CN107696882B - Aerial charging device of unmanned aerial vehicle - Google Patents

Aerial charging device of unmanned aerial vehicle Download PDF

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Publication number
CN107696882B
CN107696882B CN201710608093.XA CN201710608093A CN107696882B CN 107696882 B CN107696882 B CN 107696882B CN 201710608093 A CN201710608093 A CN 201710608093A CN 107696882 B CN107696882 B CN 107696882B
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China
Prior art keywords
frame
unmanned aerial
aerial vehicle
vertical pipes
power box
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CN201710608093.XA
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Chinese (zh)
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CN107696882A (en
Inventor
宋惠忠
赵玉勇
沈浚
俞晓良
施海峰
方敏
刘继文
孙东方
俞威
方鑫勇
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Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
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Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
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Priority to CN201710608093.XA priority Critical patent/CN107696882B/en
Publication of CN107696882A publication Critical patent/CN107696882A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/16Information or communication technologies improving the operation of electric vehicles

Abstract

The utility model provides an aerial charging device of unmanned aerial vehicle, includes unmanned aerial vehicle, wire pole, power supply box, the control unit, charging module and communication antenna A. The power supply box, the control unit, the charging module and the communication antenna A are all fixedly arranged at the upper end of the telegraph pole. The control unit is connected with the power box, the charging module and the communication antenna A. The unmanned aerial vehicle is provided with a communication antenna B for communicating with the communication antenna A, and a judging device for judging the distance between the residual power and the charging device.

Description

Aerial charging device of unmanned aerial vehicle
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and relates to an unmanned aerial vehicle for various occasions such as field construction, exploration, transportation, tourism, rescue and the like. More particularly, the present invention relates to an unmanned aerial vehicle air charging station arrangement.
Background
At present, unmanned aerial vehicles are widely applied in the fields of field construction, exploration, transportation, tourism, rescue and the like, and mainly play roles in observing field conditions, acquiring information, transmitting a small amount of materials and the like. The system has unique advantages, is not limited by terrain, can quickly reach the site of a fault position, even a place with rare occurrence, and can carry out close-range observation; through the shooting and camera equipment, video and image data are sent to relevant departments, so that technicians of the relevant departments can analyze and judge the site, or materials can be rapidly conveyed to the site to carry out rescue, and a good effect is achieved.
However, the current unmanned aerial vehicle has the following problems:
firstly, in the process of inspection and observation, as repeated and long-time suspended observation is needed to collect image data, the energy consumption is very high, and the capacity of a battery is limited, the working time is limited; secondly, if the electric quantity of the unmanned aerial vehicle is exhausted, the unmanned aerial vehicle must return to the ground and be recharged or the battery is replaced, and because the operation place of the unmanned aerial vehicle is far away from the landing and charging place, the unmanned aerial vehicle needs to consume a large amount of time in the processes of returning to the ground, charging or replacing the battery and recovering operation in the process of returning to the operation place, and the work is interrupted, so that the normal and continuous operation in the air is delayed.
Application number 201510704012.7, application publication number CN 105270627A, name "two unmanned aerial vehicle systems of air charge promotion duration" disclose an unmanned aerial vehicle charging mode: "it contains female unmanned aerial vehicle, son unmanned aerial vehicle, aerial docking mechanism that charges, and female unmanned aerial vehicle, son unmanned aerial vehicle link together through aerial docking mechanism that charges and form two unmanned aerial vehicle systems, and aerial docking mechanism that charges comprises fixed mounting at the docking control mechanism of female unmanned aerial vehicle below, fixed mounting at the docking plug of son unmanned aerial vehicle top. The invention aim of the inventor is to expect that the unmanned aerial vehicle system can solve the problem of endurance of the existing unmanned aerial vehicle system, can be charged in the air, increases endurance and achieves the purpose of infinite endurance; the defects of interruption of the execution task and inaccurate position when the existing 2 separated unmanned aerial vehicles are used for realizing long voyage are overcome; the problem of current unmanned aerial vehicle's load and the defect that can not be nimble changeable during navigation is solved. "there are problems: there are stability, reliability problem in mother unmanned aerial vehicle and son unmanned aerial vehicle when the butt joint in the air, also have the problem that can not fine butt joint and bump one of them unmanned aerial vehicle promptly.
Disclosure of Invention
The invention mainly aims to provide an aerial charging device of an unmanned aerial vehicle, which is high in reliability.
The technical scheme adopted by the invention is as follows: the utility model provides an aerial charging device of unmanned aerial vehicle, includes unmanned aerial vehicle, the wire pole, the upper end of wire pole has set firmly a power supply box, the control unit, the module of charging, communication antenna A, power supply box installation bobbin cradle and safety guard subassembly. A power box, a control unit, a charging module, a communication antenna A, a power box mounting barrel frame and a safety cover assembly are all arranged at the upper end of the telegraph pole. The control unit is connected with the power box, the charging module and the communication antenna A; the unmanned aerial vehicle is provided with a communication antenna B for communicating with the communication antenna A, and a judging device for judging the distance between the residual power and the charging device;
the lower end of the power box mounting barrel frame is sleeved and fixed at the upper end of the telegraph pole, and the periphery of the upper end of the power box mounting barrel frame is horizontally bent outwards to form a charging module mounting part; the power box and the control unit are fixedly arranged at the upper end of the power box mounting barrel frame and below the wireless charging module;
the safety cover assembly comprises a safety cover framework and a rainproof cover cloth; the lower end of the safety shield framework comprises a plurality of lower hollow vertical pipes, a large lower frame, a small lower frame and a plurality of lower frame connecting pipes; two ends of the lower frame connecting pipe are fixedly connected with the large lower frame and the small lower frame respectively; the positions of the large lower frame and the small lower frame are lower than the lowest end of the unmanned aerial vehicle; the large lower frame is fixedly connected with a plurality of lower hollow vertical pipes, and the small lower frame is fixedly connected with the telegraph pole; a rain-proof cover cloth accommodating mechanism is arranged above the large lower frame and comprises a torsion spring and a rotating shaft; the upper end of the safety shield framework comprises movable vertical pipes with the same number as the lower hollow vertical pipes and a safety shield connecting frame connected with the upper ends of the movable vertical pipes; the movable vertical pipes are inserted into the corresponding hollow vertical pipes, and the positions can be adjusted up and down when the movable vertical pipes work; the rain-proof cover cloth comprises side wall rain-proof cover cloth and top cover rain-proof cover cloth, the lower side of the side wall rain-proof cover cloth is connected with the rotating shaft, and the upper side of the side wall rain-proof cover cloth is connected with the safety cover connecting frame; a torsional spring and a torsional spring rotating shaft are arranged in one frame edge of the safety shield connecting frame, two side frame edges connected with the frame edge are provided with guide rails, sliding seats are arranged on the guide rails, and the two sliding seats are connected by a sliding seat connecting rod; one side of the top cover rainproof cover cloth is connected with the torsion spring rotating shaft, and the other side of the top cover rainproof cover cloth is connected with the sliding seat connecting rod.
Here, the unmanned aerial vehicle aerial charging device is installed on the upper end of the utility pole of a 10kV medium voltage line or a 0.4kV low voltage line, except for the unmanned aerial vehicle. In order to overcome the spreading effect of the side wall rainproof cover cloth and the top cover rainproof cover cloth of the torsion spring, the safety cover assembly further comprises a corresponding motor. Waiting to accept the in-process that unmanned aerial vehicle charges, the activity standpipe falls to the extreme low position, and the rain-proof cover cloth of side wall is in the state of packing up, and the rain-proof cover cloth of top cap then covers the safety guard connection frame in order to carry out rain-proof, sun-proof protection to components such as motors. When accepting unmanned aerial vehicle and will returning to charge, then pack up the rain-proof cover cloth of top cap in good time, wait unmanned aerial vehicle and rise movable standpipe to highest position after the whereabouts targets in place on the device again, then spread out the rain-proof cover cloth of top cap and come, wait until unmanned aerial vehicle fills again after the electricity and pack up the rain-proof cover of top cap, descend the activity standpipe to the lowest position, and then just can operate unmanned aerial vehicle and leave the position of charging and carry out corresponding work. When the unmanned aerial vehicle works, the unmanned aerial vehicle can judge and limit the flight distance and the flight time of the unmanned aerial vehicle by utilizing the residual power and the distance between the unmanned aerial vehicle and the charging device through the communication relation between the communication antenna A and the communication antenna B, so that the unmanned aerial vehicle can timely fly towards the position of the communication antenna A when the power needs to be supplemented, and then land on the charging module for charging. According to the invention, the power box is provided with the voltage reduction device, can be used in places with 10kV medium-voltage lines or 0.4kV low-voltage lines, and has the advantages of wide application range, convenience and reliability in use.
Preferably, the charging module is a wireless charging module, and comprises a flat plate and a wireless charging head arranged on the flat plate; correspondingly, be equipped with the wireless receiving head on the unmanned aerial vehicle. This preferred scheme, rational in infrastructure, operational reliability is high.
Preferably, the periphery of the charging module mounting portion is bent upward. This preferred scheme is favorable to charging the accurate installation of module.
Preferably, the power box is arranged below the control unit, and the power box mounting barrel is fixedly provided with a power box supporting block between the lower part of the power box and the upper end of the telegraph pole. Preferably, the lower end of the power box supporting block is provided with a conical concave cavity matched with the upper end of the telegraph pole, the upper end of the telegraph pole is inserted into the conical concave cavity, the power box mounting barrel is provided with an upper hoop outside the position corresponding to the concave cavity, a plurality of corresponding lower hollow vertical pipes are provided with a second upper hoop in the corresponding positions, the second upper hoop is fixedly connected with the lower hollow vertical pipes, the lower hollow vertical pipes are connected with the upper hoop through corresponding supporting rods, and the second upper hoop and the upper hoop are lower than the lowest point of the unmanned aerial vehicle. This preferred scheme is favorable to improving the stability of structure and the reliability of work.
Preferably, the lower end of the power box mounting barrel frame is fixed on the upper end of the telegraph pole by a hoop. This preferred scheme, the sound construction is reliable.
Preferably, the communication antenna A is fixedly arranged on the side wall of the power box mounting barrel frame.
Preferably, the two frames of the safety guard connecting frame provided with the rails are arched frames. This preferred scheme is convenient for in time get rid of the water droplet, improves the safety in utilization.
Preferably, the upper end parts of the plurality of lower hollow vertical pipes are located between the upper surface and the lower surface of the charging module, a supporting structure is arranged between the upper end parts of the lower hollow vertical pipes, the supporting structure comprises four length-adjustable supporting rods, and two ends of the four length-adjustable supporting rods are respectively connected with the upper end parts of the two lower hollow vertical pipes. This preferred scheme is favorable to improving the stability of structure.
In conclusion, the beneficial effects of the invention are as follows: the problem that the unmanned aerial vehicle needs to be frequently recovered to the hand to be charged manually in the using process can be well solved. The invention has reasonable structure and safe, reliable and convenient use.
Drawings
FIG. 1: the invention has a structure schematic diagram;
in the figure: unmanned aerial vehicle 1, wire pole 2, power supply box 3, the control unit 4, the module of charging 5, dull and stereotyped 5.1, communication antenna A6, power supply box installation bobbin cradle 7, safety guard subassembly 8, power supply box supporting shoe 9.
Detailed Description
The technical scheme of the invention is further specifically described by the following embodiments and the accompanying drawings.
The intelligent unmanned aerial vehicle comprises an unmanned aerial vehicle 1, a telegraph pole 2, a power box 3, a control unit 4, a charging module 5, a communication antenna A6, a power box mounting barrel frame 7, a safety guard assembly 8 and a power box supporting block 9. The power supply box 3, the control unit 4, the charging module 5 and the communication antenna a6 are provided at the upper end of the utility pole 2. The control unit 4 is connected with the power supply box 3, the charging module 5 and the communication antenna a 6. The unmanned aerial vehicle 1 is provided with a communication antenna B for communicating with the communication antenna a6, and a determination device for the remaining power and the distance to the charging device. The lower end of the power box mounting barrel frame 7 is sleeved and fixed at the upper end of the telegraph pole 2, the periphery of the upper end of the power box mounting barrel frame 7 is horizontally bent outwards to form a charging module mounting part, and the periphery of the charging module mounting part is further bent upwards. The charging module 5 is a wireless charging module, and comprises a flat plate 5.1 and a wireless charging head which is arranged on the flat plate 5.1 and is not shown in the figure; correspondingly, the unmanned aerial vehicle 1 is provided with a wireless receiving head not shown in the figure; the power box 3 and the control unit 4 are fixedly arranged at the upper end of the power box mounting barrel frame 7 in an insulating manner and are positioned below the wireless charging module. Preferably, the power box 3 is arranged below the control unit 4, the power box supporting block 9 is fixedly arranged between the lower part of the power box 3 and the upper end of the telegraph pole 2 in the power box mounting barrel frame 7, the lower end of the power box supporting block 9 is provided with a conical concave cavity matched with the upper end of the telegraph pole 2, and the upper end of the telegraph pole 2 is inserted into the conical concave cavity. The lower end of the power supply box mounting cartridge 7 is fixed to the upper end of the utility pole 2 with an anchor ear not shown in the drawings. Meanwhile, the power box mounting barrel frame 7 is provided with an upper hoop at a position corresponding to the conical cavity, the power box mounting barrel frame 7 is fixedly connected with the upper end of the telegraph pole 2 through the upper hoop, and the power box mounting barrel frame 7 is fixedly connected with the upper end of the telegraph pole 2 through the upper hoop; the corresponding position of a plurality of lower hollow vertical pipes is provided with a second upper hoop, the second upper hoop and the upper hoop are lower than the lowest point of the unmanned aerial vehicle, the second upper hoop is fixedly connected with the lower hollow vertical pipes, and the lower hollow vertical pipes are connected with the upper hoops through corresponding support rods. The communication antenna a6 is provided on the side wall of the power box mounting cartridge 7. The safety hood assembly 8 comprises a safety hood framework and a rainproof hood cloth. The lower end of the safety shield framework comprises four lower hollow vertical pipes, a large lower frame, a small lower frame and four lower frame connecting pipes. The two ends of the lower frame connecting pipe are fixedly connected with the large lower frame and the small lower frame respectively. The position of big, little lower frame is less than unmanned aerial vehicle 1's the lower extreme. The large lower frame is fixedly connected with the four lower hollow vertical pipes. The small lower frame is fixedly connected with the telegraph pole 2 and also fixedly connected with the lower end of the power box mounting barrel frame 7, when the small lower frame is fixedly connected with the lower end of the power box mounting barrel frame 7, the small lower frame is fixedly connected with the hoop for fixing the lower end of the power box mounting barrel frame 7 on the upper end of the telegraph pole 2 by the hoop or is of an integrated structure, and the small lower frame is fixedly connected with the telegraph pole 2 in the embodiment. In addition, in order to improve the structural stability, the upper end portions of the four lower hollow vertical pipes are located between the upper surface and the lower surface of the charging module, the upper ends of the four lower hollow vertical pipes are fixedly connected with a large upper frame, a supporting structure is arranged between the upper end portions of the four lower hollow vertical pipes, the supporting structure comprises four length-adjustable supporting rods, and the two ends of the four length-adjustable supporting rods are respectively connected with the upper end portions of the two lower hollow vertical pipes to form a square. And the rain-proof cover cloth receiving mechanism is arranged above the large lower frame and comprises a torsion spring and a rotating shaft, and the specific structural details are not described herein because of being a simple technology. The upper end of the safety shield framework comprises movable vertical pipes with the same number as the lower hollow vertical pipes and a safety shield connecting frame connected with the upper ends of the movable vertical pipes; the movable vertical pipes are inserted into the corresponding hollow vertical pipes, and the positions can be adjusted up and down during working. The rain cover cloth comprises side wall rain cover cloth and top cover rain cover cloth, the lower edge of the side wall rain cover cloth is connected with the rotating shaft, and the upper edge of the side wall rain cover cloth is connected with the safety cover connecting frame. A torsion spring and a torsion spring rotating shaft are arranged in one frame edge of the safety cover connecting frame, two side frame edges connected with the frame edge are provided with guide rails, sliding seats are arranged on the guide rails, and the two sliding seats are connected through sliding seat connecting rods. One side of the top cover rainproof cover cloth is connected with the torsion spring rotating shaft, and the other side of the top cover rainproof cover cloth is connected with the sliding seat connecting rod. The lifting and rolling movements of the side wall rainproof cover cloth and the tiling movement and rolling movement of the top cover rainproof cover cloth comprise linear motor mechanisms which are not shown in the figure, the linear motors are all connected with the control unit and the power box, and the specific structural details are not described herein because the linear motors are simple known technologies.
The above embodiments are merely preferred embodiments of the present invention, and not intended to limit the structure and scope of the invention. Indeed, many equivalent variations in the shapes, constructions and design objectives of the devices according to the present invention are possible. Therefore, all equivalent changes in the shapes, structures and design objectives of the present invention are intended to be covered by the present invention, and all such equivalent changes are intended to be protected by the present invention.

Claims (7)

1. The utility model provides an aerial charging device of unmanned aerial vehicle, includes unmanned aerial vehicle (1), wire pole (2), characterized by: the upper end of the telegraph pole (2) is fixedly provided with a power supply box (3), a control unit (4), a charging module (5), a communication antenna A (6), a power supply box mounting barrel frame (7) and a safety cover assembly (8); the control unit (4) is connected with the power box (3), the charging module (5) and the communication antenna A (6); the unmanned aerial vehicle (1) is provided with a communication antenna B which communicates with the communication antenna A (6), and a judging device of the distance between the surplus power and the charging device;
the lower end of the power box mounting barrel frame (7) is sleeved and fixed at the upper end of the telegraph pole (2), and the periphery of the upper end of the power box mounting barrel frame (7) is horizontally bent outwards to form a charging module mounting part; the power box (3) and the control unit (4) are fixedly arranged at the upper end of the power box mounting barrel frame (7) and below the wireless charging module;
the safety cover component (8) comprises a safety cover framework and a rainproof cover cloth; the lower end of the safety shield framework comprises a plurality of lower hollow vertical pipes, a large lower frame, a small lower frame and a plurality of lower frame connecting pipes; two ends of the lower frame connecting pipe are fixedly connected with the large lower frame and the small lower frame respectively; the positions of the large lower frame and the small lower frame are lower than the lowest end of the unmanned aerial vehicle (1); the large lower frame is fixedly connected with a plurality of lower hollow vertical pipes, and the small lower frame is fixedly connected with the telegraph pole (2); a rain-proof cover cloth accommodating mechanism is arranged above the large lower frame and comprises a torsion spring and a rotating shaft; the upper end of the safety shield framework comprises movable vertical pipes with the same number as the lower hollow vertical pipes and a safety shield connecting frame connected with the upper ends of the movable vertical pipes; the movable vertical pipes are inserted into the corresponding hollow vertical pipes, and the positions can be adjusted up and down when the movable vertical pipes work; the rain-proof cover cloth comprises side wall rain-proof cover cloth and top cover rain-proof cover cloth, the lower side of the side wall rain-proof cover cloth is connected with the rotating shaft, and the upper side of the side wall rain-proof cover cloth is connected with the safety cover connecting frame; a torsional spring and a torsional spring rotating shaft are arranged in one frame edge of the safety shield connecting frame, two side frame edges connected with the frame edge are provided with guide rails, sliding seats are arranged on the guide rails, and the two sliding seats are connected by a sliding seat connecting rod; one side of the top cover rainproof cover cloth is connected with the torsion spring rotating shaft, and the other side of the top cover rainproof cover cloth is connected with the sliding seat connecting rod.
2. The aerial charging device of unmanned aerial vehicle of claim 1, characterized by: the periphery of the charging module mounting part is bent upwards.
3. The aerial charging device of unmanned aerial vehicle of claim 2, characterized by: a power box supporting block (9) is fixedly arranged below the power box (3) of the power box mounting barrel frame (7), and the power box (3) is fixedly arranged below the control unit (4); the lower end of the power supply box supporting block (9) is provided with a conical concave cavity matched with the upper end of the telegraph pole (2), and the upper end of the telegraph pole (2) is inserted into the conical concave cavity; an upper hoop is arranged outside the part of the power box mounting barrel frame (7) corresponding to the concave cavity, and the power box mounting barrel frame (7) is fixedly connected with the upper end of the telegraph pole (2) through the upper hoop; the corresponding position of a plurality of lower hollow vertical pipes is provided with a second upper hoop, the second upper hoop is fixedly connected with the lower hollow vertical pipes, the lower hollow vertical pipes are connected with the upper hoops through corresponding support rods, and the second upper hoop and the upper hoops are lower than the lowest point of the unmanned aerial vehicle.
4. The aerial charging device of unmanned aerial vehicle of claim 2, characterized by: the lower end of the power box mounting barrel frame (7) is fixed at the upper end of the telegraph pole (2) by a hoop.
5. The aerial charging device of unmanned aerial vehicle of claim 2, characterized by: the communication antenna A (6) is fixedly arranged on the side wall of the power box mounting barrel frame (7).
6. An aerial charging device for unmanned aerial vehicles according to any one of claims 1-5, wherein: the two frames of the safety cover connecting frame provided with the tracks are arched frames.
7. An aerial charging device for unmanned aerial vehicles according to any one of claims 1-5, wherein: the upper end parts of the lower hollow vertical pipes are located between the upper surface and the lower surface of the charging module, a supporting structure is arranged between the upper end parts of the lower hollow vertical pipes, the supporting structure comprises four length-adjustable supporting rods, and two ends of the four length-adjustable supporting rods are respectively connected with the upper end parts of the two lower hollow vertical pipes.
CN201710608093.XA 2017-07-24 2017-07-24 Aerial charging device of unmanned aerial vehicle Active CN107696882B (en)

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Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
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CN107696882B true CN107696882B (en) 2020-03-24

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Publication number Priority date Publication date Assignee Title
JP2006048483A (en) * 2004-08-06 2006-02-16 Toyota Motor Corp Power source device, method of correcting incoming and outgoing of power thereof, and method of estimating current-voltage characteristic of power source
JP2007128778A (en) * 2005-11-04 2007-05-24 Toyota Motor Corp Fuel cell system, its control method, and vehicle mounting it
CN202929383U (en) * 2012-09-11 2013-05-08 深圳一电科技有限公司 Unmanned plane and automatic charging system thereof
CN203982395U (en) * 2014-07-23 2014-12-03 潘若愚 Electric drive unmanned plane is stopped maintenance system
CN105471073A (en) * 2015-12-30 2016-04-06 天津天瑞达自动化设备有限公司 Intelligent charging apparatus
CN106026261B (en) * 2016-06-24 2018-03-16 国网安徽省电力公司黄山供电公司 The remote patrol UAV charging station of electric power
CN106685001B (en) * 2017-01-16 2019-06-21 北京交通大学 Charging system is affiliated to for multi-rotor unmanned aerial vehicle
CN207128651U (en) * 2017-07-24 2018-03-23 国网浙江海宁市供电公司 A kind of aerial charging device of unmanned plane

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