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

Aerial charging device of unmanned aerial vehicle Download PDF

Info

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
Authority
CN
China
Prior art keywords
frame
power box
unmanned aerial
charging device
aerial vehicle
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.)
Active
Application number
CN201710608093.XA
Other languages
Chinese (zh)
Other versions
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
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.)
Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
Original Assignee
Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
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 Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd filed Critical Haining Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
Priority to CN201710608093.XA priority Critical patent/CN107696882B/en
Publication of CN107696882A publication Critical patent/CN107696882A/en
Application granted granted Critical
Publication of CN107696882B publication Critical patent/CN107696882B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION 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
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION 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
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

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)

1.一种无人机空中充电装置，包括无人机（1），电线杆（2），其特征是：电线杆（2）的上端固设有一个电源箱（3），控制单元（4），充电模块（5），通信天线A（6），电源箱安装筒架（7）和安全罩组件（8）；控制单元（4）和电源箱（3）、充电模块（5）、通信天线A（6）相连；无人机（1）上设有和通信天线A（6）进行通信的通信天线B，以及剩余电力和与充电装置之间的距离的判断装置；1. An aerial charging device for unmanned aerial vehicles, comprising an unmanned aerial vehicle (1) and a utility pole (2), characterized in that a power supply box (3) is fixed on the upper end of the utility pole (2), and a control unit (4) ), the charging module (5), the communication antenna A (6), the power box mounting drum holder (7) and the safety cover assembly (8); the control unit (4) and the power box (3), the charging module (5), the communication The antenna A (6) is connected; the drone (1) is provided with a communication antenna B that communicates with the communication antenna A (6), and a judging device for remaining power and the distance from the charging device; 电源箱安装筒架（7）的下端套置固定在电线杆（2）的上端，电源箱安装筒架（7）的上端的四周水平向外折弯构成充电模块安装部；电源箱（3）和控制单元（4）固设于电源箱安装筒架（7）的上端、无线充电模块的下方；The lower end of the power box installation cylinder frame (7) is sleeved and fixed on the upper end of the utility pole (2), and the upper end of the power box installation cylinder frame (7) is horizontally bent outward to form the charging module installation part; the power box (3) and the control unit (4) are fixed on the upper end of the power box installation cylinder frame (7) and below the wireless charging module; 安全罩组件（8）包括安全罩骨架和防雨罩布；安全罩骨架的下端包括若干下空心竖管、一大下边框、一小下边框及若干下边框连接管；下边框连接管的两端分别和大、小下边框固连；大、小下边框的位置低于无人机（1）的最下端；大下边框和若干下空心竖管固连，小下边框和电线杆（2）固连；大下边框上方设有防雨罩布收纳机构，所述防雨罩布收纳机构包括扭簧和转轴；安全罩骨架的上端包括和下空心竖管根数相同的活动竖管以及一个和各活动竖管上端相连的安全罩连接框；活动竖管插置在相应的空心竖管内，工作时位置可上下调节；防雨罩布包括侧围防雨罩布和顶盖防雨罩布，侧围防雨罩布的下边和转轴相连，侧围防雨罩布的上边和安全罩连接框相连；安全罩连接框的一个框边里设有扭簧及扭簧转轴，与该框边相连的两个侧框边设有导轨，导轨上设有滑座，两个滑座用滑座连杆相连；顶盖防雨罩布的一边和扭簧转轴相连，另一边和滑座连杆相连。The safety cover assembly (8) includes a safety cover frame and a rain cover cloth; the lower end of the safety cover frame includes a plurality of lower hollow vertical pipes, a large lower frame, a small lower frame and a plurality of lower frame connecting pipes; The ends are respectively fixed to the large and small lower frames; the positions of the large and small lower frames are lower than the lowermost end of the drone (1); ) fixedly connected; a rain cover cloth storage mechanism is arranged above the large lower frame, and the rain cover cloth storage mechanism includes a torsion spring and a rotating shaft; the upper end of the safety cover frame includes the same number of movable vertical pipes as the lower hollow vertical pipes and A safety cover connection frame connected to the upper end of each movable standpipe; the movable standpipe is inserted into the corresponding hollow standpipe, and the position can be adjusted up and down during operation; the rain cover cloth includes the side wall rain cover cloth and the top cover rain cover cloth, the lower side of the side wall rain cover cloth is connected with the rotating shaft, and the upper side of the side wall rain cover cloth is connected with the safety cover connecting frame; a frame edge of the safety cover connecting frame is provided with a torsion spring and a torsion spring rotating shaft, which is connected with the frame. There are guide rails on the sides of the two side frames connected to each other, and a sliding seat is arranged on the guide rail. The two sliding seats are connected by a sliding seat connecting rod; rods are connected. 2.根据权利要求1所述的无人机空中充电装置，其特征是：充电模块安装部的四周向上折弯。2 . The aerial charging device for unmanned aerial vehicles according to claim 1 , wherein the periphery of the mounting portion of the charging module is bent upwards. 3 . 3.根据权利要求2所述的无人机空中充电装置，其特征是：电源箱安装筒架（7）在电源箱（3）的下方固设有电源箱支撑块（9），电源箱（3）固设于控制单元（4）的下方；电源箱支撑块（9）的下端设有一个和电线杆（2）的上端适配的锥形凹腔，电线杆（2）的上端插置在所述锥形凹腔内；电源箱安装筒架（7）在与所述凹腔相应的部位外设有上抱箍，电源箱安装筒架（7）和电线杆（2）上端用上抱箍固连；相应的若干下空心竖管在对应的位置设有第二上抱箍，所述第二上抱箍和下空心竖管固连，下空心竖管又通过相应的支撑杆和上抱箍相连，所述第二上抱箍、上抱箍均低于无人机的最低点。3. The aerial charging device for unmanned aerial vehicles according to claim 2, characterized in that: the power box installation cylinder frame (7) is fixedly provided with a power box support block (9) below the power box (3), and the power box ( 3) It is fixed below the control unit (4); the lower end of the power box support block (9) is provided with a conical cavity that fits with the upper end of the utility pole (2), and the upper end of the utility pole (2) is inserted In the conical cavity; the power box installation cylinder frame (7) is provided with an upper hoop outside the corresponding part of the cavity, and the power box installation cylinder frame (7) and the upper end of the utility pole (2) are used for The hoop is fixedly connected; the corresponding several lower hollow standpipes are provided with a second upper hoop at the corresponding position, the second upper hoop and the lower hollow standpipe are fixedly connected, and the lower hollow standpipe passes through the corresponding support rod and the lower hollow standpipe. The upper hoop is connected, and the second upper hoop and the upper hoop are both lower than the lowest point of the drone. 4.根据权利要求2所述的无人机空中充电装置，其特征是：电源箱安装筒架（7）的下端用抱箍固定在电线杆（2）的上端。4. The aerial charging device for unmanned aerial vehicles according to claim 2, characterized in that: the lower end of the power box installation cylinder frame (7) is fixed on the upper end of the utility pole (2) with a hoop. 5.根据权利要求2所述的无人机空中充电装置，其特征是：通信天线A（6）固设于电源箱安装筒架（7）的侧壁上。5 . The aerial charging device for unmanned aerial vehicles according to claim 2 , wherein the communication antenna A ( 6 ) is fixedly installed on the side wall of the power box installation cylinder frame ( 7 ). 6 . 6.根据权利要求1-5任意一项所述的无人机空中充电装置，其特征是：安全罩连接框中设有轨道的两个边框为拱形边框。6 . The aerial charging device for unmanned aerial vehicles according to claim 1 , wherein the two frames provided with the rails in the connection frame of the safety cover are arched frames. 7 . 7.根据权利要求1-5任意一项所述的无人机空中充电装置，其特征是：若干下空心竖管的上端端部位于充电模块上下表面之间，且下空心竖管的上端端部之间设有支撑结构，所述支撑结构包括四根长度可调撑杆，四根长度可调撑杆的两端分别和两根下空心竖管的上端端部相连。7. The aerial charging device for unmanned aerial vehicles according to any one of claims 1-5, wherein the upper ends of the plurality of lower hollow risers are located between the upper and lower surfaces of the charging module, and the upper ends of the lower hollow risers are located between the upper and lower surfaces of the charging module. A support structure is arranged between the parts, and the support structure includes four length-adjustable struts, and two ends of the four length-adjustable struts are respectively connected with the upper ends 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)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710608093.XA CN107696882B (en) 2017-07-24 2017-07-24 Aerial charging device of unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710608093.XA CN107696882B (en) 2017-07-24 2017-07-24 Aerial charging device of unmanned aerial vehicle

Publications (2)

Publication Number Publication Date
CN107696882A CN107696882A (en) 2018-02-16
CN107696882B true CN107696882B (en) 2020-03-24

Family

ID=61170741

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710608093.XA Active CN107696882B (en) 2017-07-24 2017-07-24 Aerial charging device of unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN107696882B (en)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006048483A (en) * 2004-08-06 2006-02-16 Toyota Motor Corp Power supply device, power balance correction method thereof, and current-voltage characteristic estimation method of power supply
JP2007128778A (en) * 2005-11-04 2007-05-24 Toyota Motor Corp Fuel cell system, control method thereof, and vehicle equipped with the same
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 Docked charging system for multi-rotor UAV
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

Also Published As

Publication number Publication date
CN107696882A (en) 2018-02-16

Similar Documents

Publication Publication Date Title
CN109638718B (en) Inspection robot for overhead transmission line
CN109279041B (en) Multifunctional unmanned aerial vehicle flight platform
CN211441970U (en) Many rotor unmanned aerial vehicle's suspension type platform that charges
CN211893686U (en) A fully automatic power inspection drone service desk
CN204967048U (en) Take shockproof electric power cabinet of base
CN209930518U (en) Vehicle mobile tethered balloon emergency communication base station
CN213027174U (en) Unmanned system of patrolling and examining of transformer substation of land-air outdoor scene perception
CN107696882B (en) Aerial charging device of unmanned aerial vehicle
CN108336798B (en) Charging station
CN205168930U (en) Multi -functional nacelle of many rotor unmanned aerial vehicle
CN213036090U (en) Follow-on airborne laser radar equipment based on unmanned aerial vehicle
CN207128651U (en) A kind of aerial charging device of unmanned plane
CN215794484U (en) Be used for surveying and mapping unmanned aerial vehicle protection device
CN109001090A (en) A kind of dust on the roads monitoring device with wireless transmission function
CN206060310U (en) The remote line walking unmanned plane charging device of electric power
CN116692049A (en) Electric power high-voltage line check out test set
CN113060021B (en) UAV wireless charging platform transmitter and receiver coil equipment
CN106657909A (en) Novel vehicle insurance loss assessment system in traffic accident
CN206107581U (en) Complementary power generation system of unmanned aerial vehicle scene
CN207060414U (en) A kind of new unmanned plane applied to power system inspection
CN106780051A (en) Vehicle insurance loss assessment system in traffic accident
CN114771813A (en) A kind of unmanned aerial vehicle monitoring device and monitoring method for bottom building
CN208190685U (en) A kind of multi-rotor aerocraft service network
CN216700174U (en) A mobile solar wireless monitoring pole
CN222310926U (en) Multi-rotor unmanned aerial vehicle equipment for operation and maintenance work of power transmission line

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant