CN106394929A - Photovoltaic charging device of rotary-wing unmanned aerial vehicle - Google Patents

Photovoltaic charging device of rotary-wing unmanned aerial vehicle Download PDF

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Publication number
CN106394929A
CN106394929A CN201610968954.0A CN201610968954A CN106394929A CN 106394929 A CN106394929 A CN 106394929A CN 201610968954 A CN201610968954 A CN 201610968954A CN 106394929 A CN106394929 A CN 106394929A
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CN
China
Prior art keywords
module
aerial vehicle
unmanned aerial
wing unmanned
accumulator
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
CN201610968954.0A
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Chinese (zh)
Inventor
孙明健
姜腾
段士奇
姚统
张泽林
冯佳时
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Harbin Institute of Technology Weihai
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Harbin Institute of Technology Weihai
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Application filed by Harbin Institute of Technology Weihai filed Critical Harbin Institute of Technology Weihai
Priority to CN201610968954.0A priority Critical patent/CN106394929A/en
Publication of CN106394929A publication Critical patent/CN106394929A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F3/00Ground installations specially adapted for captive aircraft
    • B64F3/02Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/02Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters
    • H02J7/022Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters characterised by the type of converter
    • H02J7/025Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters characterised by the type of converter using non-contact coupling, e.g. inductive, capacitive
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/06Unmanned aerial vehicles; Equipment therefor characterised by in-flight supply of energy
    • B64C2201/066Unmanned aerial vehicles; Equipment therefor characterised by in-flight supply of energy by recharging of batteries, e.g. by induction

Abstract

The invention relates to a photovoltaic charging device of a rotary-wing unmanned aerial vehicle. The photovoltaic charging device of the rotary-wing unmanned aerial vehicle comprises a device structured shell, and a power system, a communication control management system, a wireless charging system and a direct-current motor system which are arranged on the device structured shell. The power system is used for supplying power for the communication control management system, the wireless charging system and the direct-current motor system; the communication control management system is used for controlling the switching on/off of the wireless charging system, and is used for communicating with the rotary-wing unmanned aerial vehicle and receiving an instruction of a command and control center. The a photovoltaic charging device provided by the invention can provide a stopping, charging and task planning platform for the rotary-wing unmanned aerial vehicle, so that the step of manually replacing batteries is saved, and the cruising ability and the autonomous flight ability of the rotary-wing unmanned aerial vehicle are improved.

Description

The photovoltaic charged device of rotor wing unmanned aerial vehicle
Technical field
The present invention relates to photovoltaic and unmanned air vehicle technique field, more particularly, to a kind of rotor wing unmanned aerial vehicle photovoltaic charged Device.
Background technology
In recent years, rotor wing unmanned aerial vehicle is because of relative low price, mobility strong, the advantages of restriction by ground obstacle, Photovoltaic plant is patrolled and examined and is increasingly widely applied with fields such as logistics distributions, is effectively improved photovoltaic plant and patrols and examines and thing The efficiency of stream dispensing, saves substantial amounts of man power and material.
But, rotor wing unmanned aerial vehicle generally existing that cruising time is short, the shortcoming of autonomous flight scarce capacity.At present, big portion The cruising time dividing rotor wing unmanned aerial vehicle is less than 1 hour, and each rotor wing unmanned aerial vehicle at least needs operator to come Control its flight.Obviously, these shortcomings largely limit unmanned plane application.
Content of the invention
The technical problem to be solved in the present invention is:Rotor wing unmanned aerial vehicle cruising time is short, the problem of autonomous flight scarce capacity.
For solving the above problems, the present invention proposes a kind of photovoltaic charged device of rotor wing unmanned aerial vehicle, including apparatus structure Outside the pale of civilization shell, and it is respectively arranged at power-supply system on described device structuring shell, communication control management system, wireless charging System and direct current motor system;
Described power-supply system is used for as described communication control management system, described wireless charging system and described unidirectional current Machine system power supply;
Described communication control management system is used for controlling the unlatching/closing of described wireless charging system;And, for institute State rotor wing unmanned aerial vehicle to be communicated, and receive the instruction of command and control center.
Alternatively, described power-supply system includes solar panel, battery cell monitoring module, accumulator, low-pressure linear voltage stabilizing Module and DC-AC inverter;
Described battery cell monitoring module respectively with described solar panel, accumulator, low-pressure linear Voltage stabilizing module and DC- AC inverter is connected;
Described battery cell monitoring module is used for mating the output voltage of described solar panel and the input of described accumulator Voltage, is monitored to be charged to described accumulator and to the electricity of described accumulator;
It is that described low-pressure linear Voltage stabilizing module, described DC-AC are inverse that described accumulator is used for by described battery cell monitoring module Become device, described direct current motor system is powered.
Described low-pressure linear Voltage stabilizing module is used for exporting relevant voltage to described communication control management system.
Described DC-AC inverter is used for exporting relevant voltage to described wireless charging system.
Alternatively, described power-supply system also includes emergency battery;
Described emergency battery is connected with described battery cell monitoring module;
Correspondingly, described battery cell monitoring module is additionally operable in described accumulator normal work it is ensured that described emergent electric power storage Pond is in Full Power State;And, when described accumulator breaks down, make described emergency battery take over described accumulator and enter Row work, and the Reflector information of described accumulator is sent to described communication control management system.
Alternatively, described communication control management system includes:Antenna, short-range communications module, remote communication module, satellite are led Model plane block and CPU module;
Described antenna is connected with described short-range communications module, satellite navigation module and remote communication module respectively;
Described CPU module is used for determining the positional information of described device by described satellite navigation module, and leads to Cross described remote communication module and the positional information of described device is sent to described rotor wing unmanned aerial vehicle;And, for by described Short-range communications module is downloaded the data of described rotor wing unmanned aerial vehicle collection and/or is uploaded the aerial mission letter of described rotor wing unmanned aerial vehicle Breath;And, for by described remote communication module to described command centre send the collection of described rotor wing unmanned aerial vehicle data and/ Or the Reflector information of described accumulator, and receive the instruction from described command centre;It is additionally operable to control described wireless charging Electric system and described direct current motor system.
Alternatively, described communication control management system also includes memory module and usb interface module;
Described memory module is used for storing the data of described rotor wing unmanned aerial vehicle collection and/or the fault mark of described accumulator Will information;
Described usb interface module is used for deriving the data in described memory module, and for rising to described device Level and maintenance.
Alternatively, described direct current motor system includes motor drive module and direct current generator;
Described accumulator is powered for described motor drive module by described battery cell monitoring module;
Described motor drive module is connected with described CPU module, and described CPU module passes through to described Motor drive module sends control instruction to control described direct current generator.
Alternatively, described device structuring shell includes hangar and shuts down platform and optical beacon;
Described optical beacon is located at described hangar and shuts down on platform;
Described optical beacon is used for being identified for described rotor wing unmanned aerial vehicle;
Described hangar and shutdown platform are used for being landed for described rotor wing unmanned aerial vehicle and stopping.
Alternatively, described device structuring shell also includes open-close type slidable panels, wheel undercarriage and pulls joint;
Described open-close type slidable panels are connected with described direct current generator;Described hangar and shutdown platform are located at described wheeled bottom On disk;Described dragging joint is located on described wheel undercarriage.
Alternatively, described wireless charging system includes electrical switch;
Described electrical switch is connected with described CPU module and described DC-AC inverter respectively;
Described CPU module be additionally operable to by described electrical switch control described wireless charging system unlatching and Close.
Alternatively, described wireless charging system also includes primary coil and secondary coil;
Described primary coil is connected with described electrical switch;Described primary coil is located on described optical beacon;
Described secondary coil is located on the undercarriage of described rotor wing unmanned aerial vehicle.
The photovoltaic charged device of the rotor wing unmanned aerial vehicle of the present invention, by power-supply system be described communication control management system, Described wireless charging system and described direct current motor system are powered, and control described wireless charging by communication control management system Unlatching/the closing of system;And, for being communicated with described rotor wing unmanned aerial vehicle, and receive the instruction of command and control center, can To provide the platform of stop, charging and mission planning for rotor wing unmanned aerial vehicle, eliminate the artificial link changing battery, improve rotation The endurance of wing unmanned plane and autonomous flight ability.
Brief description
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing Have technology description in required use accompanying drawing do simply introduce it should be apparent that, drawings in the following description are the present invention Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also basis These accompanying drawings obtain other accompanying drawings.
Fig. 1 is the structured flowchart of the photovoltaic charged device of rotor wing unmanned aerial vehicle of one embodiment of the invention;
Fig. 2 is the primary coil arrangement effect diagram in the wireless charging system of one embodiment of the invention;
Fig. 3 is the secondary coil arrangement effect diagram in the wireless charging system of one embodiment of the invention;
Fig. 4 is the structural representation of the outside the pale of civilization shell of apparatus structure of one embodiment of the invention.
Specific embodiment
Purpose, technical scheme and advantage for making the embodiment of the present invention are clearer, below in conjunction with the embodiment of the present invention In accompanying drawing, the technical scheme in the embodiment of the present invention is explicitly described it is clear that described embodiment is the present invention A part of embodiment, rather than whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art are not having The every other embodiment being obtained under the premise of making creative work, broadly falls into the scope of protection of the invention.
Fig. 1 is the structured flowchart of the photovoltaic charged device of rotor wing unmanned aerial vehicle of one embodiment of the invention, as shown in figure 1, The photovoltaic charged device of the rotor wing unmanned aerial vehicle that the present embodiment provides includes power-supply system 1, communication control management system 2, wireless charging Electric system 3, direct current motor system 4, the outside the pale of civilization shell of apparatus structure 5;
Described power-supply system 1 is used for described communication control management system 2, described wireless charging system 3, described unidirectional current Machine system 4 is powered;
The effect of described communication control management system 2 is to send control signal to described direct current motor system 4, controls described The opening and closing of wireless charging system 3, are communicated with rotor wing unmanned aerial vehicle, and receive the instruction from command and control center;
Described power-supply system 1, communication control management system 2, wireless charging system 3 and direct current motor system 4 are all located at institute State on the outside the pale of civilization shell of apparatus structure 5.
The photovoltaic charged device of the rotor wing unmanned aerial vehicle of the present invention, by power-supply system be described communication control management system, Described wireless charging system and described direct current motor system are powered, and control described wireless charging by communication control management system Unlatching/the closing of system;And, for being communicated with described rotor wing unmanned aerial vehicle, and receive the instruction of command and control center, can To provide the platform of stop, charging and mission planning for rotor wing unmanned aerial vehicle, eliminate the artificial link changing battery, improve rotation The endurance of wing unmanned plane and autonomous flight ability.
Further, preferred as above-described embodiment, described power-supply system 1 specifically may include:Solar panel 11, Battery cell monitoring module 12, accumulator 13, emergency battery 14, low-pressure linear Voltage stabilizing module 15 and DC-AC inverter 16, its In:
Described solar panel 11 is connected with described battery cell monitoring module 12.Described battery cell monitoring module 12 and described storage Battery 13 is connected.Described battery cell monitoring module 12 is connected with described emergency battery 14.Described battery cell monitoring module 12 with described Low-pressure linear voltage regulator module 15 is connected.Described battery cell monitoring module 12 is connected with described DC-AC inverter 16.Described battery prison The effect of control module 12 is the output voltage to described solar panel 11 and described accumulator 13, described emergency battery 14 Input voltage mated, thus charging to described accumulator 13 and described emergency battery 14;To described accumulator 13 He The electricity of described emergency battery 14 is monitored it is ensured that in the case of described accumulator 13 normal work, described emergent storage Battery 14 keeps Full Charge Capacity (now not access system), when described accumulator 13 breaks down, described emergency battery 14 energy Access system, to ensure the normal work of device, sends Reflector information to described communication control management system 2 simultaneously;
Described accumulator 13 and described emergency battery 14 are respectively described low-voltage line by described battery cell monitoring module 12 Property Voltage stabilizing module 15, described DC-AC inverter 16, motor drive module 41 are powered.Described low-pressure linear Voltage stabilizing module 15 can be defeated Go out different size of voltage to use for described communication control management system 2.Described DC-AC inverter 16 is used for described wireless charging Electric system 3 is powered;
Alternatively, described battery cell monitoring module 12 has multiple interfaces;
Described low-pressure linear Voltage stabilizing module 15 is respectively described short-range communications module 22, described remote communication module 23, institute State satellite navigation module 24, described CPU module 25, described memory module 26 are powered;Described DC-AC inverter 16 Powered for described primary coil 321-328 by described electrical switch 31.
Further, preferred as above-described embodiment, described communication control management system 2 specifically may include:Antenna 21, Short-range communications module 22, remote communication module 23, satellite navigation module 24, CPU module 25, memory module 26, Usb interface module 27, wherein:
Described antenna 21 respectively with described short-range communications module 22, described remote communication module 23 and described satellite navigation mould Block 24 connects.Described CPU module 25 determines the positional information of device by described satellite navigation module 24, and leads to Cross described remote communication module 23 and the positional information of device is sent to rotor wing unmanned aerial vehicle;
When rotor wing unmanned aerial vehicle reaches near device, rotor wing unmanned aerial vehicle is identified by self-contained vision guided navigation device Optical beacon 52 in hangar and shutdown platform 51, and described central processing unit mould is received by described short-range communications module 22 The guide of block 25 come to drop to described hangar and shut down platform 51 on;
Described CPU module 25 downloads the data of rotor wing unmanned aerial vehicle collection by described short-range communications module 22 With upload rotor wing unmanned aerial vehicle aerial mission information next time;
Specifically, described CPU module 25 downloads the data of unmanned plane collection by described short-range communications module 22 With upload unmanned plane aerial mission next time, and store data in described memory module 26;Described memory module Data in 26 both command and control center can be sent to by described remote communication module 22 it is also possible to by manual type from Described usb interface module 27 is derived;
The data that described CPU module 25 is collected by described 23 rotor wing unmanned aerial vehicles of remote communication module and Reflector information with regard to described accumulator 13 is sent to command centre, and receives the instruction from commander command centre;
Described CPU module 25 controls the opening and closing of wireless charging system by electrical switch 31;
Described usb interface module 27 is used for deriving data in memorizer it is possible to for being upgraded to device and tieing up Shield.
Further, preferred as above-described embodiment, described wireless charging system 3 specifically may include:Electrical switch 31, Primary coil 321-328, secondary coil 331-334 (referring to Fig. 2, Fig. 3), wherein:
Described electrical switch 31 is connected with described CPU module 25.Described electrical switch 31 is inverse with described DC-AC Become device 16 to be connected.Described electrical switch 31 is connected with described primary coil 321-328.Described primary coil 321-328 is located at institute State on optical beacon 52;Described secondary coil 331-334 is located on the undercarriage of rotor wing unmanned aerial vehicle;
When rotor wing unmanned aerial vehicle drops on described shutdown platform 51, described central processing module 25 controls electrical switch 31 Open, described wireless charging system 3 starts to charge to rotor wing unmanned aerial vehicle;When rotor wing unmanned aerial vehicle is fully charged, led to by described short range Letter 22 charge completion informations of module are sent to described central processing module 25, and described central processing module 25 controls described electronics Switch 31 closing, rotor wing unmanned aerial vehicle charging process terminates;
Specifically, described CPU module 25 controls the opening and closing of described electrical switch 31, makes described DC-AC Inverter 16 can be powered for described primary coil 321-328, and the secondary coil 331-334 by installing on unmanned plane undercarriage To charge to rotor wing unmanned aerial vehicle.
As shown in Fig. 2 described primary coil 321-328 is located on described optical beacon 52;As shown in figure 3, described secondary Coil 331-334 is located on rotor wing unmanned aerial vehicle undercarriage.
Further, as shown in figure 1, preferred as above-described embodiment, described direct current motor system 4 specifically may include: Motor drive module 41, direct current generator 42, wherein:
Described motor drive module 41 is connected with described CPU module 25.Described motor drive module 41 with described Direct current generator 42 is connected.
Described CPU module 25 sends control instruction to described motor drive module 41, realizes to direct current generator 42 Control.
Fig. 4 is the structural representation of the outside the pale of civilization shell of apparatus structure of one embodiment of the invention, as shown in figure 4, as above-mentioned Embodiment preferred, described device structuring shell 5 specifically may include:Hangar and shutdown platform 51, optical beacon 52, open-close type Slidable panels 53, wheel undercarriage 54, dragging joint 55, wherein:
Described optical beacon 52 is located at described hangar and shuts down on platform 51;Described hangar and shutdown platform 51 are positioned at described On wheel undercarriage 54;Described dragging joint 55 is located on described wheel undercarriage 54;Described open-close type slidable panels 53 are located at described Shut down on platform 51, and be connected with described direct current generator 42.
Wherein, described solar panel 11 is located on described open-close type slidable panels 53.
Described power-supply system 1, described communication control management system 2, described wireless charging system 3 and described direct current generator System 4 is respectively positioned on described hangar and shuts down inside platform 51;
Described direct current generator 42 is connected by drive mechanism with described open-close type slidable panels 53, makes described direct current generator 42 Opening and closing of described open-close type slidable panels 53 can be controlled.
Compared with prior art, technique scheme at least has following beneficial effect:
1) the photovoltaic charged device of described rotor wing unmanned aerial vehicle can provide stop, charge for executing the rotor wing unmanned aerial vehicle of task Platform, eliminate the artificial link changing battery, improve endurance and the autonomous flight ability of rotor wing unmanned aerial vehicle.
2) the photovoltaic charged device of described rotor wing unmanned aerial vehicle can be downloaded to the data of rotor wing unmanned aerial vehicle collection, and on Carry the mission planning to rotor wing unmanned aerial vehicle, improve the AUTONOMOUS TASK ability of rotor wing unmanned aerial vehicle.
3) the photovoltaic charged device of described rotor wing unmanned aerial vehicle can obtain energy by self-contained solar panel, leads to Cross remote communication module to get in touch with command centre, and there is wheel undercarriage and pull joint, can easily be deployed in partially Far region.
4) the photovoltaic charged device of described rotor wing unmanned aerial vehicle has open-close type slidable panels.In the good situation of weather conditions Lower open-close type slidable panels are opened, and let rotor wing unmanned aerial vehicle execution task fly away;In the case of weather conditions difference, recall rotor unmanned Machine, open-close type slidable panels are closed, and rotor wing unmanned aerial vehicle is played a protective role.
Above example is merely to illustrate technical scheme, is not intended to limit;Although with reference to the foregoing embodiments The present invention has been described in detail, it will be understood by those within the art that:It still can be to aforementioned each enforcement Technical scheme described in example is modified, or carries out equivalent to wherein some technical characteristics;And these are changed or replace Change, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.

Claims (10)

1. a kind of photovoltaic charged device of rotor wing unmanned aerial vehicle, it is characterised in that including the outside the pale of civilization shell of apparatus structure, and is respectively provided with Power-supply system on described device structuring shell, communication control management system, wireless charging system and direct current motor system;
Described power-supply system is used for as described communication control management system, described wireless charging system and described direct current generator system System power supply;
Described communication control management system is used for controlling the unlatching/closing of described wireless charging system;And, for described rotation Wing unmanned plane is communicated, and receives the instruction of command and control center.
2. device according to claim 1 is it is characterised in that described power-supply system includes solar panel, battery prison Control module, accumulator, low-pressure linear Voltage stabilizing module and DC-AC inverter;
Described battery cell monitoring module is inverse with described solar panel, accumulator, low-pressure linear Voltage stabilizing module and DC-AC respectively Become device to be connected;
Described battery cell monitoring module is used for mating the output voltage of described solar panel and the input voltage of described accumulator, It is monitored to be charged to described accumulator and to the electricity of described accumulator;
Described accumulator be used for by described battery cell monitoring module be described low-pressure linear Voltage stabilizing module, described DC-AC inverter, Described direct current motor system is powered.
Described low-pressure linear Voltage stabilizing module is used for exporting relevant voltage to described communication control management system.
Described DC-AC inverter is used for exporting relevant voltage to described wireless charging system.
3. device according to claim 2 is it is characterised in that described power-supply system also includes emergency battery;
Described emergency battery is connected with described battery cell monitoring module;
Correspondingly, described battery cell monitoring module is additionally operable in described accumulator normal work it is ensured that at described emergency battery In Full Power State;And, when described accumulator breaks down, make described emergency battery take over described accumulator and carry out work Make, and send the Reflector information of described accumulator to described communication control management system.
4. device according to claim 2 is it is characterised in that described communication control management system includes:Antenna, short range are led to Letter module, remote communication module, satellite navigation module and CPU module;
Described antenna is connected with described short-range communications module, satellite navigation module and remote communication module respectively;
Described CPU module is used for determining the positional information of described device by described satellite navigation module, and passes through institute State remote communication module and the positional information of described device is sent to described rotor wing unmanned aerial vehicle;And, for by described short range Communication module downloads the data of described rotor wing unmanned aerial vehicle collection and/or the aerial mission information uploading described rotor wing unmanned aerial vehicle;With And, for sending data and/or the institute of described rotor wing unmanned aerial vehicle collection to described command centre by described remote communication module State the Reflector information of accumulator, and receive the instruction from described command centre;It is additionally operable to control described wireless charging system System and described direct current motor system.
5. device according to claim 4 is it is characterised in that described communication control management system also includes memory module And usb interface module;
Described memory module is used for storing the data of described rotor wing unmanned aerial vehicle collection and/or the Reflector letter of described accumulator Breath;
Described usb interface module is used for deriving data in described memory module, and for described device is carried out upgrading and Safeguard.
6. device according to claim 4 is it is characterised in that described direct current motor system includes motor drive module and straight Stream motor;
Described accumulator is powered for described motor drive module by described battery cell monitoring module;
Described motor drive module is connected with described CPU module, and described CPU module passes through to described motor Drive module sends control instruction to control described direct current generator.
7. device according to claim 6 is it is characterised in that described device structuring shell includes hangar and shuts down platform And optical beacon;
Described optical beacon is located at described hangar and shuts down on platform;
Described optical beacon is used for being identified for described rotor wing unmanned aerial vehicle;
Described hangar and shutdown platform are used for being landed for described rotor wing unmanned aerial vehicle and stopping.
8. device according to claim 7 is it is characterised in that described device structuring shell also includes open-close type sliding surface Plate, wheel undercarriage and dragging joint;
Described open-close type slidable panels are connected with described direct current generator;Described hangar and shutdown platform are located at described wheel undercarriage On;Described dragging joint is located on described wheel undercarriage.
9. device according to claim 7 is it is characterised in that described wireless charging system includes electrical switch;
Described electrical switch is connected with described CPU module and described DC-AC inverter respectively;
Described CPU module is additionally operable to control the opening and closing of described wireless charging system by described electrical switch.
10. device according to claim 9 it is characterised in that described wireless charging system also include primary coil and time Level coil;
Described primary coil is connected with described electrical switch;Described primary coil is located on described optical beacon;
Described secondary coil is located on the undercarriage of described rotor wing unmanned aerial vehicle.
CN201610968954.0A 2016-11-03 2016-11-03 Photovoltaic charging device of rotary-wing unmanned aerial vehicle Pending CN106394929A (en)

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CN107994644A (en) * 2017-12-21 2018-05-04 天津大学 Solar powered unmanned plane energy conversion method
CN108255163A (en) * 2018-01-24 2018-07-06 衢州职业技术学院 The control system and control method of plant protection unmanned plane
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CN108910036A (en) * 2018-06-19 2018-11-30 智飞智能装备科技东台有限公司 A kind of multi-functional rotor of unmanned plane
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CN109286209A (en) * 2017-07-20 2019-01-29 重庆邮电大学 Adaptive unmanned plane charging unit
CN109874643A (en) * 2019-03-13 2019-06-14 安徽鼎博新能源科技发展有限公司 A kind of photovoltaic power generation intelligent agricultural system and its irrigation method
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CN104638702A (en) * 2013-11-13 2015-05-20 沈阳新松机器人自动化股份有限公司 Photovoltaic charging system for outdoor robot
WO2016059555A1 (en) * 2014-10-13 2016-04-21 Systems Engineering Associates Corporation Systems and methods for deployment and operation of vertical take-off and landing (vtol) unmanned aerial vehicles
CN204279932U (en) * 2014-10-28 2015-04-22 深圳九星智能航空科技有限公司 Bottom is provided with the unmanned vehicle of wireless charging current-collecting device
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CN107140194A (en) * 2017-05-16 2017-09-08 华东交通大学 A kind of many rotor railway automatic tour inspection systems of tracking for supporting automatic charging
CN109286209A (en) * 2017-07-20 2019-01-29 重庆邮电大学 Adaptive unmanned plane charging unit
CN107994644A (en) * 2017-12-21 2018-05-04 天津大学 Solar powered unmanned plane energy conversion method
CN108255163A (en) * 2018-01-24 2018-07-06 衢州职业技术学院 The control system and control method of plant protection unmanned plane
CN108490971A (en) * 2018-03-21 2018-09-04 深圳臻迪信息技术有限公司 Unmanned plane job platform
CN108762313A (en) * 2018-06-14 2018-11-06 合肥凯石投资咨询有限公司 Solar energy unmanned plane towed solar cell folding electromagnetic accommodation method
CN108910036A (en) * 2018-06-19 2018-11-30 智飞智能装备科技东台有限公司 A kind of multi-functional rotor of unmanned plane
CN109216487A (en) * 2018-07-27 2019-01-15 合肥凯石投资咨询有限公司 Towed unmanned plane solar cell encapsulation method based on netted FPC bottom plate
CN109874643A (en) * 2019-03-13 2019-06-14 安徽鼎博新能源科技发展有限公司 A kind of photovoltaic power generation intelligent agricultural system and its irrigation method
CN111319786A (en) * 2020-04-01 2020-06-23 中国人民解放军陆军工程大学 Mooring type unmanned aerial vehicle power supply system and power supply method thereof

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