CN206775150U - The aircraft and charging system of auxiliary charging - Google Patents
The aircraft and charging system of auxiliary charging Download PDFInfo
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- CN206775150U CN206775150U CN201720103706.XU CN201720103706U CN206775150U CN 206775150 U CN206775150 U CN 206775150U CN 201720103706 U CN201720103706 U CN 201720103706U CN 206775150 U CN206775150 U CN 206775150U
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Abstract
The utility model provides the aircraft and charging system of a kind of auxiliary charging, is related to charging equipment technical field.A kind of aircraft of auxiliary charging, including：Structure is captured, to fly in aircraft to electrical equipment situation, electrical equipment is captured；Charge auxiliary unit, to be carry in aircraft in the case that electrical equipment flies to charging equipment, connects the charging circuit of electrical equipment.With the aircraft of auxiliary charging of the present utility model, the charging of electrical equipment is no longer limited by factors such as power supply source interface position, conductor lengths, is improved the automaticity of electrical equipment charging, is improved charge efficiency and Consumer's Experience.
Description
Technical field
It the utility model is related to charging equipment technical field, more particularly to a kind of intelligent charge technique field.
Background technology
With the fast development of electrical equipment, at home, factory, increasing electrical equipment can under natural environment
Realize unattended, these electrical equipments need to be connected with power interface, and/or setting electricity storage structure such as battery is to provide
Power supply.Some electrical equipments are directly connected in power outlet, and these electrical equipments can only be on the ground for being provided with power outlet
Side's work.In addition also some electrical equipments be can by the advance storing up electricity of battery pack, then again by battery supply needed for power supply,
In battery electric quantity deficiency, it usually needs user's active operation, carry out charging operations for electrical equipment, often user needs to close for it
The charge condition of electrical equipment is noted, reduces Consumer's Experience.
Currently, also occurring can be with the electrical equipment of automatic charging, its generally use following manner：Electrical equipment detects
During not enough power supply, electrical equipment voluntarily returns to cradle and charged, and it generally requires electrical equipment and reserves sufficient electricity, with
Meet that electrical equipment can successfully move to the position of cradle from current location.As an example, for example, electrical equipment battery
It is expected that stand-by time is 10h, the power source that is returned due to needing to reserve a part of electricity as electrical equipment, when its expection is standby
Between may taper to 8h.Due to reserving the presence of electricity, which further reduces the time that electrical equipment maintains normal work.
Meanwhile the mode that flight structure is integrated in electrical equipment may cause what the manufacture craft of electrical equipment became to answer
It is miscellaneous, add cost of manufacture.
The content of the invention
The purpose of this utility model is：Overcome the deficiencies in the prior art, there is provided one kind can allow electrical equipment not by electricity
The limitation of supply socket position, in electrical equipment not enough power supply, automatic Portable power equipment, which is gone to, carries out charging behaviour at charging equipment
The aircraft and charging system of the auxiliary charging of work.In this way, improving the automaticity of electrical equipment charging, user is improved
Experience.
To realize above-mentioned target, the utility model provides following technical scheme.
A kind of aircraft of auxiliary charging, including：Structure is captured, to fly in aircraft to electrical equipment situation
Under, electrical equipment is captured；Charge auxiliary unit, flies to carry electrical equipment in aircraft to charging equipment
In the case of, connect the charging circuit of electrical equipment.
Further, in addition to power unit, for providing the electric energy of aircraft work；Navigation elements, for obtaining electricity consumption
The positional information of equipment simultaneously generates flight path；Control unit, for controlling the flight parameter of flight structure；Information gathering list
Member, for receiving charge requirement that electrical equipment sends, flying away from desired signal.
Further, including electrical equipment location structure, for after the charge requirement information of electrical equipment is received, collection
The positional information of electrical equipment, and positional information is sent to control unit；Control unit is according to the positional information of acquisition, control
Aircraft flies the position to where electrical equipment.
Further, including electrical equipment size collecting unit, for flying in aircraft to the position where electrical equipment,
The dimension information of electrical equipment is gathered, and the crawl scope and angle of crawl structure are controlled according to the dimension information of acquisition.
Further, in addition to charging trigger element, for set triggering aircraft carry out flight operation trigger condition, and
Judge whether the trigger condition is met, and when meeting trigger condition, send charge requirement signal.
Further, the charge requirement signal includes the electricity being filled with required for electrical equipment；Aircraft obtains the electricity
After amount, the charging equipment of selection matching is required according to the electricity.
Further, the charging auxiliary unit includes interface docking structure, and the interface docking structure can set electricity consumption
Standby relative charging equipment fixed position, and the external charging inlet of charging equipment is connected with the charging connector of electrical equipment.
Further, including module is flown away from, for being powered off after electrical equipment detects charging complete, and is sent to aircraft
The control signal triggering aircraft Portable power equipment flown away from flies away from charging equipment；Or for after charging complete is detected,
Electrical equipment position is voluntarily gone to, Portable power equipment flies away from charging equipment.
Further, including landing identifying unit, for aircraft capture electrical equipment before gather electrical equipment position
Information and image information, determine whether to meet drop conditions after identification, and are judging that landing can cause itself and/or his thing
It is judged to not meeting drop conditions during injury, no longer landing and feedback message is to electrical equipment.
Further, in addition to alarm unit, for taking off, fly, surrounding enviroment information, and root being gathered in descent
According to default flight environment of vehicle standard, surrounding enviroment are judged if appropriate for flight, if being not suitable for, are maked a return voyage or break-off.
The utility model additionally provides a kind of charging system, including：It is provided with flight structure and captures the aircraft of structure；
For the charging equipment to be charged to electrical equipment；The aircraft can fly to electrical equipment position according to the demand of electrical equipment
Put and electrical equipment is captured, Portable power equipment flies to charging equipment position or leaves charging equipment position, to electricity consumption
Equipment carries out charging operations or returns to operation.
Further, the electrical equipment is computing terminal equipment.
Further, wireless mode is provided with charging equipment and sends electric energy so as to the charging to electrical equipment charging
Induction structure.
Further, the electrical equipment is provided with electricity determination module, judges electrical equipment by electricity determination module
Electricity it is whether enough；In the case of judgement is inadequate, charge requirement signal is sent, triggers aircraft flight.
Further, the electricity determination module can also in the information that the electricity for collecting electrical equipment has been filled with, to
Aircraft, which is sent, flies away from signal.
Further, electricity output metering module is provided with charging equipment, the electricity exports metering module to visit
When measuring electricity can not export to electrical equipment again, and sent to aircraft and fly away from signal.
The utility model is due to using above technical scheme, compared with prior art, has the following advantages that and actively imitates
Fruit：1) the utility model is utilized, in the case of electrical equipment not enough power supply, aircraft flies in a manner of flying to electrical equipment
Place, and electrical equipment is captured, then aircraft Portable power equipment flies to charging equipment, and electrical equipment is filled
Electrically operated, the charging of electrical equipment is no longer limited by factors such as power supply source interface position, conductor lengths.2) when needing charging,
Electrical equipment is connected with charging equipment without user's manual operation, when charging finishes, without manual operation so that charging is set
It is standby to be disconnected between electrical equipment.The automaticity of electrical equipment charging is improved, improves charge efficiency and user
Experience.
Brief description of the drawings
Fig. 1 is the flow chart for the charging method that the utility model embodiment provides.
Fig. 2 is the aircraft that the utility model embodiment provides and the structural representation of electrical equipment.
Fig. 3 is the structural representation that the aircraft that the utility model embodiment provides captures electrical equipment.
Fig. 4 is the structural representation for the charging equipment that the utility model embodiment provides.
In Fig. 5, Fig. 5 A, Fig. 5 B are operating diagram when being charged to electrical equipment that the utility model embodiment provides.
Fig. 6 is the construction module figure of the aircraft for the auxiliary charging that the utility model embodiment provides.
Label is as follows in figure：
Electrical equipment 100, screen 110, charge requirement shows 111；
Aircraft 200, flight structure 210, structure 220 is captured, charge auxiliary unit 230, power unit 240, and navigation is single
Member 250, control unit 260, information acquisition unit 270, alarm unit 280；
Interface docking structure 231；
Charging equipment 300, charge induction structure 310, charging equipment power connecting plug 320, external charging inlet 330.
Embodiment
Aircraft and charging system below in conjunction with the drawings and specific embodiments to auxiliary charging provided by the utility model
It is described in further detail.It should be noted that the combination of technical characteristic or technical characteristic described in following embodiments is not
Should be considered as isolated, they can be mutually combined so as to reach superior technique effect.In the attached of following embodiments
In figure, the identical label that each accompanying drawing occurs represents identical feature or part, can be applied in different embodiments.
It should be noted that structure, ratio, size depicted in this specification institute accompanying drawings etc., only coordinating explanation
Content disclosed in book, so that those skilled in the art understands and reads, it 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(that does not influence utility model and can be generated
Under effect and the purpose that can reach, it all should fall in the range of the technology contents disclosed in utility model can 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.
Embodiment
It is shown in Figure 1, a kind of charging method, comprise the following steps.
S100, the aircraft with flight structure fly to electrical equipment position and electrical equipment are captured.
The flight structure of aircraft can include flying wing and flight dynamic devices.The flying wing of flight structure, Ke Yishi
One or more in rotor structure, fixed wing structure, umbrella wing structure, jet-propelled structure, flapping wing structure.Flight dynamic devices can
Using piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching type or jet-propelled, in the present embodiment, flight dynamic devices
Preferably by electrodynamic type engine.The power source of motor, it is unrestricted as an example such as carry-on to be arranged on
Battery, battery and motor are electrically connected by wire.
The crawl structure for capturing electrical equipment is provided with aircraft.Described crawl, refer to consolidate electrical equipment
Determine on board the aircraft, in order to which aircraft Portable power equipment is flown.
The crawl structure, can be suspension hook or sucker.When using sucker, the sucker is preferably inhaled using electromagnetism
Disk, the electric supply installation of the magnechuck can respond the control of aircraft.
Described crawl structure, can also be claw structure.During implementation, the claw structure includes at least one set of clamping jaw,
Each group of clamping jaw includes two clamping jaws.Preferably, claw structure includes clamping jaw and jig arm, the clamping jaw can be moved in jig arm with
The distance between clamping jaw is adjusted, various sizes of electrical equipment is adapted to this.
Electrical equipment, can be computing terminal equipment in the present embodiment.Preferably, it is mobile computing terminal, such as respectively
The wireless vehicle mounted terminal of kind, wireless handheld terminal.It is unrestricted as an example, for example, mobile phone, tablet personal computer, Portable hand electricity
Brain, unmanned plane, intelligent watch etc..
Aircraft is flying to before electrical equipment, the step of can also including Aerial vehicle position electrical equipment.
It the mode of Aerial vehicle position electrical equipment, can be that aircraft flies in the air, by scanning surrounding environment, find
Need the electrical equipment to charge.During using this mode, it is preferred that recognition unit is set on board the aircraft, identified after gathering information
Positioned after electrical equipment.
The recognition unit, can be by gathering image information and/or where audio-frequency information identifies and judge electrical equipment
Position.It is unrestricted as an example, the structure of the collection image information can be installed in carry-on camera device,
The structure of the collection audio-frequency information can be the image for gathering aircraft periphery with this installed in carry-on microphone
And/or acoustic information, and then electrical equipment is identified, and further obtain the positional information of electrical equipment.
The method for identifying electrical equipment, also can be by wireless location side in addition to collection image information and/or audio-frequency information
Formula.It is unrestricted as an example, for example wireless positioning unit can be set on board the aircraft, it is corresponding, set in the electrical equipment
Wireless signal Transmit-Receive Unit is equipped with, the signal of the wireless positioning unit collection wireless messages Transmit-Receive Unit, identifies and judges to use
The position of electric equipment.Location technology common at present mainly has PPD location technologies, gps satellite positioning, bluetooth positioning, WIFI nets
Network positioning, Big Dipper positioning, the positioning of GPRS/CDMA mobile communication technologies etc..Mobile terminal positioning technology is based on currently used
Exemplified by, the principle of the location technology is：The Base Transmitter signal of multiple known locations, institute's transmission signal carries and base station location
Relevant characteristic information, after mobile terminal receives these signals, its geometry site between each base station is determined, and
Positioning estimation is carried out to its own position according to related algorithm, so as to obtain the positional information of itself.
The mode of Aerial vehicle position electrical equipment, it is also possible that user sets the position specified to believe in aircraft in advance
Breath.The position specified, is the position that user generally places electrical equipment, and the aircraft is according to the positional information, i.e.,
The electrical equipment for being placed on specified location can be positioned.
The mode of Aerial vehicle position electrical equipment, it is also possible that aircraft flies to electrical equipment position, collection electricity consumption is set
Standby charge requirement signal.After the aircraft receives the charge requirement information of electrical equipment, the position of electrical equipment is gathered
Information, fly the position to where electrical equipment according to the positional information of acquisition.Preferably, the electrical equipment is correspond to, is set
Have to trigger the trigger condition that aircraft carries out flight operation；Judge whether the trigger condition is met, meet triggering bar
During part, the agent equipment that is associated by the electrical equipment to foregoing aircraft or with the flight trigger action of foregoing aircraft, hair
Go out charge requirement signal.Unrestricted as an example, the charge requirement signal is filled with required for comprising at least electrical equipment
Electricity, after obtaining the electricity, required according to the electricity, aircraft can select the charging equipment of matching.Under this mode, one
Aircraft can be associated with multiple charging equipments, it is necessary to when, corresponding charging equipment administrative unit is set on board the aircraft, it is described
Charging equipment administrative unit can obtain the letter such as the numbering of each charging equipment, positional information, information about power, work/idle state
Breath, consequently facilitating aircraft selects suitable charging equipment according to the needs of electrical equipment.
Described trigger condition, it is unrestricted as an example, for example whether can be the electricity of electrical equipment less than default
Threshold value.Now, it is preferred that electricity determination module can be set in the electrical equipment, pass through the electricity determination module
To judge whether the electricity of electrical equipment is enough；In the case where judging that not enough power supply is enough, (i.e. electricity is less than default threshold value
In the case of), meet trigger condition, the agent equipment associated to foregoing aircraft or with the charging trigger action of foregoing aircraft
Send charge requirement signal.In the present embodiment, state and normal work when electrical equipment can also send to charge requirement signal
State when making makes a distinction, and can be identified in order to aircraft, user understands electrical equipment state.
The aircraft of the present embodiment, electrical equipment information unit can also be included, after user orders charging service, flight
Device can obtain the identification information of the electrical equipment of the user.Electrical equipment information unit obtains the side of the identification information of electrical equipment
Formula, it is unrestricted as an example, by taking mobile phone as an example, such as after user's order charging service, you can the model of user mobile phone is believed
Breath, handset identity code information, the positional information of mobile phone etc. are transferred to the electrical equipment information unit of aircraft, in this way, aircraft
Obtain the identification information of the electrical equipment of the user.
Aircraft flies to the position where electrical equipment to be charged using flight structure thereon, passes through aircraft
On crawl structure electrical equipment is captured.
Preferably, the aircraft flies to the position where electrical equipment, gathers the dimension information of electrical equipment, according to
The crawl scope and angle of the dimension information control crawl structure of acquisition.
It is shown in Figure 2, illustrate aircraft and fly to electrical equipment position, and prepare the knot captured to electrical equipment
Structure schematic diagram.Electrical equipment 100 is mobile phone, and crawl structure 220 uses a pair of clamping jaws and jig arm.
When electrical equipment (mobile phone) 100 sends charge requirement signal, show that charge requirement shows on its display screen 110
Show the symbol of 111, such as battery.Aforesaid way is unrestricted as an example, can also use other modes such as light
One or more modes in flicker, screen in the mode such as text prompt, vibration or audio broadcasting.
After aircraft receives the charge requirement signal of electrical equipment, the positional information of electrical equipment is gathered, according to acquisition
Positional information fly position to where electrical equipment.The present embodiment China, it is contemplated that the security of landing, captured in aircraft
Before electrical equipment, the positional information and image information of electrical equipment are gathered, determines whether to meet drop conditions after identification, when sentencing
Fixed landing can cause to be judged to not meeting drop conditions when itself and/or his thing injury, no longer landing and feedback message to electricity consumption
Equipment.
If meeting drop conditions, aircraft landing captures to electrical equipment.With continued reference to shown in Fig. 2.Aircraft 200
Including flight structure 210 and crawl structure 220.A pair of clamping jaws of crawl structure 220 are symmetricly set on the both ends of jig arm, jig arm bag
Outer bar and two interior bars are included, nesting is arranged on outer bar both ends respectively for one end of two interior bars, and interior bar can be withdrawn and stretch with respect to outer bar
Go out.The other end of two interior bars connects clamping jaw respectively.During crawl, adjusted by adjusting the flexible of interior bar between two clamping jaws
Distance, Fig. 3 illustrate the structural representation of aircraft crawl electrical equipment.
The jig arm by contractable element install on board the aircraft, can by the contractable element adjust jig arm with
The distance between aircraft so that crawl structure is remote or close to the aircraft.Using said structure, aircraft can basis
Electrical equipment to be captured is stretched with capturing the distance between structure, barrier, regulation crawl structure, avoids barrier infringement from flying
Row device and/or aircraft infringement barrier.
S200, aircraft Portable power equipment fly to charging equipment, and charging operations are carried out to electrical equipment.
After aircraft crawl electrical equipment, Portable power equipment flies to charging equipment, and connection charging equipment is set with electricity consumption
It is standby, so as to realize the charging to electrical equipment.
Charging equipment exports the mode of electric energy, can be wireless charging or wired charging.
Wireless charging technology (Wireless charging technology), comes from wireless power transmission technology, at present
Compare the wireless charging technology of main flow mainly by three kinds of modes once in market：Electromagnetic induction, radio wave, resonant interaction.It is right
Charged in low-power wireless, generally use is induction；Charged for high-power wireless, generally use resonant mode is set by powering
Standby (charger) transmits its energy to the device of electricity consumption, and the device is charged using the energy received to battery, and supplies it simultaneously
Running itself is used.
When exporting electric energy using wireless mode, it is preferred that on the flight structure of described aircraft and/or storing up electricity structure
It is provided with wireless mode and sends electric energy so as to the charging induction structure to electrical equipment charging.The charging induction structure can
Electric energy is exported wirelessly, and electrical equipment is charged, such as magnetic induction way, microwave induced mode etc..
When exporting electric energy using wired mode, it is preferred that set on the flight structure of the aircraft and/or storing up electricity structure
It is equipped with the external charging inlet to be charged to electrical equipment.In the present embodiment, using can wireless charging can have again
The charging equipment of micro USB electricity.
The structural representation of charging equipment shown in Figure 4.Charging equipment 300, including charging induction structure 310, fill
Electric equipment power connecting plug 320, and externally charging inlet 330.
Charging equipment power connecting plug 320 be used for by charging equipment and power network or can power supply unit be connected, described company
Connect, including be directly connected to and be indirectly connected with.It is unrestricted as an example such as straight by charging equipment power connecting plug 320
Power outlet is connect in succession.
Charge induction structure 310 can be wirelessly --- such as magnetic induction way, microwave induced mode --- to
Electrical equipment exports electric energy, so as to be charged to electrical equipment.During operation, after electrical equipment is placed on charging equipment, you can
Start charging process.Fig. 5 is operating diagram when being charged to electrical equipment that the utility model embodiment provides.Fig. 5 A are
After electrical equipment is placed on charging equipment, the aircraft 200 of crawl structure has been withdrawn, now, has captured the clamping jaw of structure 220
Withdrawn with respect to jig arm, crawl structure 220 is withdrawn also by the contraction relative flight device body of jig arm.
Charging connector of the external charging inlet 330 for connecting electrical equipment, external charging inlet and electrical equipment are filled
Charging circuit can be connected after electric connection connection.In the present embodiment, acquisition electricity consumption is also provided with the charging equipment and is set
The interface position unit of standby charging connector positional information.The position of the charging connector of electrical equipment is obtained in interface position unit
After information, then the interface docking structure by being set on aircraft or charging equipment, realize the external charging inlet of charging equipment with
The connection of electrical equipment charging connector.
The interface docking structure, it can set on board the aircraft, can also be arranged on charging equipment.The interface pair
Binding structure can connect the charging of external charging inlet and electrical equipment by electrical equipment with respect to behind charging equipment fixed position
Head.Unrestricted as an example, the interface docking structure includes electrical equipment fixed structure and charging inlet embedded structure.
The electrical equipment fixed structure, for electrical equipment to be fixed on into charging equipment.It is unrestricted as an example,
For example it is sucker or fixed claw.
The charging inlet embedded structure, for connecting external charging inlet and the charging of electrical equipment of charging equipment
Head.It is unrestricted as an example, for example be the contractable element or foldable member on external charging inlet, external
Behind charging inlet alignment charging connector position, contractable element or foldable member elongation is controlled to fill charging inlet insertion
Connection is realized in electric connection.
After the aircraft collects the message that finishes of charging, after the connection for disconnecting electrical equipment and charging equipment, to
Electric equipment is captured, and Portable power equipment is back to initial position or other specified locations.
In another embodiment, it is additionally provided with the process of detection charge condition.It is unrestricted as an example, such as in electricity consumption
Electricity determination module is provided with equipment, when the electricity determination module collects the information that the electricity of electrical equipment has been filled with
When, sent to aircraft and fly away from signal.Or electricity output metering module is provided with charging equipment, when the electricity is defeated
When going out metering module and detecting electricity and can not be exported again to electrical equipment, charging equipment stops charging, sends and flies away to aircraft
Signal.
After electrical equipment electricity is full of, aircraft can obtain and fly away from signal.It is unrestricted as an example, such as electricity consumption
After equipment detects charging complete, power off and the control signal flown away from is sent to aircraft, trigger aircraft Portable power equipment
Charging equipment is flown away from, returns to initial position or other default specified locations.Or after aircraft detects charging complete, from
Row goes to electrical equipment position, and Portable power equipment flies away from charging equipment, returns to initial position or other are default specified
Position.
It is unrestricted as an example when charging process is interrupted, it can be adjusted one of in the following way.
Mode one, charging equipment send the signal of charging process termination to aircraft, and aircraft crawl electrical equipment returns
Initial position finds other charging equipments.
Mode two, the information that aircraft automatic data collection is interrupted to charging --- it is unrestricted as an example, for example pass through knowledge
The dispaly state of other electrical equipment --- rear to start the process (Portable power equipment flies away from charging equipment) that flies away from, aircraft crawl is used
Electric equipment returns to initial position or finds other charging equipments.
In view of the security during aircraft flight, electrical equipment or other objects, medium pair in-flight are prevented
Aircraft causes to damage, and/or aircraft damages to other objects, can set alarm unit on board the aircraft.It is described
Alarm unit is used to take off, fly, gather surrounding enviroment information in descent, and according to default flight environment of vehicle standard,
Surrounding enviroment are judged if appropriate for flight, if being not suitable for, control aircraft makes a return voyage or break-off.It is unrestricted as an example,
For example the visibility criterion value of environment can be preset, or wind-force standard value, do not reached when the visibility for collecting current environment is small
During to standard value, or during the excessive inaptitude for flying of wind-force, make a return voyage or groung.
Fig. 6 is the construction module figure of the aircraft of auxiliary charging provided by the utility model.
A kind of aircraft 200 of auxiliary charging, including flight structure 210, structure 220 is captured, charge auxiliary unit 230,
Power unit 240, navigation elements 250, control unit 260, information acquisition unit 270, alarm unit 280.
Flight structure 210, flight structure can include flying wing and flight dynamic devices.The flying wing of flight structure, can
With the one or more for being rotor structure, fixing in wing structure, umbrella wing structure, jet-propelled structure, flapping wing structure.Flying power fills
Piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching type or jet-propelled, in the present embodiment, flying power can be used by putting
Device uses electrodynamic type engine.
Structure 220 is captured to fly in aircraft to electrical equipment situation, electrical equipment is captured, as
It is for example and not limitation, in the present embodiment, the structures such as suspension hook, sucker, clamping jaw can be used.
Charge auxiliary unit 230, to be carry in aircraft in the case that electrical equipment flies to charging equipment, connection
The charging circuit of electrical equipment.In the present embodiment, charging auxiliary unit comprises at least interface docking structure 231, the interface pair
Binding structure 231 can be by electrical equipment with respect to the external charging inlet and use for behind charging equipment fixed position, connecting charging equipment
The charging connector of electric equipment.
Power unit 240, the main electric energy that aircraft work is provided.During implementation, power unit can use charging type electric
Power supply module or power generating type supply of electric power module.
Navigation elements 250, for obtaining the positional information of electrical equipment and generating flight path.
Control unit 260, for controlling the flight parameter of aircraft.Charging process can be further controlled when needing；And
The process, Portable power equipment that Portable power equipment is flown away from after charging can be also further controlled to return to initial position or default specified
The process of position.
Information acquisition unit 270, for receiving charge requirement that electrical equipment sends, flying away from desired signal.
Alarm unit 280, for take off, fly and/or descent in gather surrounding enviroment information, and according to default
Flight environment of vehicle standard, judge that surrounding enviroment if appropriate for flight, if being not suitable for, are maked a return voyage or break-off.
The aircraft can also include electrical equipment location structure, for believing in the charge requirement for receiving electrical equipment
After breath, the positional information of electrical equipment is gathered, and positional information is sent to control unit；Control unit is according to the position of acquisition
Information, control aircraft fly the position to where electrical equipment.Electrical equipment size collecting unit, for flying in aircraft to using
Behind position where electric equipment, the dimension information of electrical equipment is gathered, and crawl structure is controlled according to the dimension information of acquisition
Capture scope and angle.
The aircraft can also charge trigger element, for setting triggering aircraft to carry out the triggering bar of flight operation
Part, and judge whether the trigger condition is met, and when meeting trigger condition, send charge requirement signal.It is described to fill
Electric desired signal includes the electricity being filled with required for electrical equipment；After aircraft obtains the electricity, require to select according to the electricity
Select the charging equipment of matching.
The charging auxiliary unit includes interface docking structure, and the interface docking structure can fill electrical equipment relatively
Electric equipment fixed position, and the external charging inlet of charging equipment is connected with the charging connector of electrical equipment.
The aircraft can also include flying away from module, for being powered off after electrical equipment detects charging complete, and to
Aircraft sends the control signal triggering aircraft Portable power equipment flown away from and flies away from charging equipment；Or for detecting
After charging complete, electrical equipment position is voluntarily gone to, Portable power equipment flies away from charging equipment.
The aircraft can also include landing identifying unit, be set for gathering electricity consumption before aircraft captures electrical equipment
Standby positional information and image information, determine whether to meet drop conditions after identification, and itself can be caused in judgement landing
And/or it is judged to not meeting drop conditions during the injury of his thing, no longer landing and feedback message to electrical equipment.
The aircraft can also also include alarm unit, for taking off, fly, surrounding enviroment being gathered in descent
Information, and according to default flight environment of vehicle standard, judge surrounding enviroment if appropriate for flight, if being not suitable for, make a return voyage or suspend work
Make.
Another embodiment, there is provided a kind of charging system, including：It is provided with flight structure and captures the aircraft of structure；
For the charging equipment to be charged to electrical equipment；The aircraft can fly to electrical equipment position according to the demand of electrical equipment
Put and electrical equipment is captured, Portable power equipment flies to charging equipment position or leaves charging equipment position, to electricity consumption
Equipment carries out charging operations or returns to operation.
In the present embodiment, the electrical equipment is computing terminal equipment.
The electrical equipment is provided with electricity determination module, is to judge the electricity of electrical equipment by electricity determination module
It is no enough；In the case of judgement is inadequate, charge requirement signal is sent, triggers aircraft flight.The electricity determination module
It can also be sent to aircraft at the information that the electricity for collecting electrical equipment has been filled with and fly away from signal.
Wireless mode is provided with charging equipment and sends electric energy so as to the charging induced junction to electrical equipment charging
Structure.
Preferably, electricity determination module is provided with electrical equipment, electricity output metering module is provided with charging equipment,
Electricity output metering module is sent to aircraft and flown away to when detecting electricity and can not be exported again to electrical equipment
Signal.
In the present embodiment, the structure of aircraft, charging equipment in charging system, it can combine what is set in preceding method
Each functional unit carries out selective combination, further to optimize the charging process to electrical equipment, will not be repeated here.
Foregoing description is only the description to the utility model preferred embodiment, not to any limit of the scope of the utility model
Fixed, the scope of preferred embodiment of the present utility model includes other realization, wherein can not press shown or discuss suitable
Sequence carrys out perform function.Any change, the 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 (16)
- A kind of 1. aircraft of auxiliary charging, it is characterised in that including：Structure is captured, to fly in aircraft to electrical equipment situation, electrical equipment is captured；Charged auxiliary unit, and to be carry in aircraft in the case that electrical equipment flies to charging equipment, connection electricity consumption is set Standby charging circuit.
- 2. aircraft according to claim 1, it is characterised in that also include：Power unit, for providing the electric energy of aircraft work；Navigation elements, for obtaining the positional information of electrical equipment and generating flight path；Control unit, for controlling the flight parameter of flight structure；Information acquisition unit, for receiving charge requirement that electrical equipment sends, flying away from desired signal.
- 3. aircraft according to claim 1, it is characterised in that：Including electrical equipment location structure, for receiving After the charge requirement information of electrical equipment, the positional information of electrical equipment is gathered, and positional information is sent to control unit；Control Unit processed controls aircraft to fly the position to where electrical equipment according to the positional information of acquisition.
- 4. aircraft according to claim 3, it is characterised in that：Including electrical equipment size collecting unit, for flying Row device flies to the position where electrical equipment, gathers the dimension information of electrical equipment, and control according to the dimension information of acquisition Capture the crawl scope and angle of structure.
- 5. aircraft according to claim 1, it is characterised in that：Also include charging trigger element, for setting triggering to fly Row device carries out the trigger condition of flight operation, and judges whether the trigger condition is met, and when meeting trigger condition, Send charge requirement signal.
- 6. aircraft according to claim 5, it is characterised in that：The charge requirement signal is included required for electrical equipment The electricity being filled with；After aircraft obtains the electricity, the charging equipment of selection matching is required according to the electricity.
- 7. aircraft according to claim 1, it is characterised in that：The charging auxiliary unit includes interface docking structure, The interface docking structure can be by electrical equipment with respect to charging equipment fixed position, and by the external charging inlet of charging equipment Connected with the charging connector of electrical equipment.
- 8. aircraft according to claim 1, it is characterised in that：Including flying away from module, for being detected in electrical equipment Powered off after charging complete, and the control signal triggering aircraft Portable power equipment flown away from is sent to aircraft and flies away from charging and sets It is standby；Or for after charging complete is detected, voluntarily going to electrical equipment position, Portable power equipment flies away from charging Equipment.
- 9. aircraft according to claim 1, it is characterised in that：Including the identifying unit that lands, for being captured in aircraft The positional information and image information of electrical equipment are gathered before electrical equipment, determines whether to meet drop conditions after identification, and It is judged to not meeting drop conditions when judging that landing can cause itself and/or the injury of his thing, no longer landing and feedback message is extremely Electrical equipment.
- 10. aircraft according to claim 1, it is characterised in that：Also include alarm unit, for taking off, fly, dropping Surrounding enviroment information is gathered during falling, and according to default flight environment of vehicle standard, judges surrounding enviroment if appropriate for flight, if Be not suitable for, make a return voyage or break-off.
- A kind of 11. charging system, it is characterised in that including：It is provided with flight structure and captures the aircraft of structure；For the charging equipment to be charged to electrical equipment；The aircraft can fly to electrical equipment position according to the demand of electrical equipment and electrical equipment captured, take Band electrical equipment flies to charging equipment position or leaves charging equipment position, and charging operations are carried out to electrical equipment or are returned to grasp Make.
- 12. charging system according to claim 11, it is characterised in that：The electrical equipment is computing terminal equipment.
- 13. charging system according to claim 11, it is characterised in that：Wireless mode is provided with charging equipment Electric energy is sent, so as to the charging induction structure to electrical equipment charging.
- 14. charging system according to claim 11, it is characterised in that：The electrical equipment is provided with electricity and judges mould Block, the electricity determination module to judge whether the electricity of electrical equipment enough, and can judge it is inadequate in the case of, Charge requirement signal is sent, triggers aircraft flight.
- 15. charging system according to claim 14, it is characterised in that：The electricity determination module can also collect During the information that the electricity of electrical equipment has been filled with, sent to aircraft and fly away from signal.
- 16. charging system according to claim 11, it is characterised in that：Electricity output metering mould is provided with charging equipment Block, electricity output metering module are sent to aircraft to when detecting electricity and can not be exported again to electrical equipment Fly away from signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720103706.XU CN206775150U (en) | 2017-01-25 | 2017-01-25 | The aircraft and charging system of auxiliary charging |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720103706.XU CN206775150U (en) | 2017-01-25 | 2017-01-25 | The aircraft and charging system of auxiliary charging |
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| CN206775150U true CN206775150U (en) | 2017-12-19 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106602671A (en) * | 2017-01-25 | 2017-04-26 | 上海量明科技发展有限公司 | Charging method, aircraft of auxiliary charging and charging system |
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2017
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106602671A (en) * | 2017-01-25 | 2017-04-26 | 上海量明科技发展有限公司 | Charging method, aircraft of auxiliary charging and charging system |
| CN106602671B (en) * | 2017-01-25 | 2024-02-20 | 上海量明科技发展有限公司 | Charging method, auxiliary charging aircraft and charging system |
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