CN205646955U - Unmanned aerial vehicle wireless charging device - Google Patents

Unmanned aerial vehicle wireless charging device Download PDF

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Publication number
CN205646955U
CN205646955U CN201620233423.2U CN201620233423U CN205646955U CN 205646955 U CN205646955 U CN 205646955U CN 201620233423 U CN201620233423 U CN 201620233423U CN 205646955 U CN205646955 U CN 205646955U
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CN
China
Prior art keywords
charging
aerial vehicle
circuit
unmanned aerial
current
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CN201620233423.2U
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Chinese (zh)
Inventor
张志强
杨伯阳
唐荣宽
李闯
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.)
Guangdong hi tech Development Co., Ltd.
Beijing Information Science and Technology University
Original Assignee
Shenzhen Chuangyi Ruixiang Sky Technology Co Ltd
Beijing Information Science and Technology University
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Priority to CN201620233423.2U priority Critical patent/CN205646955U/en
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Publication of CN205646955U publication Critical patent/CN205646955U/en
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Abstract

The utility model provides an unmanned aerial vehicle wireless charging device, including the charging device who locates the platform that charges to and locate the current -collecting device on the unmanned aerial vehicle, charging device is including the oscillation circuit, amplifier circuit, boost circuit and the charging electrode that connect gradually, the current -collecting device receives electrode, reduction voltage circuit, rectifier circuit and unmanned aerial vehicle battery including what connect gradually. By last, can realize quick wireless the charging to unmanned aerial vehicle. The induction electric field that the utilization produced through following the two sets of asymmetric dipoles of vertical direction coupling transmits electric power, and its advantage lies in being fit for the short distance and charges, and conversion efficiency is higher, and it is lower to generate heat.

Description

Unmanned plane wireless charging device
Technical field
This utility model relates to unmanned aerial vehicle (UAV) control technical field, wireless particularly to a kind of unmanned plane Charging device.
Background technology
The commonly used wired charging technique of unmanned plane is charged.For SUAV, Wired charging has energy conversion and disposably obtains, and energy loss is little, energy-conserving and environment-protective, high in nothing Frequently electromagnetic radiation, equipment and technology content is low, and economic input is little, feature easy to maintenance.With Time to have the range of accommodation of electrical power wider, be suitable for the electric power storage of multiple different voltage and current grades The advantages such as pond energy storage supply.
But wired charging there is also simultaneously equipment move carrying inconvenience and power supply lead wire long Problem, manual operation is loaded down with trivial details.Charger operationally floor space is excessive, in manual operation During, the shortcoming such as excessive wear and insecurity factor that equipment easily occurs.
Existing wireless charging includes following several types:
1, induction charging: electric current passes through coil, coil produces magnetic field, to neighbouring line Circle produces induction electromotive force, thus produces electric current.Primary coil passes to the alternating current of certain frequency, Certain electric current can be produced by electromagnetic induction at secondary coil, thus energy is turned from transmission ends Move on to receiving terminal.
It, disadvantageously, specific putting position, could accurately charge: being electrically charged product must put Near charger, current effective propagation path is about 10cm;Secondary in end product Must shield between coil and circuit;Metal sensing contact can be generated heat: charger must have Standby otherwise can transmit energy to the most any metal product to being electrically charged the ability that product is identified Amount, causes heating, thus produces danger.
2, radio waves charging: environmental electromagnetic wave is converted to electric current, passes through circuit transmission Electric current.Mainly being made up of microwave launcher and microwave receiving device, receiving circuit can catch To the radio wave energy rebounded from wall, then with load adjust while keep stable DC voltage.
It is disadvantageously, charging interval length (through-put power is low): cannot complete at short notice Charging tasks;Conversion efficiency is relatively low: a large amount of power that emitter sends are with the form of radio wave It is wasted.
3, magnetic resonance type charging: transmitting terminal energy runs into the receiving terminal that resonant frequency is identical, by Resonance effect carries out electric energy transmission, and it is by energy dispensing device, and energy acceptance device composition, When two devices are adjusted to same frequency, resonate in a specific frequency in other words, they Just can exchange energy each other.
Its shortcoming is: miniaturization, high efficiency are more difficult, and existence safety is asked with healthy Topic.
Utility model content
In view of this, main purpose of the present utility model is, it is provided that a kind of unmanned plane wireless charging Electric installation, including being located at the charging device of battery charger cradle, and the current-collecting device being located on unmanned plane,
Oscillating circuit that described charging device includes being sequentially connected with, amplifying circuit, booster circuit and Charging electrode;
Described current-collecting device include being sequentially connected with by electricity electrode, reduction voltage circuit, rectification circuit and Unmanned plane battery.
By upper, it is possible to achieve the fast wireless for unmanned plane charges.Utilize by along Vertical Square To the induction field coupling two groups of asymmetric dipoles and produce to transmit electric power, have an advantage in that Being suitable for short distance charging, conversion efficiency is higher, generates heat relatively low.
Optionally, also include charge control module, be connected with described unmanned plane battery.
Optionally, described charge control module includes main control chip, and the most connected Current detection circuit, voltage detecting circuit and memorizer.
Described memorizer prestores the capability value of charging voltage threshold value and battery.
When the charging voltage of battery reaches charging voltage threshold value, then detect charging current, if filling When electricity electric current is less than 0.05 times of battery capacity, then stops the charging to battery, i.e. cut off unmanned The current supply circuit of machine battery.Otherwise continue charging.By being subject to electricity system and airborne power supply airborne Install charge controller between system additional, the use safety in wireless charging power station can be protected, can protect again Protect unmanned plane battery, improve battery.
Optionally, described current detection circuit includes and adopting that described unmanned plane battery is connected in series Sample resistance;
Described voltage detecting circuit includes the sampling resistor being connected with described unmanned plane cell parallel.
By upper, realized for battery current and the collection of voltage by sampling resistor, with low cost And sampling is accurately.
Optionally, the described bottom being fixed on a fixing device by electricity electrode, described fixing device It is fixed on the undercarriage of described unmanned plane by card and mode.
Optionally, the bottom surface of described fixing device and plane-parallel.
Optionally, described charging electrode is located at the upper surface of described battery charger cradle.
Accompanying drawing explanation
Fig. 1 is the principle schematic of unmanned plane wireless charging device;
Fig. 2 is the structural representation of unmanned plane wireless charging device;
Fig. 3 is the upward view of unmanned plane undercarriage.
Detailed description of the invention
For the defect overcoming prior art to exist, this utility model provides a kind of unmanned plane wireless charging Electric installation, using field coupling formula wireless charging is that unmanned plane carries out wireless charging, at unmanned plane Land and install current-collecting device additional at fulcrum, when unmanned plane rests on charging device, current-collecting device The electric energy of charging device transmission can be received, thus be embodied as unmanned plane charging.
As it is shown in figure 1, unmanned plane wireless charging device described in the utility model includes charging device 10 and current-collecting device 20.
Oscillating circuit 101 that described charging device 10 includes being sequentially connected with, amplifying circuit 102, Booster circuit 103 and charging electrode 104.Produced a pair by oscillating circuit 101 and reversely input letter Number, carry out power amplification by amplifying circuit 102, then carry out merit liter through booster circuit 103 Pressure, is ultimately connected to charging electrode 104.
Wherein, oscillating circuit 101 sends the frequency range square wave at 46kHz~50kHz.
Amplifying circuit 102, is connected with described oscillating circuit 101, for oscillating circuit 101 The square wave sent carries out power amplification, the conversion frequency about 50Khz of described amplifying circuit 102, Output voltage peak value is about 24V.Described amplifying circuit can use metal-oxide-semiconductor to realize.
Described 24V voltage is risen to 1-1.5KV by booster circuit.Charging electrode 104 uses and covers copper Plate is as transmission pole plate.It is located at the upper surface of unmanned plane charging platform, with unmanned plane described hereinafter The electricity motor 201 that is subject on undercarriage forms electric field, is used for transmitting electric energy.
Described charging device 10 also includes power supply acquisition module (not shown), with outside city Electrical connection, for being converted to low-voltage DC by outside 220V alternating current, to charging device 10 Each circuit provides running voltage.
Current-collecting device 20 include being located at be sequentially connected with on unmanned plane support by electricity electrode 201, fall Volt circuit 202 and current rectifying and wave filtering circuit 203, also include the on-board batteries being located on unmanned plane 205。
It is connected with field coupling form between described charging electrode 104 by electricity electrode 201, uses In obtaining electricity from charging electrode 104, reduction voltage circuit 202 carry out blood pressure lowering, general blood pressure lowering To 12.6V-25.2V, and by current rectifying and wave filtering circuit 203 rectifying and wave-filtering, and finally export to Unmanned aerial vehicle onboard battery 205.
In the present embodiment, at current-collecting device 20 before unmanned aerial vehicle onboard battery 205 charges, also Need to be through the charge protection of charge control module 204.Described charge control module 204 includes main Control chip, and connected current detection circuit, voltage detecting circuit and memorizer respectively. Described current detection circuit and voltage detecting circuit can be by being connected with unmanned aerial vehicle onboard battery 205 Sampling resistor realize.Wherein, for detecting sampling resistor and the unmanned aerial vehicle onboard battery of electric current 205 are connected in series, in parallel with unmanned aerial vehicle onboard battery 205 for detecting the sampling resistor of voltage Connect.Described memorizer prestores charging voltage threshold value and the appearance of unmanned aerial vehicle onboard battery 205 Value.
When the charging voltage of unmanned aerial vehicle onboard battery 205 reaches charging voltage threshold value, then detect Charging current, if charging current is less than 0.05 times of battery 205 capacity, then stops unmanned The charging of machine on-board batteries 205, i.e. cuts off the current supply circuit of unmanned aerial vehicle onboard battery 205.Instead Continuation charging.
Installed additional charge controller airborne by between electricity system and airborne electric power system, can protect The use safety in wireless charging power station, can protect again unmanned plane battery, improves battery.
As in figure 2 it is shown, described charging device 10 is located in battery charger cradle 21, wherein, fill described in Electricity electrode 104 is located at the upper surface of battery charger cradle 21.When unmanned plane drop to battery charger cradle 21, Charging electrode on unmanned plane undercarriage 30 104 with on unmanned plane undercarriage 30 by electricity electrode 201 are coupled, thus realize wireless charging.
It should be noted that the described bottom being fixed on a fixing device 22 by electricity electrode 201. This fixing device 22 and described unmanned plane undercarriage use card and mode to fix, in order to realize Dismounting.It addition, the bottom surface of described fixing device 22 keeps parallel with horizontal plane.Thus may be used Once by the coupling area between electricity electrode 201 and charging electrode 104, to keep charge efficiency.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this reality With novel.In a word, all within spirit of the present utility model and principle, any amendment of being made, Equivalent, improvement etc., within should be included in protection domain of the present utility model.

Claims (7)

1. a unmanned plane wireless charging device, it is characterised in that include being located at battery charger cradle (21) Charging device (10), and the current-collecting device (20) being located on unmanned plane,
Described charging device (10) includes the oscillating circuit (101) being sequentially connected with, amplifies electricity Road (102), booster circuit (103) and charging electrode (104);
Described current-collecting device (20) includes that be sequentially connected with is subject to electricity electrode (201), blood pressure lowering electricity Road (202), rectification circuit (203) and unmanned aerial vehicle onboard battery (205).
Device the most according to claim 1, it is characterised in that also include control of charging Module (204), is connected with described unmanned aerial vehicle onboard battery (205).
Device the most according to claim 2, it is characterised in that described charging controls mould Block (204) includes main control chip, and connected current detection circuit, voltage respectively Testing circuit and memorizer.
Device the most according to claim 3, it is characterised in that described current detecting electricity Road includes the sampling resistor being connected in series with described unmanned aerial vehicle onboard battery (205);
Described voltage detecting circuit includes being connected in parallel with described unmanned aerial vehicle onboard battery (205) Sampling resistor.
Device the most according to claim 1, it is characterised in that described by electricity electrode (201) Being fixed on the bottom surface of a fixing device (22), described fixing device (22) is by card and mode It is installed on the undercarriage (30) of described unmanned plane.
Device the most according to claim 5, it is characterised in that described fixing device (22) Bottom surface parallel setting with horizontal plane.
Device the most according to claim 5, it is characterised in that described charging electrode (104) It is located at the upper surface of described battery charger cradle (21).
CN201620233423.2U 2016-03-24 2016-03-24 Unmanned aerial vehicle wireless charging device Active CN205646955U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620233423.2U CN205646955U (en) 2016-03-24 2016-03-24 Unmanned aerial vehicle wireless charging device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620233423.2U CN205646955U (en) 2016-03-24 2016-03-24 Unmanned aerial vehicle wireless charging device

Publications (1)

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CN205646955U true CN205646955U (en) 2016-10-12

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106451663A (en) * 2016-11-15 2017-02-22 哈工大机器人集团上海有限公司 Automatic wheeled robot charging device
CN107972513A (en) * 2017-11-30 2018-05-01 无锡龙翼智能科技有限公司 A kind of UAV Intelligent charging method and device
CN111987780A (en) * 2020-08-31 2020-11-24 重庆大学 Unmanned aerial vehicle electric field coupling mechanism and wireless charging system, platform and unmanned aerial vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106451663A (en) * 2016-11-15 2017-02-22 哈工大机器人集团上海有限公司 Automatic wheeled robot charging device
CN107972513A (en) * 2017-11-30 2018-05-01 无锡龙翼智能科技有限公司 A kind of UAV Intelligent charging method and device
CN111987780A (en) * 2020-08-31 2020-11-24 重庆大学 Unmanned aerial vehicle electric field coupling mechanism and wireless charging system, platform and unmanned aerial vehicle
CN111987780B (en) * 2020-08-31 2022-04-22 重庆大学 Unmanned aerial vehicle electric field coupling mechanism and wireless charging system, platform and unmanned aerial vehicle

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C14 Grant of patent or utility model
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20180130

Address after: 516029 Guangdong District of Huicheng city in Huizhou province road six Tonghu Zhongkai Ecological Innovation Park 1 building 4 floor Tai Technology

Co-patentee after: Beijing Information Science and Technology University

Patentee after: Guangdong hi tech Development Co., Ltd.

Address before: 518000 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A

Co-patentee before: Beijing Information Science and Technology University

Patentee before: Shenzhen Chuangyi Ruixiang Sky Technology Co., Ltd.

TR01 Transfer of patent right