CN206293942U - From seeking formula flight charging equipment, system - Google Patents
From seeking formula flight charging equipment, system Download PDFInfo
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- CN206293942U CN206293942U CN201720001751.4U CN201720001751U CN206293942U CN 206293942 U CN206293942 U CN 206293942U CN 201720001751 U CN201720001751 U CN 201720001751U CN 206293942 U CN206293942 U CN 206293942U
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- 238000005299 abrasion Methods 0.000 description 1
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- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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Abstract
The utility model provides one kind from formula flight charging equipment, system is sought, and is related to charging equipment technical field.This includes power supply source and the charging head being arranged on power supply source from formula flight charging equipment is sought, and the first flight structure is provided with the charging head, and charging head is flown to electrical equipment position by the first flight structure, and charging operations are carried out to electrical equipment.Using the utility model, manual steps when being charged to electrical equipment are reduced, improve the automaticity of charging equipment, improve charge efficiency and Consumer's Experience.
Description
Technical field
The utility model is related to charging equipment technical field.
Background technology
In recent years, all circles are energetically to such as motor vehicle driven by mixed power, electric vehicle, or use clean energy resource as dynamic
The commercialization of the fuel-cell vehicle in power source is studied.Electric vehicle is supplied with external power source and then battery is charged,
And produced as the power of mechanical energy by being coupled to the motor of wheel by the use of the charging voltage in battery.In other words, because
It is the charging voltage drive motor during electric vehicle uses battery, Large Copacity rechargeable battery is used in electric vehicle and sets
The battery charging equipment for being charged to Large Copacity rechargeable battery is equipped with, car owner needs to be frequently utilized that charging equipment fills to battery
Electricity is ensureing energy resource supply.
Conventional electric vehicle charging equipment, by taking charging pile as an example, generally includes casing at present, and electricity is provided with casing
Gas equipment etc., and power supply interface is provided with casing, live wire is connected on the power supply interface, the outer end of the electric wire is connected with
Charging gun.So, using the electric connection of electric wire and power supply interface so that charging gun can be connected with charging source, by charging gun and
When the charging inlet of the batteries such as electric automobile is connected, then the charging such as electric automobile is can be implemented as.When being charged, Yong Huxu
Will first by electric automobile during traveling to charging pile adjacent domain, then need artificial operation by the power supply interface of electric wire and charging pile,
Electric wire is connected with the charging inlet of electric automobile, then could realize charging electric automobile etc., when charging is finished, then needs
Artificial operation causes to be disconnected between the two, operates very inconvenient, complete manual operation, using inconvenience, necessarily
Charge efficiency and Consumer's Experience are reduced in degree.
Simultaneously as the electric wire of above-mentioned charging pile is chronically exposed to outward, therefore, electric wire easily weares and teares, and its outer layer
It is easily aging.When user is when charging, then easily there is the phenomenon of electric leakage, trigger electric shock accidents, or even threat to life, and no matter
During charging, or when not charging, electric wire all exposes outside, using very inconvenient.Electric wire is connected through outside casing with charging source
Charging inlet realizes that charging inlet is generally exposed outside, and the phenomenon that electric wire is disconnected with it easily occurs, or appearance is damaged
Bad phenomenon, causing to charge fails, and greatly increases operation of the user when charging, in-convenience in use, and there is larger safety
Hidden danger.
The content of the invention
The purpose of this utility model is：Overcome the deficiencies in the prior art, there is provided a kind of to seek formula flight charging equipment certainly, with
And system.Charging equipment of the present utility model does not require that electrical equipment is located at charging equipment adjacent domain, and user without artificial
With the charging inlet of the power supply interface, electric wire and electrical equipment of power supply source be connected electric wire by operation, improves charging equipment oneself
Dynamicization degree, improves charge efficiency and Consumer's Experience.
The technical solution of the utility model is not limited to the charging equipment for electric automobile, and other electrical equipments were used
Artificial operation connection power supply source also can be by using the utility model with the not convenient operation of electrical equipment the need for being run into journey
The charging equipment of offer is addressed.
To realize above-mentioned target, the utility model provides following technical scheme.
It is a kind of to seek formula flight charging equipment, including power supply source and the charging head being arranged on power supply source, the charging head certainly
On be provided with the first flight structure, charging head is flown to electrical equipment position by the first flight structure, electrical equipment is entered
Row charging operations.
Further, charging head connects power supply source by electric wire, the second flight structure is provided with the electric wire, in charging head
In flight and/or charging process, the position of electric wire is adjusted by second flight structure.
Further, charging head connects power supply source by electric wire, and electric wire lower section is provided with using lower section supporting surface as receiving
The supporting construction that power fulcrum is realized, in charging head flight and/or charging process, electric wire is adjusted by the supporting construction
Position.
Further, flight structure is rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella wing structure or flapping wing knot
Structure.
Further, the power source of flight structure in the following way one or more：Mode one, is set on charging head
Power supply；Mode two, sets flight power source special, electrically connects power source special and flight structure.
Further, also including recognition unit, the recognition unit is recognized simultaneously by gathering image information and/or audio-frequency information
Position where judging electrical equipment.
Further, also including wireless positioning unit, wireless signal Transmit-Receive Unit, the nothing are provided with the electrical equipment
Line positioning unit gathers the signal of wireless messages Transmit-Receive Unit, recognizes and judge the position of electrical equipment.
Further, also including electrical equipment information unit, after user orders charging service, charging equipment can obtain the use
The identification information of the electrical equipment at family.
Further, the interface position unit of the charging inlet positional information for obtaining electrical equipment is provided with charging head.
Further, electrical equipment fixed structure and charging inlet embedded structure, the electrical equipment are provided with charging head
Fixed structure is used to for charging head to be fixed on electrical equipment, and the charging inlet embedded structure is used to connect the charging of charging head
Joint and charging inlet.
Further, the charging connector of charging head is connected with power supply source by electric wire, the charging connector and electrical equipment
Turn-on current after charging inlet docking, is charged by electric wire to electrical equipment.
Further, the charging connector of charging head and power supply source wireless connection, the charging of the charging connector and electrical equipment
After interface docking, charged to electrical equipment after charging connector receives the electromagnetic wave of power supply source and is converted into electric current.
The utility model additionally provides a kind of from seeking formula flight charging system, including formula of seeking certainly in preceding solution flies
Row charging equipment, and electrical equipment, the electrical equipment are used to receive described from the charging head for seeking formula flight charging equipment.
The utility model compared with prior art, as an example, has the following advantages that due to using above technical scheme
And good effect：1) user is without manually operating the power supply interface of electric wire and power supply source, electric wire and electrical equipment when charging
Charging inlet is connected, and when charging is finished, causes to be disconnected between charging equipment and electrical equipment without artificial operation, is improved
The automaticity of charging equipment, improves charge efficiency and Consumer's Experience.2) further, charging head passes through nothing with power supply source
The mode of line is connected, it is to avoid the limitation of charging wire length in the prior art, and the abrasion of charging electric wire, aging may be caused
Potential safety hazard.
Brief description of the drawings
Fig. 1 is the structural representation sought certainly when formula flight charging equipment works that the utility model embodiment one is provided.
Fig. 2 is the structural representation one of the charging head in above-described embodiment.
Fig. 3 is the structural representation two of the charging head in above-described embodiment.
Fig. 4 is the part-structure schematic diagram one for seeking formula flight charging equipment certainly that the utility model embodiment two is provided.
The part-structure schematic diagram two for seeking formula flight charging equipment certainly that Fig. 5 is provided for above-described embodiment.
Fig. 6 is the function structure chart for seeking formula flight charging system certainly that embodiment two is provided.
Fig. 7 is the part-structure schematic diagram for seeking formula flight charging equipment certainly that the utility model embodiment three is provided.
The flow chart for seeking formula flight charging method certainly that Fig. 8-10 is provided for the utility model example IV.
Label is as follows in figure：
From seeking formula flight charging equipment 100；
Power supply source 110；
Electric wire 120；
Charging head 130, charging head body 131, charging connector 132；
Power lug 140；
Electrical equipment 200；
First flight structure 300, flying wing 301, flight dynamic devices 302, flying wing connector 303；
Second flight structure 400, flying wing 401, flight dynamic devices 402；
Supporting construction 500；
Power supply receives structure 600, electromagnetic wave receiving element 601, pose adjustment element 602, electric current conversion elements 603.
Specific embodiment
Below in conjunction with the drawings and specific embodiments the utility model is provided seek certainly formula flight charging equipment, system make into
One step is described in detail.It should be noted that the combination of the technical characteristic or technical characteristic described in following embodiments should not
It is considered as isolated, they can be mutually combined so as to reach superior technique effect.In the accompanying drawing of following embodiments,
The identical label that each accompanying drawing occurs represents identical feature or part, in can be applied to different embodiments.
It should be noted that, structure, ratio, size depicted in this specification institute accompanying drawings etc. are only used to coordinate explanation
Content disclosed in book, so that those skilled in the art understands and reads, is not limited to the enforceable limit of utility model
Fixed condition, the modification of any structure, the change of proportionate relationship or the adjustment of size, in the work(for not influenceing utility model can be generated
Under effect and the purpose to be reached, all should fall in the range of the technology contents disclosed in utility model to be covered.This practicality
The scope of new preferred embodiment includes other realization, wherein order that is shown or discussing can not be pressed, including root
According to involved function by it is basic simultaneously in the way of or in the opposite order, carry out perform function, this should be by reality of the present utility model
A person of ordinary skill in the field is applied to be understood.
The technical solution of the utility model includes but is not limited to the charging equipment for electric automobile, and other electrical equipments make
Artificial operation connection power supply source also can be by using this practicality with the not convenient operation of electrical equipment the need for being run into during
The charging equipment of new offer is addressed.Typical mode, electrical equipment can also be various aircraft, Portable movable end
End etc..
Embodiment one
Fig. 1 is the structural representation sought certainly when formula flight charging equipment works that the utility model embodiment one is provided.
Fig. 2 is the structural representation one of the charging head in above-described embodiment.
Fig. 3 is the structural representation two of the charging head in above-described embodiment.
It is shown in Figure 1, it is a kind of from seeking formula flight charging equipment 100, including power supply source 110 be arranged on power supply source 110
On charging head 130, be provided with the first flight structure 300 on the charging head 130, charging head 130 can be tied by the first flight
Structure 300 flies to the position of electrical equipment 200, and charging operations are carried out to electrical equipment 200.
The power supply source is the structure that may be electrically connected to power network, and it can extract electric energy from power network and make it possible to supply
Charging equipment is used.The power supply source extracts the mode of electric energy from power network, typically can be by electric wire by power utilization network
Electric energy is transferred in power supply source.The structure of the power supply source, it is unrestricted as an example, can be using the charging of body structure
The structures such as stake, charging station.
The charging head is the connection equipment for connecting electrical equipment charging inlet and power supply source, in charging head and electrical equipment
It is capable of achieving to charge after charging inlet connection, the structure of charging head is typically related to electrical equipment, charging current type.Referring to Fig. 2
Shown, charging head 130 generally includes charging head body 131 and charging connector 132.Charging head body 131 passes through power lug 140
It is connected with electric wire 120.
The type association of charging connector 132 and electrical equipment, different electrical equipments match different charging connectors.Charge
The structure of joint, it is unrestricted as an example, by taking electric automobile as an example, charging pole seat and charging pole are generally included, it is shown
Charging pole one end is connected with electric wire, and the other end is connected with the charging circuit of electrical equipment, is embodied as electrical equipment or electricity consumption sets
Standby battery charges.
Referring to Fig. 2, the first flight structure 300 is provided with charging head 130, the first flight structure includes the He of flying wing 301
Flight dynamic devices 302.The flying wing of flight structure can be using rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella
Wing structure or flapping wing structure etc..Flight dynamic devices can use piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching press
Formula is jet-propelled, and the power set in the present embodiment use electrodynamic type engine.Can be installation as the power source of motor
Power supply on charging head, it is also possible to set flight power source special in addition, electrically connects power source special and flight structure, in the present embodiment
The power supply of flight structure is directly installed on charging head.Power supply can be the battery in charging head body 131, store
Battery is electrically connected with the power set of flying wing.It is easily understood that in the case that charging head is provided with battery, can be in charging head
Circuit board on charging circuit is set, charging circuit is used for when battery electric quantity is not enough as battery is charged.The electricity that charges
Road is known to those skilled in the art, for example, charging circuit includes the voltage reduction module, rectification module and the filtering mould that are sequentially connected
Block, the voltage reduction module is used to for external power source High Level AC Voltage to be converted into low-voltage AC, and the rectification module is used for will be low
Pressure alternating current is converted into low-voltage DC, and the filtration module is used to be filtered the direct current after rectification.The electricity of charging head
Road plate can also include the Voltage stabilizing module with overvoltage and overcurrent protection, prevent overvoltage or excessively stream from causing circuit components
Damage.The Voltage stabilizing module is known to those skilled in the art, and here is omitted.
The quantity of the first flight structure 300 set on charging head 130 can be one or more, the first flight structure 300
Comprising the quantity of flying wing can also be one or more.Fig. 3 is illustrated using 2 flying wings as the first flight structure
300 situation.Shown in Figure 3, the first flight structure 300 includes flying wing 301, flight dynamic devices 302 and connection two
The flying wing connector 303 of individual flying wing.Obviously, the quantity of above-mentioned flying wing can also be 4,6 etc., flying wing connector
303 can be using yi word pattern, X fonts ,+font etc..
In the present embodiment, accurately flown for ease of charging head to electrical equipment position, further, the charging sets
Standby upper also including recognition unit, the recognition unit is recognized and judges that electricity consumption sets by gathering image information and/or audio-frequency information
The position at standby place.Unrestricted as an example, the structure of the collection image information can be on charging equipment
Camera head, the structure of the collection audio-frequency information can be the microphone on charging equipment, and gathering charging with this sets
The image and/or acoustic information on standby periphery, and then electrical equipment is recognized, can also further obtain the positional information of electrical equipment.
The method for recognizing electrical equipment, in addition to collection image information and/or audio-frequency information, also can be by wireless location side
Formula, can set wireless positioning unit on charging equipment, corresponding, wireless signal transmitting-receiving is provided with the electrical equipment single
Unit, the wireless positioning unit gathers the signal of wireless messages Transmit-Receive Unit, recognizes and judge the position of electrical equipment.Often at present
The location technology seen mainly has PPD location technologies, gps satellite positioning, bluetooth to position, WIFI network positioning, the Big Dipper are positioned,
GPRS/CDMA mobile communication technologies positioning etc..As a example by commonly using at present based on mobile terminal positioning technology, the location technology
Principle is：The Base Transmitter signal of multiple known locations, institute's transmission signal carries the characteristic information relevant with base station location, when
After mobile terminal receives these signals, itself and the geometry site between each base station are determined, and according to related algorithm to it
Self-position carries out positioning estimation, so as to obtain the positional information of itself.
The charging equipment of the present embodiment, also including electrical equipment information unit, after user orders charging service, charging sets
The identification information of the standby electrical equipment that can obtain the user.Electrical equipment information unit obtains the side of the identification information of electrical equipment
Formula, unrestricted as an example, by taking electric vehicle as an example, such as user is after ordering charging service, you can by the car of user
The trade mark, vehicle and positional information are transferred to the electrical equipment information unit of charging equipment, in this way, charging equipment is to obtain this
The identification information of the electrical equipment of user.
Need to be properly inserted in the charging inlet of electrical equipment in view of charging head, acquisition is additionally provided with the charging head
The interface position unit of the charging inlet positional information of electrical equipment.The charging inlet of electrical equipment is obtained in interface position unit
Positional information after, by charging head set electrical equipment fixed structure and charging inlet embedded structure realizing charging
Head and the connection of charging inlet.
The electrical equipment fixed structure, for charging head to be fixed on into electrical equipment.It is unrestricted as an example, than
Such as the rotary buckle can be fixed on sucker or fixed claw in electrical equipment, or for that can be fixed at charging inlet outer rim or
Fixed claw.
The charging inlet embedded structure, charging connector and charging inlet for connecting charging head.As an example rather than
Limitation, such as be contractable element or foldable member on charging inlet, in charging connector alignment charging inlet institute
Postpone in place, control contractable element or foldable member elongation will realize connection in charging connector insertion charging inlet.
The transmission means of electric energy, can also be used using wire transmission and be wirelessly transferred.In the present embodiment, charging head fills
Electric connection is connected with power supply source by electric wire 120, the charging connector docked with the charging inlet of electrical equipment after turn-on current,
Charged to electrical equipment by electric wire 120.
Embodiment two
Fig. 4 is the part-structure schematic diagram one for seeking formula flight charging equipment certainly that the utility model embodiment two is provided.
The part-structure schematic diagram two for seeking formula flight charging equipment certainly that Fig. 5 is provided for above-described embodiment.
Fig. 6 is the function structure chart for seeking formula flight charging system certainly that embodiment two is provided.
The difference of the embodiment and embodiment one, is the structure that adjustment electric wire position is provided with the electric wire transmitted electricity, with
This, charging head 130 fly and/or charging process in, suitably reduce the shadow that other objects in wire pair environment are caused
Ring.
The structure of electric wire position is adjusted in the present embodiment, can be adjusted using flight structure.It is shown in Figure 4, charge
First 130 connect the (not shown) of power supply source 110 by electric wire 120.The second flight structure 400 is provided with the electric wire 120, is being filled
Dateline 130 fly and/or charging process in, by second flight structure 400 adjust electric wire position.Second flight structure
400 structure can be similar with the first flight structure, unrestricted as an example, including flying wing 401 and flight dynamic devices
402.The flying wing of the second flight structure also can be using rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella wing structure
Or flapping wing structure etc..Flight dynamic devices can use piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching type or spray
Gas formula, the power set in the present embodiment use electrodynamic type engine, similar to drive form with the first flight structure, herein not
Repeat again.The quantity of the second flight structure 400 set on electric wire 120 can be one or more, and the second flight structure 400 is included
The quantity of flying wing can also be one or more, can be selected according to the length of electric wire, material etc..
In addition to aforesaid way, the structure of adjustment electric wire position can also be the solid support thing that electric wire lower section is set, such as
Support bar, support frame etc..Shown in Figure 5, charging head 130 connects the (not shown) of power supply source 110, the electricity by electric wire 120
The lower section of line 120 is provided with the supporting construction 500 realized as fulcrum force using lower section supporting surface, in charging head flight and/or
In charging process, the position of electric wire is adjusted by the supporting construction 500.It is unrestricted as an example, it is preferred that charging head exists
Position that can be according to where supporting construction in flight course selects flight path, can accurately lay on the support structure electric wire
Portion.
Using it is above-mentioned from seek formula flight charging equipment certainly seeking formula flight charging system to function structure chart referring to Fig. 6 institutes
Show.Include that electrical equipment is used to receive described from formula flight charging equipment, and electrical equipment is sought from formula flight charging system is sought
From the charging head for seeking formula flight charging equipment.Include power supply source, charging head, recognition unit, wireless from formula flight charging equipment is sought
Positioning unit, electrical equipment information unit and electric wire.
The recognition unit is by gathering image information and/or audio-frequency information is recognized and position where judging electrical equipment
Put.The method for recognizing electrical equipment, in addition to collection image information and/or audio-frequency information, also can be by wireless location mode, can be
Wireless positioning unit is set on charging equipment, it is corresponding, wireless signal Transmit-Receive Unit, the nothing are provided with the electrical equipment
Line positioning unit gathers the signal of wireless messages Transmit-Receive Unit, recognizes and judge the position of electrical equipment.The charging of the present embodiment
Equipment also includes electrical equipment information unit, and after user orders charging service, the electricity consumption that charging equipment can obtain the user sets
Standby identification information.Electrical equipment information unit obtains the mode of the identification information of electrical equipment, unrestricted as an example, with
As a example by electric vehicle, such as user is after ordering charging service, you can pass the license plate number of user, vehicle and positional information
The electrical equipment information unit of charging equipment is defeated by, in this way, charging equipment is the identification letter of the electrical equipment for obtaining the user
Breath.
Need to be properly inserted in the charging inlet of electrical equipment in view of charging head, acquisition is additionally provided with the charging head
The interface position unit of the charging inlet positional information of electrical equipment.The charging inlet of electrical equipment is obtained in interface position unit
Positional information after, by charging head set electrical equipment fixed structure and charging inlet embedded structure realizing charging
Head and the connection of charging inlet.Said structure is similar with embodiment one, repeats no more.
Flight structure, the wire of transmission electric current and position adjustment structure are provided with electric wire.Position adjustment structure can be used
Mode described above, repeats no more.
Embodiment three
Fig. 7 is the part-structure schematic diagram for seeking formula flight charging equipment certainly that the utility model embodiment three is provided.
The difference of the embodiment and embodiment one, is that electrical equipment is charged using wireless transmission method.
Shown in Figure 7, charging connector 132 and the (not shown) wireless connection of power supply source 110 of charging head 130 are described to fill
After electric connection 132 is docked with the charging inlet of electrical equipment, the electromagnetic wave that power supply source is launched is received by charging connector 132, and
The electromagnetic wave that will be received charges after being converted into electric current to electrical equipment.
Unrestricted as an example, the electromagnetic wave can be microwave or laser.It is electrically charged aircraft and receives microbeam, will
Microwave is converted into electric current, so as to realize being electrically charged the charging of spacecraft.It is shown in Figure 7 by taking microwave as an example, charging head
Power supply is installed on 130 and receives structure 600, the power supply receives structure 600 includes electromagnetic wave receiving element 601, pose adjustment
Element 602 and electric current conversion elements 603.Now, power supply source includes that microwave can be converted the current into and can launch the structure of microwave,
It is unrestricted as an example, such as including high frequency electric source, magnetron, power amplifier and microwave transmission antenna, first by storing
Battery pack provides energy for high frequency electric source, and high frequency electric source produces high frequency electric, while batteries produce low-frequency current, the height
Frequency electric current and low-frequency current are input in magnetron simultaneously, in magnetron the orthogonal stationary magnetic field of low-frequency current generation and
Steady electric field, the electromagnetic field of high frequency produced with high frequency electric interacts, the energy conversion obtained from stationary magnetic field
It is microwave, is exported microwave to power amplifier by magnetron, microwave is carried out by energy amplification by power amplifier, and pass through
Microwave transmission antenna is launched to head location to be charged direction.
In the present embodiment, the microwave that power supply source is launched, appearance can be received as electromagnetic wave receiving element 601 using dish aerials
State adjustment element 602 is used to adjusting position, height and the angle of dish aerials, and electric current conversion elements 603 are used to receive
Microwave is converted into electric current.Unrestricted as an example, electric current conversion elements 603 may include that low-tension current diode, electron beam are returned
Rotation accelerator, two magnetic elements and convertor, conversion process can be in the following way.Obtain micro- by dish aerials first
Ripple, two magnetic elements produce stationary magnetic fields, and microwave is input to low-tension current diode and electron beam cyclotron composition
In circuit, electronics acceleration is converted into high-frequency ac current in the presence of the stationary magnetic field, electron beam cyclotron will
High-frequency ac current is input to convertor, and alternating current is converted into DC current by convertor, you can DC current is defeated
Enter and charged to the batteries of electrical equipment.
When using Laser Transmission energy, power supply source includes that laser and the structure that Laser emission is gone out can be produced.Now,
Using light-sensitive device as the receiving element of laser, photogenerated current, photogenerated current warp are generated after light-sensitive device reception laser light photograph
Overcurrent amplifier exports electric signal, forms DC current.
Example IV
The flow chart for seeking formula flight charging method certainly that Fig. 8-10 is provided for the utility model example IV.
The utility model additionally provides one kind from formula flight charging method is sought, and comprises the following steps：
S100, the charging head that can be flown flies to electrical equipment position.
S200, charging head carries out charging operations after being docked with electrical equipment to it.
The mode that charging head flies to electrical equipment position in step S100 may include following steps：
S110, the positional information where positioning unit acquisition electrical equipment on charging head；Or, power supply belonging to charging head
The positional information where positioning unit acquisition electrical equipment on source.
S120, controls the charging head to fly to electrical equipment position according to the positional information for obtaining.
The interface position list of the charging inlet positional information for obtaining electrical equipment is provided with the present embodiment, on charging head
Unit, unrestricted as an example, the mode that charging head is docked with electrical equipment in step S200 may include following steps.
S210, interface position unit obtains the positional information of the charging inlet of electrical equipment.
S220, controls the charging head to drop to charging inlet position according to the positional information for obtaining.
S230, controls the charging connector of charging head to be docked and connected with the charging inlet.
Electrical equipment fixed structure and charging inlet embedded structure are provided with the present embodiment, on charging head, electricity consumption is obtained
After the charging inlet positional information of equipment, charging head is fixed on charging inlet or charging inlet by electrical equipment fixed structure
Near zone；The charging connector insertion charging inlet of the charging inlet embedded structure control charging head on charging head；Charging connector
Charging operations are carried out after being connected with charging inlet；After charging complete, charging head returns to power supply source position.
Foregoing description is only the description to the utility model preferred embodiment, not to any limit of the utility model scope
Fixed, the scope of preferred embodiment of the present utility model includes other realization, wherein can not press shown or discussion suitable
Sequence carrys out perform function.Any change, modification that the those of ordinary skill in the utility model field does according to the disclosure above content,
Belong to the protection domain of claims.
Claims (10)
- It is 1. a kind of to seek formula flight charging equipment, including power supply source and the charging head being arranged on power supply source certainly, it is characterised in that：Fill The first flight structure is provided with dateline, charging head is flown to electrical equipment position by the first flight structure, electricity consumption is set It is standby to carry out charging operations.
- It is 2. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Charging head is connected by electric wire and powered Source, is provided with the second flight structure on the electric wire, in charging head flight and/or charging process, flown by described second The position of structural adjustment electric wire.
- It is 3. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Charging head is connected by electric wire and powered Source, electric wire lower section is provided with the supporting construction realized as fulcrum force using lower section supporting surface, charging head flight and/ Or in charging process, the position of electric wire is adjusted by the supporting construction.
- It is 4. according to claim 1 and 2 to seek formula flight charging equipment certainly, it is characterised in that：The power source of flight structure is adopted With one or more of following manner,Mode one, sets power supply on charging head；Mode two, sets flight power source special, electrically connects power source special and flight structure.
- It is 5. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Also include recognition unit, the knowledge Other unit is by gathering image information and/or audio-frequency information is recognized and position where judging electrical equipment.
- It is 6. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Also include wireless positioning unit, institute State and be provided with electrical equipment wireless signal Transmit-Receive Unit, the wireless positioning unit gathers the letter of wireless messages Transmit-Receive Unit Number, recognize and judge the position of electrical equipment.
- It is 7. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Also include electrical equipment information list Unit, after user orders charging service, charging equipment can obtain the identification information of the electrical equipment of the user.
- It is 8. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Acquisition electricity consumption is provided with charging head The interface position unit of the charging inlet positional information of equipment.
- It is 9. according to claim 1 to seek formula flight charging equipment certainly, it is characterised in that：Electrical equipment is provided with charging head Fixed structure and charging inlet embedded structure, the electrical equipment fixed structure are used to for charging head to be fixed on electrical equipment, The charging inlet embedded structure is used to connect the charging connector and charging inlet of charging head.
- 10. it is a kind of to seek formula flight charging system certainly, it is characterised in that including：Formula flight charging equipment is sought certainly any one of claim 1-9；Electrical equipment, it is described from the charging head for seeking formula flight charging equipment for receiving.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720001751.4U CN206293942U (en) | 2017-01-03 | 2017-01-03 | From seeking formula flight charging equipment, system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720001751.4U CN206293942U (en) | 2017-01-03 | 2017-01-03 | From seeking formula flight charging equipment, system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206293942U true CN206293942U (en) | 2017-06-30 |
Family
ID=59098656
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720001751.4U Expired - Fee Related CN206293942U (en) | 2017-01-03 | 2017-01-03 | From seeking formula flight charging equipment, system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206293942U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106505697A (en) * | 2017-01-03 | 2017-03-15 | 上海量明科技发展有限公司 | From seeking formula flight charger, system and method |
-
2017
- 2017-01-03 CN CN201720001751.4U patent/CN206293942U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106505697A (en) * | 2017-01-03 | 2017-03-15 | 上海量明科技发展有限公司 | From seeking formula flight charger, system and method |
| CN106505697B (en) * | 2017-01-03 | 2024-02-27 | 上海量明科技发展有限公司 | Self-seeking type flight charging equipment, system and method |
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| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
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| CF01 | Termination of patent right due to non-payment of annual fee |