CN105634083A - Wireless charging aircraft - Google Patents

Wireless charging aircraft Download PDF

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Publication number
CN105634083A
CN105634083A CN201410587672.7A CN201410587672A CN105634083A CN 105634083 A CN105634083 A CN 105634083A CN 201410587672 A CN201410587672 A CN 201410587672A CN 105634083 A CN105634083 A CN 105634083A
Authority
CN
China
Prior art keywords
aircraft
charging
wireless charging
earth station
aerocraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201410587672.7A
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Chinese (zh)
Inventor
吴贤城
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201410587672.7A priority Critical patent/CN105634083A/en
Publication of CN105634083A publication Critical patent/CN105634083A/en
Pending legal-status Critical Current

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Abstract

The present invention relates to the field of a smart aircraft, and especially designs a smart aircraft system capable of automatic charging through the wireless charging technology and the method thereof. According to the invention, the automatic charging of an aircraft is realized through combination of software and hardware. The aircraft on the basis of wireless charging comprises a ground station; an aircraft and a control system; the ground station is provided with a wireless charging emission system; the aircraft carries a wireless charging receiving system; and the control system is configured to perform electric quantity monitoring, task execution and flight return charging of the aircraft.

Description

Wireless charging aircraft
Technical field
The present invention relates to Intelligent flight device field, especially design a kind of Intelligent flight device system and method thereof being realized automatic charging by wireless charging technology.
Background technology
At present, adopt battery as the aircraft of the energy due to battery energy storage limited ability so that the continuation of the journey ability to work of aircraft is restricted. Aircraft performing after task a period of time, makes a return voyage back replaced on ground battery owing to battery power exhausts needs, and this process also tends to need artificial assistance to complete, such as plug battery etc. This cruising time causing aircraft and execution task are very limited, simultaneously need to substantial amounts of manual intervention, use cost is high.
Summary of the invention
For this problem overcoming existing aircraft to exist, the present invention tangible aircraft automatic charging of method by software and hardware combining. Software system obtains power information by monitoring power sensor, and judge whether that needs make a return voyage charging according to the state of power supply and the current situation performing task, if desired for making a return voyage, charging is then obtained the place of charging of making a return voyage and preengages charging by earth station, controls aircraft further and makes a return voyage charging; Charging process obtains power information by power sensor, and combined ground station performs task situation with aircraft and judged whether charging, leaves earth station and continue executing with task after charging complete. Hardware system comprises power supply, power sensor, aircraft wireless charging receiver and earth station's energy discharger.
It is an object of the invention to provide a kind of aircraft based on wireless charging technology, applying this technical scheme can so that Intelligent flight device possesses automatic power supplementary functions, it is not necessary to manual intervention, reduces cost of labor and improves convenience.
The technical scheme that the present invention is complete is: a kind of aerocraft system based on wireless charging, it includes earth station, aircraft and control system, earth station has wireless charging emission system, aircraft carries wireless charging and receives system, and control system is responsible for the electric quantity monitoring of aircraft, execution task and charging of making a return voyage.
The aircraft of execution task obtains battery information by power sensor, and control system is according to the state computation of battery and judges whether earth station's charging of making a return voyage.
Aircraft both can by earth station's wireless charging in the way of stop, it is also possible to obtain power supply in the way of hovering.
Aircraft changes battery without plug can complete charging, connects without cable during charging.
During charging, aircraft obtains battery information by power sensor, and control system calculates according to battery information and aircraft task situation and judged whether charging and continued executing with task.
Wireless charging transmits energy by electromagnetic wave and microwave. Wireless charging includes the wireless charging technology such as electromagnetic induction, electromagentic resonance and radio wave.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the program flow diagram of the present invention;
Fig. 2 is the overall structure framework of the present invention;
Fig. 3 is the aircraft automatic charging system front view of the present invention;
Fig. 4 is the aircraft automatic charging system lateral plan of the present invention;
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments. Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
Embodiment 1:
As shown in Figure 1, after flight control obtains power information and earth station's information by power sensor, in conjunction with the current situation performing task, calculated by microprocessor and be charged the need of earth station of making a return voyage, if without charging, continue executing with task and continue to be monitored power supply status determining the need for charging of making a return voyage after being interrupted 10 seconds; If needing to charge, aircraft performs to make a return voyage, and holds consultation with earth station, performs wireless charging operation after having consulted; Namely charging process reacquires power sensor information and earth station's information at interval of a period of time, complete charge is decided whether, if without terminating, continuing charging and persistently power supply and earth station's information be monitored in conjunction with the current situation performing task; If needing to terminate, leaving earth station, whether completing to perform next step operation according to task.
It is illustrated in figure 2 the total system framework of the present invention. Mainly comprise two big hardware system, respectively aircraft and earth station's two parts, be responsible for the execution of software system by the microprocessor of carry-on microprocessor Yu earth station simultaneously and control whole automatic charging process. Carry-on power sensor obtains the information of energy-storage system in real time and transfers data to microprocessor and carry out computing and judgement, is charged according to the result the judged earth station that decides whether to make a return voyage. Wireless charging module comprises wireless charging receiver and the two-part hardware of wireless charging discharger, the middle transmission being realized energy by electromagnetic wave and microwave.
As it is shown on figure 3, aircraft module 301 comprises microprocessor, power supply, power sensor module and wireless charging receiver, for the ease of aircraft flight and charging, each correlation module is packaged in shell 301; Ground station module 302 comprises wireless charging discharger and position sensor, in order to attractive in appearance and be easy to charging, each correlation module is packaged in shell 302. When adopting the modes such as electromagentic resonance, microwave or radio frequency to realize energy field transmitting when wireless charging discharger, corresponding also has antenna as energy emitting device. When wireless charging discharger adopts electromagnetic induction technology, discharger is realized by coil generating electromagnetic field.
In order to realize goal of the invention, the present embodiment provides a kind of wireless charging method based on electromagnetic induction, the steps include:
Input electric energy is to earth station;
Earth station converts electrical energy into electromagnetic field by coil;
Energy is propagated surrounding space by electromagnetic field by wireless charging discharger;
The wireless charging receiver of aircraft catches the energy of electromagnetic field transmission by coil;
Wireless charging receiver is by energy savings to battery.
Device embodiment described above is merely schematic, the wherein said unit illustrated as separating component can be or may not be physically separate, the parts shown as unit can be or may not be physical location, namely may be located at a place, or can also be distributed on multiple NE. Some or all of module therein can be selected according to the actual needs to realize the purpose of the present embodiment scheme. Those of ordinary skill in the art, when not paying performing creative labour, are namely appreciated that and implement.
Through the above description of the embodiments, those skilled in the art is it can be understood that can add the mode of required general hardware platform by software to each embodiment and realize, naturally it is also possible to pass through hardware. Based on such understanding, the part that prior art is contributed by technique scheme substantially in other words can embody with the form of software product, this computer software product can store in a computer-readable storage medium, such as ROM/RAM, magnetic disc, CD etc., including some instructions with so that a computer equipment (can be personal computer, server, or the network equipment etc.) perform the method described in some part of each embodiment or embodiment.
Embodiments described above, is not intended that the restriction to this technical scheme protection domain. The amendment made within any spirit at above-mentioned embodiment and principle, equivalent replacement and improvement etc., should be included within the protection domain of this technical scheme.

Claims (10)

1. being automatically replenished an aircraft for the energy, aircraft carries wireless energy and receives system, it is characterized in that: aircraft is without the artificial supplementation energy, either directly through earth station's wireless receiving energy and continue executing with task.
2. aerocraft system according to claim 1, is characterized in that: be made up of earth station, aircraft and control system.
3. aerocraft system according to claim 1, is characterized in that: earth station has wireless charging emission system, and flying instrument has wireless charging to receive system.
4. aerocraft system according to claim 1, is characterized in that: automatic charging system carries out electric quantity monitoring, execution task and charging of making a return voyage by microprocessor control system.
5. aerocraft system according to claim 1, is characterized in that: the aircraft performing task obtains battery information by power sensor, and control system is charged according to the state computation of battery judging whether earth station of making a return voyage.
6. aerocraft system according to claim 1, is characterized in that: aircraft both can by earth station's wireless charging in the way of stop, it is also possible to obtain power supply in the way of hovering.
7. aerocraft system according to claim 1, is characterized in that: aircraft changes battery without plug can complete charging, connects without cable during charging.
8. aerocraft system according to claim 1, is characterized in that: during charging, aircraft obtains battery information by power sensor, and control system calculates according to battery information and aircraft task situation and judged whether charging and continued executing with task.
9. aerocraft system according to claim 1, is characterized in that: system comprises wireless charging module.
10. aerocraft system according to claim 1, is characterized in that: wireless charging includes the wireless charging technology such as electromagnetic induction, electromagentic resonance and radio wave.
CN201410587672.7A 2014-10-29 2014-10-29 Wireless charging aircraft Pending CN105634083A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410587672.7A CN105634083A (en) 2014-10-29 2014-10-29 Wireless charging aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410587672.7A CN105634083A (en) 2014-10-29 2014-10-29 Wireless charging aircraft

Publications (1)

Publication Number Publication Date
CN105634083A true CN105634083A (en) 2016-06-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410587672.7A Pending CN105634083A (en) 2014-10-29 2014-10-29 Wireless charging aircraft

Country Status (1)

Country Link
CN (1) CN105634083A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018048627A1 (en) * 2016-09-09 2018-03-15 Wal-Mart Stores, Inc. Solar rechargeable unmanned vehicle systems and methods to monitor a geographic area

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018048627A1 (en) * 2016-09-09 2018-03-15 Wal-Mart Stores, Inc. Solar rechargeable unmanned vehicle systems and methods to monitor a geographic area
US20180075760A1 (en) * 2016-09-09 2018-03-15 Wal-Mart Stores, Inc. Solar rechargeable unmanned vehicle systems and methods to monitor a geographic area
GB2568003A (en) * 2016-09-09 2019-05-01 Walmart Apollo Llc Solar rechargeable unmanned vehicle systems and methods to monitor a geographic area

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160601

WD01 Invention patent application deemed withdrawn after publication