle
The aircraft of unit；There are one the suspension assemblies to lift battery unit for the aircraft lower end connection；
It is fixedly mounted above second top plate there are one the lifting push rod of output rod vertically upward, the lifting push rod
Output rod upper end is fixedly connected with that there are one the whole rounded shutdown platforms stopped for the aircraft；The shutdown platform
Disengaging recess is formed close to the side of the first top plate, described shut down is connected with close to the position of periphery with for winged above platform
The arc-shaped positioning magnet ring of row device positioning；The lifting push rod is electrically connected with controller；
The suspension assembly includes the connecting rod being fixedly connected with aircraft lower end, is fixedly connected on connecting rod lower end
Kuppe is fixedly connected on the inserted link of kuppe lower end, and the lifting rod being slidably connected in inserted link is fixedly connected under lifting rod
The expansion-head at end and it is fixedly mounted on the motor that in kuppe and output shaft is threadedly coupled with lifting rod top；
The control circuit board of the motor and aircraft electrically connects；
The expansion-head includes there are one circular main part and is integrally attached to multiple valve bodies of main part periphery
Portion, in the high taper surface in intermediate low periphery, each valve body upper end offsets with taper surface for the lower end of the inserted link；It is described
The valve body portion is slided along taper surface oblique upper when lifting rod moves up, and valve body portion is made finally to be clamped on stepped hole inner wall position
In the lower section of step part；When each valve body upper end is detached from taper surface, the circumference residing for each valve body upper end outer wall is straight
Diameter is less than the internal diameter on stepped hole top.
Preferably：It is equipped with to detect between the output rod upper end shut down platform lower end and lift push rod
The pressure sensor that aircraft whether is stopped on platform is shut down, the pressure sensor is electrically connected with controller；
Centre position installation is there are one by compressing switch above the positioning projection seat, described by compressing switch and controller Electricity Federation
It connects；
When the battery unit quantity on the battery disassembly and assembly seat reaches pre-provisioning request, and pressure sensor detects that shutdown is flat
When stop has aircraft on platform, lifting push rod shortening makes the inserted link of suspension assembly and expansion-head be inserted into the stepped hole of battery unit
Interior, when expansion-head lower end is pressed by compressing switch, lifting push rod stops；
Then the control circuit board control motor rotation of aircraft makes expansion-head expansion be clamped on bottom battery unit
In stepped hole；
The control circuit board of the aircraft is communicated to connect with controller.
Preferably：The angle of 1-10 degree, and the battery are formed between the cell support frame and horizontal direction
Supporting rack is tilted towards the cradle side；The cell support frame includes the branch being symmetrically mounted in two opposed inner walls of housing
Fagging is also symmetrically rotatablely equipped with multigroup support wheel that connection is rolled with battery unit lower end in two support plates, makes
The charging output electrode obtained on charging electrode and cradle on battery unit closely offsets.
Compared with prior art, the beneficial effects of the invention are as follows：By loading multiple battery lists in charging pile housing
Member, and battery unit can on battery disassembly and assembly seat assembled integrated battery module, in this way can be according to different electric vehicle institutes
The distance of predicted travel substantially estimates institute's electricity demand to determine required battery unit number, then by aircraft by one
Or multiple battery units are transported to electric vehicle position and provide electricity supply for electric vehicle.Such mode is compared to appearance
For measuring fixed battery module, the utilization rate of battery unit can be significantly improved；Especially in electric vehicle predicted travel distance
When shorter, aircraft only needs to carry small number of battery unit, reduces the aircraft during conveying battery unit
Energy consumption.
Further, the battery disassembly and assembly seat cooperation conveying mechanism（Predominantly lifting motor and electromagnet）Electricity can be realized
The assembling and fractionation of pool unit, execution unit is few, reduces the holistic cost of charging pile.Specifically, the guide head of battery tray
Coordinate with the guide groove in guide sleeve so that can produce relative rotation and realize between two battery units of the top
Be screwed on convex block and being screwed on of bayonet part of being screwed between upper and lower two battery units, without extra execution unit.Furthermore it is tearing open
When dividing battery module, by devising the damper being made of damping piston and damping piston cylinder in battery tray lower end so that
Battery unit positioned at the top can be adjacent with lower section when being raised battery unit mutually disengage, smart structural design.
In addition, on the one hand the fastening screw on the battery unit coordinates lifting for high-speed double electromagnet battery unit, it is another
Aspect fastening screw after two battery units are connected by the convex block that is screwed on the bayonet part that is screwed on play prevent from being screwed on convex block and
The effect that the bayonet part that is screwed on is detached from stablizes splicing so as to fulfill between multiple battery units.
Furthermore on the one hand the lifting push rod plays the function that platform is shut down in support, on the other hand lift spelling in aircraft
During the battery module installed, lifting push rod shortening makes the inserted link of suspension assembly and expansion-head part be inserted into bottom battery
In the stepped hole of unit.
Description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is configuration state figure when aircraft lifts two battery units.
Fig. 3, Fig. 4 are the internal structure schematic diagrams of the present invention.
Fig. 5 is the decomposition texture schematic diagram of battery disassembly and assembly seating portion.
Fig. 6 is the schematic cross-sectional view of guide sleeve part.
Fig. 7 is the structure diagram of battery unit.
Fig. 8 is the mounting structure schematic diagram of battery unit fastening screw.
Fig. 9 is the structure diagram of suspension assembly.
Figure 10 is the schematic cross-sectional view of suspension assembly.
Figure 11 is the structure diagram of aircraft resting state.
Figure 12 is the structure diagram of state of flight of the present invention.
Figure 13 is the schematic cross-sectional view of aircraft.
Figure 14 is the A portions schematic enlarged-scale view of Figure 13.
Figure 15 is the schematic cross-sectional view of undercarriage part.
Figure 16 is the decomposition texture schematic diagram of undercarriage part.
, housing；101st, the first top plate；102nd, the second top plate；11st, lifting seat；111st, horizontal guide；12nd, lifting motor；
121st, leading screw；122nd, lifting guide pillar；13rd, cell support frame；131st, support wheel；15th, cradle；
2nd, battery unit；21st, charging electrode；22nd, fastening screw；23rd, splice recess；231st, be screwed on convex block；25th, lower output
Electrode；26th, stepped hole；27th, splice convex block；271st, be screwed on bayonet part；28th, upper output electrode；29th, spacing collar；
3rd, platform is shut down；31st, push rod is lifted；32nd, magnet ring is positioned；33rd, recess is passed in and out；
5th, battery disassembly and assembly seat；51st, battery tray；511st, projection seat is positioned；512nd, rotation stop male part；513rd, sliding bar；515、
Guide head；516th, by compressing switch；
52nd, spring；53rd, guide sleeve；531st, guide groove；55th, damping piston；56th, damping piston cylinder；561st, piston cylinder is fixed
Plate；562nd, check valve；563rd, air admission hole；
6th, battery Mobile base；61st, sliding seat；62nd, electromagnet；63rd, horizontal push；
9th, aircraft；90th, main part；900th, fan mounting portion；901st, discharge pipe；902nd, upper bracket；903rd, lower carriage；
904th, circuit board installation cavity；905th, air inlet hole；906th, vent；
91st, go out vane；910th, socket pipe；911st, nut set；912nd, outlet air gap；913rd, training wall；914th, interior curved wall；
915th, it rises and falls Holder joint；
92nd, accumulator；
93rd, undercarriage；931st, outlet air tube 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、
Idler wheel；937th, spring；
94th, air intake cover；
951st, upper driving fan；952nd, lower driving fan；
96th, motor；961st, screw rod；
97th, suspension assembly；971st, connecting rod；972nd, kuppe；973rd, inserted link；975th, expansion-head；976th, lifting rod；977、
Motor.
Specific embodiment
Embodiment 1
According to Fig. 1 to Figure 10, the present embodiment is a kind of electric automobile charging pile, includes the housing of rectangular shape
1, side and the multiple cell support framves 13 being placed equidistant with along longitudinal direction, it is enterprising to be placed on each cell support frame in housing
The battery unit 2 of row charging, battery disassembly and assembly seat 5 mounted on case top and above the cell support frame and is mounted on
The conveying mechanism for the conveying battery unit between each cell support frame and battery disassembly and assembly seat in housing.
The upper part of the housing is stepped, and the case top is located at cell support frame upper section for the first top plate 101,
The case top is the second top plate 102 different from the part of the first top plate, and the position of the second top plate is higher than the first top plate；It is described
Housing have between the first top plate and the second top plate there are one for battery unit disengaging side opening.
The conveying mechanism includes longitudinal translating device associated and horizontal transport agency；The longitudinal translating device associated includes perpendicular
It is directly mounted in housing different from the leading screw 121 of cell support frame side and lifting guide pillar 122, is connected with leading screw by screw-driven
The lifting seat 11 that connect, is slidably connected with lifting guide pillar and it is fixedly mounted on housing bottom and the lifting being connect with lead screw transmission
Motor 12.Leading screw is driven to rotate so as to drive moving up and down for lifting seat by the rotating of lifting motor.
The horizontal transport agency include there are one square battery Mobile base 6 and be connected to battery Mobile base with
Horizontally disposed horizontal push 63 between lifting seat；On the lifting seat two are fixedly connected with towards the side of battery Mobile base
A horizontally disposed horizontal guide 111 is connected with the slip being slidably connected with two with horizontal guide on the battery Mobile base
Seat 61；4 electromagnet 62 that battery unit is sucked by magnetic force are installed close to four vertex positions on the Mobile base.
The battery unit is integrally square, and close four vertex positions form wide at the top and narrow at the bottom on the battery unit
Step through-hole, the fastening screw of the magnetic conductive material being packed into from top to bottom is slidably fitted in each step through-hole
22, the spacing collar 29 for being plugged with to stop that fastening screw is detached from step through-hole is fixed on the step through-hole top；It is described
Outer flange collar that there are one the medium position periphery moldings of fastening screw length direction, between the outer flange collar upper end and spacing collar lower end
Spring a fastening screw to be pushed down on is installed；The electromagnet is sucked with fastening screw thus will be electric by magnetic field force
Pool unit lifts.The elastic force of the spring a is without very big, it is only necessary to ensure fastening screw in the case where not acted on by other external force just
Extreme position can be moved down into and be maintained at stable state, it is ensured that electromagnet fastening screw can be picked up upwards and
Resistance is smaller.
Battery unit upper end centre position integrally connected there are one splicing convex block 27, splice the periphery of convex block equidistantly into
Type has multiple bayonet parts 271 that are screwed on, and there are two the upper output electrodes of the annular of concentric setting for splicing convex block upper end installation
28；The battery unit lower end centre position molding there are one splicing recess 23, it is described splicing recess inner circumferential form with it is described
The convex block 231 that is screwed on that the bayonet part that is screwed on is connected, the annular for splicing concentric setting there are two the installations of bottom in recess
Lower output electrode 25.
Connected between neighbouring two battery units by the bayonet part that is screwed on the convex block that is screwed on, and when be screwed on bayonet part and
When the convex block that is screwed on is connected in place, the fastening screw for the battery unit being located above is inserted into the step of underlying battery unit
Through-hole top；It is connected in parallel between neighbouring two battery units by the realization that offsets of upper output electrode and lower output electrode.
Each lateral wall of the battery unit is equipped with charging electrode 21；The inner walls are located at each cell support
Frame top position is equipped with the cradle 15 for charging for battery unit, the charging output electrode on cradle just with battery
Charging electrode on unit, which offsets, to be electrically connected.The electricity for being equipped with to monitor battery unit electricity on each cradle is supervised
Survey module.
The charging electrode of each side of battery unit is form in parallel, i.e. every side of battery unit all can be with cradle
Connection is charged.Upper output electrode and lower output electrode are also the form being connected in parallel, the multiple lithium electricity of installation in battery unit
Pond, connection boosting, regulator circuit after multiple lithium battery connection in series-parallel, boosting, circuit output end of pressure-stabilizing and the upper output electrode, under
Output electrode connects, and the output voltage of cell voltages multiple in this way can be consistent, convenient for multiple used in parallel.It boosts, is steady
Volt circuit is existing conventional techniques, is not unfolded to describe herein.
The battery disassembly and assembly seat includes the guide sleeve 53 that is fixedly connected on the first top plate lower end and across the first top plate
With the battery tray 51 of guide sleeve sliding connection.
There are one the positioning projection seats of the splicing recess grafting with battery unit lower end for battery tray upper end integrally connected
511, the periphery of the positioning projection seat, which forms, to be plugged in splicing recess between the two neighboring convex block that is screwed on outside the rotation stop of position
Protrusion 512 is connected with the sliding bar 513 that the guide sleeve is slidably connected, the slip among the battery tray lower end
Bar outer wall forms more than two guide heads 515 being distributed with circumference array.
The guide sleeve inner wall forms the guide groove 531 of quantity identical with guide head, and the guide head is slidably connected to
In the guide groove；The guide groove includes helical groove portion and is connected to the longitudinal slot portion of helical groove portion lower end.Helicla flute
Portion causes battery tray to be oppositely oriented during set moves down while generates rotation.
Be arranged with spring outside the sliding bar, the both ends of the spring be located in battery tray lower end and the first top plate upper end it
Between；The sliding bar lower end is fixedly connected with damping piston 55, is located at below damping piston that be equipped with can be in the housing
The damping piston cylinder 56 that damping piston is connected；The damping piston cylinder is in the groove body of upper end opening, the damping piston cylinder
There are one the check valve 562 by damping piston cylinder Inside To Outside one-way conduction, and the damping piston cylinder lower ends for lower end connection
Air admission hole 563 is offered different from the position of check valve, the internal diameter of air admission hole is 1-2mm.The damping piston cylinder passes through piston cylinder
Fixed plate 561 is fixed on inner walls.
The lifting motor, horizontal push, each electromagnet and each cradle respectively in housing
Controller electrically connect.
When having more than one battery unit on battery disassembly and assembly seat, and needing to load another battery unit, lifting
Motor work makes lifting seat be moved to a fully charged battery unit top position in housing together with battery Mobile base, then water
Flat-pushing bar elongation makes battery Mobile base be moved to the surface of battery unit, and then electromagnet energization, which is sucked on battery unit, determines
Position bolt battery unit lifts.
Then horizontal push, which is retracted, makes battery unit be detached from cell support frame region, and then lifting motor work drives battery
Unit is moved upward to above the battery unit loaded on battery disassembly and assembly seat, and then horizontal push elongation makes battery to be loaded
Unit is moved to right over the battery unit loaded.
Then lifting motor driving battery Mobile base and the battery unit of below to be loaded move down and oppress electricity
Pond pallet to guide head reaches the lower end position of guide sleeve inside spin groove portion, and in the process, the battery unit loaded connects
It is moved down with battery tray while generates rotation, the convex block that is screwed on of battery unit lower end finally to be loaded is caught in what is loaded
Position between the two neighboring bayonet part that is screwed on of battery unit upper end.
The battery unit for driving battery Mobile base and below to be loaded followed by lifting motor moves up, battery tray
Disk and the battery unit loaded are moved up and are turned round under the restoring force effect of spring, so as to make battery unit to be loaded
The convex block that is screwed on be caught in and loaded being screwed among bayonet part of corresponding position on battery unit；Then the electromagnetism on battery Mobile base
Iron power-off makes fastening screw disengage and be inserted into the step through-hole for the battery unit being disposed below with electromagnet.
When being disassembled on battery disassembly and assembly seat there are two above battery unit, lifting motor work drives battery
Mobile base is moved to the top position of battery unit to be dismantled on battery disassembly and assembly seat；Then horizontal push elongation moves battery
Seat is moved to right over battery unit to be dismantled, and the battery unit positioned at the top is sucked in then electromagnet energization, makes simultaneously
The step through-hole of fastening screw and battery unit adjacent below for obtaining the battery unit positioned at the top is detached from.
Then lifting motor driving battery Mobile base moves down compressing battery unit and battery tray to guide head reaches
The lower position of longitudinal slot portion in guide sleeve；In the process, other batteries other than the battery unit for being located at the top
Unit generates rotation with battery tray；When guide head reaches the lower end position of guide sleeve inside spin groove portion, positioned at the top
Battery unit lower end be screwed on convex block and the bayonet part disengagement that is screwed on of adjacent battery unit upper end below；It is reached in guide head
In to guide sleeve during the lower position of longitudinal slot portion, damping piston is slipped into the damping piston cylinder, the sky in damping piston cylinder
Gas is discharged from check valve and air admission hole.
Battery Mobile base and battery unit positioned at the top is driven to move up followed by lifting motor, battery tray with
And the battery unit do not disassembled is slowly mobile upwards under the restoring force of spring and the force action of damping piston and turns round, herein
It is separated from the process positioned at the battery unit of the top and adjacent battery unit below.
Final level push rod retracts the top that the battery unit under having disassembled is made to be detached from battery disassembly and assembly seat, then lifting motor
Battery unit under driving battery Mobile base and having disassembled is moved to above unloaded cell support rack position, then horizontal push
Elongation makes the battery unit under disassembling be moved to right over cell support frame, and then electromagnet power-off makes the battery unit under disassembling
It is detached from battery Mobile base.
Further include the aircraft to convey more than one battery unit between battery disassembly and assembly seat and electric vehicle
9；There are one the suspension assemblies 97 to lift battery unit for the aircraft lower end connection.
The lifting push rod 31 of output rod vertically upward there are one being fixedly mounted above second top plate, the lifting push rod
Output rod upper end be fixedly connected with that there are one the whole rounded shutdown platforms 3 stopped for the aircraft；The shutdown
Platform forms disengaging recess 33 close to the side of the first top plate, and the position connection for shutting down close periphery above platform is useful
For the arc-shaped positioning magnet ring 32 of Aerial vehicle position；The lifting push rod is electrically connected with controller.
The suspension assembly includes the connecting rod 971 being fixedly connected with aircraft lower end, is fixedly connected under connecting rod
The kuppe 972 at end is fixedly connected on the inserted link 973 of kuppe lower end, the lifting rod 976 being slidably connected in inserted link, fixed
It is connected to the expansion-head 975 of lifting rod lower end and is fixedly mounted in kuppe and output shaft connects with lifting rod top screw thread
The motor 977 connect.The control circuit board of the motor and aircraft electrically connects.
The expansion-head includes there are one circular main part and is integrally attached to multiple valve bodies of main part periphery
Portion, in the high taper surface in intermediate low periphery, each valve body upper end offsets with taper surface for the lower end of the inserted link；It is described
The valve body portion is slided along taper surface oblique upper when lifting rod moves up, and valve body portion is made finally to be clamped on stepped hole inner wall position
In the lower section of step part；When each valve body upper end is detached from taper surface, the circumference residing for each valve body upper end outer wall is straight
Diameter is less than the internal diameter on stepped hole top.
Being equipped with to detect between the output rod upper end shut down platform lower end and lift push rod to shut down on platform is
No to stop the pressure sensor for having aircraft, the pressure sensor is electrically connected with controller.
Centre position installation is there are one by compressing switch 516 above the positioning projection seat, described by compressing switch and controller electricity
Connection.
When the battery unit quantity on the battery disassembly and assembly seat reaches pre-provisioning request, and pressure sensor detects that shutdown is flat
When stop has aircraft on platform, lifting push rod shortening makes the inserted link of suspension assembly and expansion-head be inserted into the stepped hole of battery unit
Interior, when expansion-head lower end is pressed by compressing switch, lifting push rod stops.
Then the control circuit board control motor rotation of aircraft makes expansion-head expansion be clamped on bottom battery unit
In stepped hole；The control circuit board of the aircraft is communicated to connect with controller.
The angle of 1-10 degree is formed between the cell support frame 13 and horizontal direction, and the cell support frame is towards described
Cradle side tilts；The cell support frame includes the support plate being symmetrically mounted in two opposed inner walls of housing, two institutes
It states and multigroup support wheel 131 that connection is rolled with battery unit lower end is also symmetrically rotatablely equipped in support plate so that battery list
Charging output electrode on charging electrode and cradle in member closely offsets.
The use process of the present invention is such, the controller of charging pile, the control circuit board of aircraft and electronic vapour
The control system of vehicle is connect by wireless network with server communication, and when electric vehicle not enough power supply, electricity is sent to server
Amount supply request, server are estimated electric needed for corresponding electric automobile during traveling process according to the subsequent traveling distance length of user
Then amount sends to charging pile and instructs, the data that the controller of charging pile is provided according to each electric quantity monitoring module, control conveys
The battery unit that mechanism advantage distillation is fully charged or electricity is more carries out the electricity that assembling forms integral type on battery disassembly and assembly seat
It is transported on corresponding electric vehicle by aircraft after the module of pond, so as to provide electricity supply for electric vehicle.
Embodiment 2
With reference to shown in Figure 11 to Figure 14, the present embodiment makes following improvement on the basis of embodiment 1：The aircraft 9
Include main part 90, the main part includes the fan mounting portion 900 of tubular, be connected to fan mounting portion periphery and with
Four equiangularly arranged discharge pipes 901 that fan mounting portion is connected and mounted on each discharge pipe outer end and with it is corresponding
What position discharge pipe was connected goes out vane 91.
It is located in the fan mounting portion above discharge pipe and is connected with upper bracket 902, is equipped on the upper bracket
Driving fan 951；It is located in the fan mounting portion below discharge pipe and is connected with lower carriage 903, 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 inner circumferential form downward opening outlet air gap 912, it is described go out vane inner circumferential be located at outlet air gap
Lower section is up-narrow and down-wide training wall 913, and the cone angle size of taper surface residing for the training wall is 10-20 degree；The training wall
Upper end is connected with interior curved wall 914 wide at the top and narrow at the bottom, and the cone angle size of taper surface residing for the interior curved wall is 15-25 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 goes out the horizontal component of the wind generation of the outlet air gap blowout of vane and the fan blade of upper driving fan
Rotation direction is opposite.
The side for going out vane described in each is connected with the discharge pipe of socket pipe 910, each socket pipe and corresponding position
It is slidably socketed；It being fixed by the bracket in the discharge pipe and motor 96 is installed, the output shaft of the motor is connected with screw rod 961,
Nut set 911 is connected with by stent in the socket pipe, is connected through a screw thread between the screw rod and nut set.
The stent is made of the connection strap with circumference array distribution of three or more, shape between the connection strap of the stent
The channel passed through into gas supply stream.
The upper driving fan, lower driving fan and each motor are electrically connected respectively with control circuit board.
The present invention provides driving force, the fraction that upper driving fan generates by the upper driving fan in fan mounting portion
From it is each go out vane outlet air gap blow out downwards, and combine each motor adjustment each go out vane with respect to main part distance,
So as to fulfill the horizontal flight or steering of aircraft, due to be located at aircraft periphery it is each go out vane only play adjustment flight
The effect of device posture, without the fan for being provided with power, go out not easily leading to when vane generates touching with foreign object aircraft it is out of control or
Person generates injury to human or animal, and safety is good.The aircraft appearance is named similar to four-axle aircraft with four-axle aircraft
It, four go out vane i.e. so-called " four axis " and only play the function of adjusting posture, therefore the present invention is essentially uniaxial aircraft.
Further, it is described go out vane outlet air gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward together, flown in this way
When the part in outlet air gap is stopped in row device flight course, the whole airflow influence that outlet air gap is formed is small, is conducive to fly
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan mounting portion are perpendicular, and go out the axial direction and level of vane
The angle of 5-20 degree is formed between direction, and goes out the horizontal wind-force of the wind generation of the outlet air gap blowout of vane and upper driving fan
Fan blade rotation direction it is opposite.Design in this way so that the wind energy for going out the outlet air gap blowout of vane enough offsets drive
The reaction force that dynamic fan or upper driving fan and lower driving fan generate when rotating；Also, by controlling each motor simultaneously
Rotating distance of the vane with respect to main part to change（Adjust the size of the arm of force）, it can be achieved that the whole rotating forward of aircraft or
Reversion.By adjusting one or it is two neighboring go out vane with respect to main part distance, it can be achieved that aircraft generally in skewed
State can drive aircraft to fly in the horizontal direction in this way.
The outlet air loop section increases with respect to lighter in weight for main part when some goes out vane with respect to the distance of main part
When, this goes out the height lifting of the present position of vane.
The lower, outer perimeter of the fan mounting portion is battery installation section, is connected in battery installation section and control circuit board electricity
The accumulator 92 of connection；The top for being located at battery installation section on the fan mounting portion is a circuit board installation cavity 904, described
Control circuit board is mounted in circuit board installation cavity；The upper surface of the circuit board installation cavity uniformly forms and fan mounting portion
The air inlet hole 905 of interior connection, the lateral wall of the circuit board installation cavity uniformly form vent 906.
A small amount of air-flow of the fan mounting portion enters from air inlet hole and is discharged from vent, control circuit board is played scattered
Heat effect.
The main part upper end connects the air intake cover 94 there are one semiellipse spherical shape, and item is uniformly formed on air intake cover
The air inlet of shape.
The outlet air pipe outer wall forms the more than one guiding draw runner set along its length, the socket inside pipe wall
Form the guide chute being slidably connected with the guiding draw runner.
The control circuit board control mode of the present invention is close, control with the control mode of conventional four-axle aircraft
Aircraft lifting processed is by controlling the rotating speed of driving fan to realize, the rotation of control aircraft and horizontal flight are then by controlling four
The rotating of motor realizes that control circuit and program part do not have substantial improvements, and non-present invention emphasis, therefore are not unfolded herein
Narration.
The aircraft lower end is equipped with more than one camera, convenient to control aircraft by artificial or machine vision
Accurate be accommodated to is shut down on platform.
Embodiment 3
With reference to Figure 15 and Figure 16, the present embodiment also makes following improvement on the basis of embodiment 2：Go out vane described in each
Position of the inner circumferential lower part far from discharge pipe forms Holder joint 915 of rising and falling, in each Holder joint of rising and falling respectively there are one connections
Undercarriage 93；The undercarriage, which includes, to be fixedly connected with Holder joint of rising and falling and is connected by Holder joint of rising and falling with going out inside vane
Logical outlet air tube body 931, the sliding tube 932 being slidably mounted in discharge pipe body, with outlet air tube body close to Holder joint one end of rising and falling
The supporting rod 935 of rotation connection, be connected on supporting rod far from rise and fall Holder joint one end permeability magnetic material idler wheel 936 and
Connecting rod 934 with being rotatablely connected in the middle part of sliding tube, in the middle part of supporting rod respectively.
The outlet air tube 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
It puts and is connected with articulated joint 9322, described connecting rod one end is rotatablely connected with articulated joint, and the outlet air tube 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 the outlet air tube body far from Holder joint of rising and falling, which is fixed, to be connected
Sealing cap 933 is connected to, the inner end of sealing cap is connected with spring positioning bar 9331, spring is arranged on the spring positioning bar
937, the both ends of the spring is against respectively between piston and sealing cap inner end；It is formed on the supporting rod and packs up shape in supporting rod
The connecting rod tank 9351 of the connecting rod is accommodated during state.
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 with the rising of aircraft, drop is packed up or is unfolded accordingly, when aircraft is in state of flight, goes out
Wind pressure in vane makes piston be moved together with sliding tube to sealing cap one end, so as to which sliding tube be made to drive connecting rod one end to sealing cap
Direction is moved, so as to which supporting rod lower end be made also to be rotated to sealing cap one end, so as to which undercarriage be made to be 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 as to make sliding tube
Connecting rod one end is driven to be moved to hinged seat direction, so as to which supporting rod lower end be made to turn to extreme position to hinged seat one end, so as to
Undercarriage is made 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.
After undercarriage expansion, each idler wheel just sucks the position that magnet ring is positioned on platform is shut down, conducive to aircraft
Positioning, convenient for the connection of suspension assembly and battery unit.
Claims (4)
1. a kind of electric automobile charging pile, it is characterised in that：Include the housing of rectangular shape, in housing side and
The multiple cell support framves being placed equidistant with along longitudinal direction are placed on the battery unit to charge on each cell support frame, installation
It is used in case top and battery disassembly and assembly seat above the cell support frame and in housing in each battery branch
The conveying mechanism of battery unit is conveyed between support and battery disassembly and assembly seat；
The upper part of the housing is stepped, and the case top is located at cell support frame upper section for the first top plate, the shell
Body top is the second top plate different from the part of the first top plate, and the position of the second top plate is higher than the first top plate；The housing is located at
There are one the side openings for battery unit disengaging for tool between first top plate and the second top plate；
The conveying mechanism includes longitudinal translating device associated and horizontal transport agency；The longitudinal translating device associated includes vertical peace
Different from the leading screw and lifting guide pillar of cell support frame side in housing, it is connect by screw-driven with leading screw, is led with lifting
The lifting seat and be fixedly mounted on housing bottom and the lifting motor being connect with lead screw transmission that bar is slidably connected；
The horizontal transport agency includes there are one the battery Mobile base of square and is connected to battery Mobile base and lifting seat
Between horizontally disposed horizontal push；It is fixedly connected towards the side of battery Mobile base on the lifting seat and is set there are two level
The horizontal guide put is connected with the sliding seat being slidably connected with two with horizontal guide on the battery Mobile base；The movement
4 electromagnet that battery unit is sucked by magnetic force are installed close to four vertex positions on seat；
The battery unit is integrally square, and platform wide at the top and narrow at the bottom is formed close to four vertex positions on the battery unit
Stepped through-hole is slidably fitted with the fastening screw for the magnetic conductive material being packed into from top to bottom in each step through-hole, described
The spacing collar for being plugged with to stop that fastening screw is detached from step through-hole is fixed on step through-hole top；The fastening screw is long
Spend the medium position periphery molding in direction there are one outer flange collar, be equipped between the outer flange collar upper end and spacing collar lower end to
The spring a that fastening screw is pushed down on；The electromagnet sucks to lift battery unit by magnetic field force with fastening screw；
Battery unit upper end centre position integrally connected there are one splicing convex block, splice convex block periphery equidistantly form it is more
A bayonet part that is screwed on, there are two the upper output electrodes of the annular of concentric setting for splicing convex block upper end installation；The battery
There are one splicing recess, the splicing recess inner circumferential forms and the bayonet part cooperation that is screwed on the molding of unit lower end centre position
The convex block that is screwed on of connection, the lower output electrode for splicing annular of the bottom installation there are two concentric setting in recess；
It is connected with the convex block that is screwed on by the bayonet part that is screwed between neighbouring two battery units, and bayonet part and is screwed on when be screwed on
When convex block is connected in place, the fastening screw for the battery unit being located above is inserted into the step through-hole of underlying battery unit
Top；It is connected in parallel between neighbouring two battery units by the realization that offsets of upper output electrode and lower output electrode；
Each lateral wall of the battery unit is equipped with charging electrode；The inner walls are located above each cell support frame
Position is equipped with the cradle for charging for battery unit, the charging output electrode on cradle just on battery unit
Charging electrode, which offsets, to be electrically connected；
The battery disassembly and assembly seat includes the guide sleeve that is fixedly connected on the first top plate lower end and across the first top plate with being oriented to
Cover the battery tray of sliding connection；
Battery tray upper end integrally connected is described there are one the positioning projection seat for splicing recess grafting with battery unit lower end
The periphery of positioning projection seat forms the rotation stop male part for being plugged on position between the two neighboring convex block that is screwed in splicing recess, described
The sliding bar that the guide sleeve is slidably connected is connected among battery tray lower end, there are two the sliding bar outer wall moldings
The above guide head being distributed with circumference array；
The guide sleeve inner wall forms the guide groove of quantity identical with guide head, and the guide head is slidably connected to the guiding
In slot；The guide groove includes helical groove portion and is connected to the longitudinal slot portion of helical groove portion lower end；
Spring is arranged with outside the sliding bar, the both ends of the spring is located between battery tray lower end and the first top plate upper end；
The sliding bar lower end is fixedly connected with damping piston, is located in the housing below damping piston and is equipped with and can live with damping
Fill in the damping piston cylinder being connected；The damping piston cylinder is in the groove body of upper end opening, the damping piston cylinder lower end connection
There are one the check valve by damping piston cylinder Inside To Outside one-way conduction, and the damping piston cylinder lower end is different from check valve
Position offers air admission hole, and the internal diameter of air admission hole is 1-2mm；
The lifting motor, horizontal push, each electromagnet and each cradle respectively with the control in housing
Device processed electrically connects；
When having more than one battery unit on battery disassembly and assembly seat, and needing to load another battery unit, lifting motor
Work makes lifting seat be moved to a fully charged battery unit top position in housing together with battery Mobile base, and then level pushes away
Bar extends the surface that battery Mobile base is made to be moved to battery unit, and the positioning that then electromagnet energization is sucked on battery unit is inserted
Pin battery unit lifts；
Then horizontal push, which is retracted, makes battery unit be detached from cell support frame region, and then lifting motor work drives battery unit
It is moved upward to above the battery unit loaded on battery disassembly and assembly seat, then horizontal push elongation makes battery unit to be loaded
It is moved to right over the battery unit loaded；
Then lifting motor driving battery Mobile base and the battery unit of below to be loaded move down and oppress battery tray
Disk to guide head reaches the lower end position of guide sleeve inside spin groove portion, and in the process, the battery unit loaded is together with electricity
Pond pallet moves down while generates rotation, and the convex block that is screwed on of battery unit lower end finally to be loaded is caught in the battery loaded
Position between the two neighboring bayonet part that is screwed on of unit upper end；
The battery unit for driving battery Mobile base and below to be loaded followed by lifting motor moves up, battery tray with
And the battery unit loaded is moved up and is turned round under the restoring force effect of spring, so as to make the rotation of battery unit to be loaded
It connects convex block and is caught in and loaded being screwed among bayonet part of corresponding position on battery unit；Then the electromagnet on battery Mobile base breaks
Electricity makes fastening screw disengage and be inserted into the step through-hole for the battery unit being disposed below with electromagnet；
When being disassembled on battery disassembly and assembly seat there are two above battery unit, lifting motor work drives battery movement
Seat is moved to the top position of battery unit to be dismantled on battery disassembly and assembly seat；Then horizontal push elongation moves battery Mobile base
It moves right over battery unit to be dismantled, then the battery unit positioned at the top is sucked in electromagnet energization, while causes position
It is detached from the fastening screw of the battery unit of the top and the step through-hole of battery unit adjacent below；
Then lifting motor driving battery Mobile base moves down compressing battery unit and battery tray to guide head reaches guiding
The lower position of longitudinal slot portion in set；In the process, other battery units other than the battery unit for being located at the top
Rotation is generated with battery tray；When guide head reaches the lower end position of guide sleeve inside spin groove portion, the electricity positioned at the top
The bayonet part disengagement that is screwed on of be screwed on convex block and the battery unit upper end adjacent below of pool unit lower end；Reach in guide head and lead
Into set during the lower position of longitudinal slot portion, damping piston is slipped into the damping piston cylinder, the air in damping piston cylinder from
Check valve and air admission hole discharge；
Battery Mobile base and battery unit positioned at the top is driven to move up followed by lifting motor, battery tray and not
The battery unit disassembled is slowly mobile upwards under the restoring force of spring and the force action of damping piston and turns round, in this process
In be located at the battery unit of the top and adjacent battery unit below is separated from；
Final level push rod retracts the top that the battery unit under having disassembled is made to be detached from battery disassembly and assembly seat, and then lifting motor drives
Battery Mobile base and the battery unit under having disassembled are moved to above unloaded cell support rack position, and then horizontal push extends
The battery unit under disassembling is made to be moved to right over cell support frame, then electromagnet power-off makes the battery unit and electricity under disassembling
Pond Mobile base is detached from.
2. a kind of electric automobile charging pile as described in claim 1, it is characterised in that：It has further included in battery disassembly and assembly seat
The aircraft of more than one battery unit is conveyed between electric vehicle；There are one the aircraft lower end connections to lift
The suspension assembly of battery unit；
The lifting push rod of output rod vertically upward there are one being fixedly mounted above second top plate, the output of the lifting push rod
Bar upper end is fixedly connected with that there are one the whole rounded shutdown platforms stopped for the aircraft；The shutdown platform is close
The side of first top plate forms disengaging recess, and the position shut down above platform close to periphery is connected with for aircraft
The arc-shaped positioning magnet ring of positioning；The lifting push rod is electrically connected with controller；
The suspension assembly includes the connecting rod being fixedly connected with aircraft lower end, is fixedly connected on the water conservancy diversion of connecting rod lower end
Cover, is fixedly connected on the inserted link of kuppe lower end, and the lifting rod being slidably connected in inserted link is fixedly connected on lifting rod lower end
Expansion-head and it is fixedly mounted on the motor that in kuppe and output shaft is threadedly coupled with lifting rod top；
The control circuit board of the motor and aircraft electrically connects；
The expansion-head includes there are one circular main part and is integrally attached to multiple valve body portions of main part periphery, institute
The lower end of inserted link is stated in the high taper surface in intermediate low periphery, each valve body upper end offsets with taper surface；The lifting
The valve body portion is slided along taper surface oblique upper when bar moves up, and valve body portion is made finally to be clamped on stepped hole inner wall and is located at platform
The lower section of exponent part；When each valve body upper end is detached from taper surface, the circle diameter residing for each valve body upper end outer wall is small
Internal diameter in stepped hole top.
3. a kind of electric automobile charging pile as claimed in claim 2, it is characterised in that：The shutdown platform lower end is pushed away with lifting
It is equipped with to detect the pressure sensor shut down and whether stop aircraft on platform, the pressure between the output rod upper end of bar
Force snesor is electrically connected with controller；
Centre position installation is described to be electrically connected by compressing switch with controller there are one by compressing switch above the positioning projection seat；
When the battery unit quantity on the battery disassembly and assembly seat reaches pre-provisioning request, and pressure sensor is detected and shut down on platform
When stop has aircraft, lifting push rod shortening makes the inserted link of suspension assembly and expansion-head be inserted into the stepped hole of battery unit,
When expansion-head lower end is pressed by compressing switch, lifting push rod stops；
Then the control circuit board control motor rotation of aircraft makes expansion-head be unfolded to be clamped on the step of bottom battery unit
In hole；
The control circuit board of the aircraft is communicated to connect with controller.
4. a kind of electric automobile charging pile as described in claim 1, it is characterised in that：The cell support frame and horizontal direction
Between form the angle of 1-10 degree, and the cell support frame is tilted towards the cradle side；The cell support frame includes
Have the support plate being symmetrically mounted in two opposed inner walls of housing, be also symmetrically rotatablely equipped in two support plates it is multigroup with
Battery unit lower end rolls the support wheel of connection so that the charging output electrode on the charging electrode and cradle on battery unit
Closely offset.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710663810.9A CN107487218B (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201810383234.7A CN108583328A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201810383267.1A CN108583329A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710663810.9A CN107487218B (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810383234.7A Division CN108583328A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201810383267.1A Division CN108583329A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
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| CN107487218A CN107487218A (en) | 2017-12-19 |
| CN107487218B true CN107487218B (en) | 2018-07-10 |
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| CN201810383267.1A Withdrawn CN108583329A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201810383234.7A Withdrawn CN108583328A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201710663810.9A Active CN107487218B (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810383267.1A Withdrawn CN108583329A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
| CN201810383234.7A Withdrawn CN108583328A (en) | 2017-08-06 | 2017-08-06 | A kind of electric automobile charging pile |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109120043A (en) * | 2018-10-23 | 2019-01-01 | 广州赛特智能科技有限公司 | A kind of robot battery charging unit |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105553058A (en) * | 2015-12-25 | 2016-05-04 | 江苏汇智知识产权服务有限公司 | High-efficiency environment-friendly charging pile |
| CN105990876A (en) * | 2015-12-21 | 2016-10-05 | 小米科技有限责任公司 | Charging pile and identification method and device thereof and automatic cleaning equipment |
| CN206124787U (en) * | 2016-08-26 | 2017-04-26 | 中山市浩成自动化设备有限公司 | Novel safe and convenient electric pile equipment of operating that fills |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101097226B1 (en) * | 2010-02-01 | 2011-12-21 | 에스비리모티브 주식회사 | Battery pack |
-
2017
- 2017-08-06 CN CN201810383267.1A patent/CN108583329A/en not_active Withdrawn
- 2017-08-06 CN CN201810383234.7A patent/CN108583328A/en not_active Withdrawn
- 2017-08-06 CN CN201710663810.9A patent/CN107487218B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105990876A (en) * | 2015-12-21 | 2016-10-05 | 小米科技有限责任公司 | Charging pile and identification method and device thereof and automatic cleaning equipment |
| CN105553058A (en) * | 2015-12-25 | 2016-05-04 | 江苏汇智知识产权服务有限公司 | High-efficiency environment-friendly charging pile |
| CN206124787U (en) * | 2016-08-26 | 2017-04-26 | 中山市浩成自动化设备有限公司 | Novel safe and convenient electric pile equipment of operating that fills |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108583329A (en) | 2018-09-28 |
| CN107487218A (en) | 2017-12-19 |
| CN108583328A (en) | 2018-09-28 |
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Effective date of registration: 20211116 Address after: 236600 38, Jianyi village, yuanqiang Town, Taihe County, Fuyang City, Anhui Province Patentee after: Ruan Fang Address before: 325000 building 3, block a, No. 329, Jinhai Third Road, economic and Technological Development Zone, Wenzhou City, Zhejiang Province Patentee before: Wenzhou ruichu Technology Co., Ltd |