WO2023184975A1 - 一种无人机自动充电机库、系统及巡检方法 - Google Patents

一种无人机自动充电机库、系统及巡检方法 Download PDF

Info

Publication number
WO2023184975A1
WO2023184975A1 PCT/CN2022/129173 CN2022129173W WO2023184975A1 WO 2023184975 A1 WO2023184975 A1 WO 2023184975A1 CN 2022129173 W CN2022129173 W CN 2022129173W WO 2023184975 A1 WO2023184975 A1 WO 2023184975A1
Authority
WO
WIPO (PCT)
Prior art keywords
hangar
control module
centering
door
uav
Prior art date
Application number
PCT/CN2022/129173
Other languages
English (en)
French (fr)
Inventor
蔡杨华
陈凯旋
熊智
王冠
易琳
吴昊
麦晓明
鲁虹
张晓晔
Original Assignee
南方电网电力科技股份有限公司
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 南方电网电力科技股份有限公司 filed Critical 南方电网电力科技股份有限公司
Publication of WO2023184975A1 publication Critical patent/WO2023184975A1/zh

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
    • B60L53/30—Constructional details of charging stations
    • 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
    • B60L53/30—Constructional details of charging stations
    • B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01W—METEOROLOGY
    • G01W1/00—Meteorology
    • G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
    • 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
    • Y02T90/12—Electric charging stations

Definitions

  • the invention relates to the technical field of unmanned aerial vehicles, and in particular to an automatic charging hangar, system and inspection method for unmanned aerial vehicles.
  • UAVs are used in fields such as electric power, surveying and mapping, forestry, agriculture, etc., and have broad application prospects.
  • the current manual drone inspection method requires time and cost to train pilots.
  • the threshold for drone operation is high, which limits the promotion of drone technology.
  • UAV automatic inspection refers to the process in which the UAV can take off on its own, complete outdoor line inspections and land on its own according to preset parameters such as time, route and work tasks.
  • the development of the infrastructure required for automatic drone inspection technology, namely the drone hangar is still relatively slow and cannot achieve precise positioning and automatic charging of drones.
  • the invention provides an automatic UAV charging hangar, system and inspection method, which solves the technical problem that the existing UAV hangar cannot achieve precise positioning and automatic charging of the UAV.
  • a first aspect of the invention provides an automatic charging hangar for a drone, which includes a hangar shell, a hangar door, a hangar door drive module, a centering module and a control module;
  • the hangar door is arranged on the top of the hangar shell and is connected to the hangar door drive module; the hangar door drive module is connected to the control module and is used to drive the machine according to the instructions of the control module.
  • the re-centering module is arranged inside the hangar shell, and includes a landing and parking plate for carrying the UAV, a re-centering device and a charging device; the landing and parking plate is provided with a space for visual identification of the UAV. Positioning tag; the re-centering device is used to re-center the UAV on the landing and parking board to a preset position according to the instruction of the control module, so that the UAV on the landing and parking board is aligned with the The charging device is docked.
  • the centering device includes four centering axes, and the four centering axes are respectively the first centering X-axis, the second centering X-axis, and the third centering axis.
  • the first central Y-axis and the second central Y-axis, one end of each central axis is connected to a sliding unit, and the other end of each central axis is connected to another sliding unit; between two adjacent sliding units Connect the drive unit so that the corresponding centering axis can be moved back to center under the driving of the drive unit.
  • the sliding unit includes a first coupling, a fixed block, a first travel switch, a slide block, a slide rail, a second travel switch and a screw.
  • the slide block The connecting block is connected to the corresponding central shaft; the power input end of the first coupling is connected to the corresponding drive unit, and the power output end of the first coupling is connected to the screw; the slider is configured on the slide rail and connected to the screw rod to slide along the slide rail driven by the rotation of the screw rod; the first travel switch and the second travel switch are used to detect whether the slider Reach the set position, and control the corresponding drive unit to stop after reaching the set position.
  • the drive unit includes a recentering motor, a first reducer, a first one-to-two synchronous coupling and a second one-to-two synchronous coupling connected in sequence. , the second one-to-two synchronous coupling is connected to the coupling.
  • the hangar door includes a flip cover
  • the hangar door drive module includes a rotating motor, a second reducer, and a third one-to-two synchronous coupling connected in sequence.
  • a shaft and a second coupling the second coupling is connected to the flip cover.
  • the automatic drone charging hangar further includes an air conditioner; the air conditioner is provided in the hangar shell and connected to the control module.
  • an access door is provided on the side of the hangar shell, the control module is adjacent to the access door, and the control module is carried by a support bottom plate, and the support bottom plate There are guide rails slidingly connected on both sides.
  • a second aspect of the present invention provides an automatic charging system for drones, including a weather monitoring device and an automatic charging hangar for drones as described in any of the above implementable ways;
  • the weather monitoring device is communicatively connected to the control module.
  • the weather monitoring device includes a signal enhancement and power supply box, a weather station support plate, a weather station, an antenna and a pillar.
  • the signal enhancement and power supply box, weather station support plate and The antenna is arranged on the pillar, wherein the antenna is located on the top of the pillar, and the weather station is arranged on the weather station support plate.
  • a third aspect of the present invention provides an inspection method for an automatic UAV charging hangar.
  • the method is based on the UAV automatic charging hangar described in any of the above implementable ways.
  • the method includes:
  • the control module receives the route information of the drone inspection sent by the drone dispatching system.
  • the route information includes take-off time, inspection task information and return time;
  • control module sends flight instructions to the UAV on the landing board according to the inspection task information, and sends an opening instruction to the hangar door drive module to open the hangar door.
  • an opening command is sent to the re-centering device to separate the drone from the charging device;
  • control module After the drone flies out of the hangar shell, the control module sends a closing command to the hangar door drive module to close the hangar door;
  • control module When the return time is reached, the control module sends a door-opening command to the hangar door drive module to open the hangar door, and at the same time sends a re-centering command to the re-centering device to connect the drone to the charging device. docking to charge the drone;
  • control module After the re-centering device completes executing the re-centering instruction, the control module sends a closing instruction to the hangar door driving module to close the hangar door.
  • the method further includes:
  • the control module receives the inspection results uploaded by the drone
  • the control module sends the inspection results to the UAV dispatching system.
  • the automatic charging hangar for drones of the present invention includes a hangar shell, a hangar door, a hangar door drive module, a centering module and a control module; the hangar door is arranged on the top of the hangar shell and is connected to the hangar door.
  • the drive module is connected; the hangar door drive module is connected to the control module, and is used to drive the opening and closing of the hangar door according to the instructions of the control module; the centering module is arranged inside the hangar shell , which includes a landing and stopping board for carrying the drone, a re-centering device and a charging device; the landing and stopping board is provided with a label for visual identification and positioning of the drone; the re-centering device is used to carry out the drone according to the According to the instructions of the control module, the UAV on the landing and parking board is moved back to the preset position so that the UAV on the landing and parking board can be docked with the charging device; the present invention realizes the charging of the UAV.
  • the control module also communicates with the drone dispatching system Connection enables automatic inspection of drones.
  • Figure 1 is a schematic diagram of the external structure of an automatic drone charging hangar (with a drone) provided by an optional embodiment of the present invention
  • Figure 2 is a schematic diagram of the internal structure of an automatic drone charging hangar (with a drone) provided by an optional embodiment of the present invention
  • Figure 3 is a schematic structural diagram of a re-centering module provided by an optional embodiment of the present invention.
  • Figure 4 is a schematic structural diagram of a sliding unit provided by an optional embodiment of the present invention.
  • Figure 5 is a schematic structural diagram of a hangar door drive module provided by an optional embodiment of the present invention.
  • Figure 6 is a schematic structural diagram of a weather monitoring device provided by an optional embodiment of the present invention.
  • Figure 7 is a flow chart of an inspection method for an automatic drone charging hangar provided by an optional embodiment of the present invention.
  • Embodiments of the present invention provide an automatic drone charging hangar, system and inspection method, which are used to solve the technical problem that existing drone hangars cannot achieve precise positioning and automatic charging of drones.
  • the invention provides an automatic charging hangar for a drone.
  • Figure 1 shows a schematic diagram of the external structure of an automatic drone charging hangar (with a drone 5) provided by an embodiment of the present invention.
  • An embodiment of the present invention provides an automatic charging hangar for a drone, which includes a hangar shell 1, a hangar door 2, a hangar door drive module 3, a centering module 4 and a control module 9.
  • the bottom of the hangar shell 1 is provided with a tripod 101, and its side is also provided with an access door 102.
  • the hangar shell 1 is supported by a frame 6 .
  • the hangar door 2 is provided on the top of the hangar shell 1 and includes a left flip cover 201 and a right flip cover 202 .
  • the hangar door 2 is connected to the hangar door drive module 3, and the hangar door drive module 3 is connected to the control module 9, and is used to drive the opening and closing of the hangar door 2 according to the instructions of the control module 9. .
  • the re-centering module 4 is provided inside the hangar shell 1, and includes a landing stop plate 413 for carrying the UAV 5, a re-centering device and a charging device 405;
  • the landing stop plate 413 is provided with a label for the drone 5 to visually identify and locate.
  • the label is a two-dimensional code.
  • the re-centering device is used to re-center the UAV 5 on the landing and stopping plate 413 to a preset position according to the instruction of the control module 9, so that the UAV 5 on the landing and stopping plate 413 can Connect with the charging device 405 .
  • the back-to-center device includes four back-to-center axes, and the four back-to-center axes are respectively the first return center X-axis 406, the second return center X-axis 407, the first return center Y-axis 410, and the second return center Y-axis.
  • Shaft 411, one end of each back-to-center shaft is connected to a sliding unit 409, and the other end of each back-to-center shaft is connected to another sliding unit 409; a driving unit 404 is connected between two adjacent sliding units 409, so as to The corresponding back-to-center axis is moved back to center under the driving of the driving unit 404.
  • the sliding unit 409 includes a first coupling 491, a fixed block 492, a first travel switch 494, a sliding block 495, a sliding rail 496, a second travel switch 498 and a screw 499.
  • the sliding block 495 is connected to the corresponding central shaft through the connecting block 408; the power input end of the first coupling 491 is connected to the corresponding drive unit 404, and the power output end of the first coupling 491 is connected to the screw 499 ;
  • the slider 495 is disposed on the slide rail 496 and connected to the screw 499 to slide along the slide rail 496 driven by the rotation of the screw 499; the first travel switch 494 and the The second travel switch 498 is used to detect whether the slider 495 reaches the set position, and to control the corresponding driving unit 404 to stop after reaching the set position.
  • the sliding unit 409 further includes a first limit switch support 493 for carrying the first limit switch 494, and a second limit switch support 497 for carrying the second limit switch 498.
  • the driving unit 404 includes a centering motor 401, a first reducer 412, a first one-to-two synchronous coupling 402 and a second one-to-two synchronous coupling 403 connected in sequence.
  • the second one-to-two synchronous coupling Coupling 403 is connected to the coupling.
  • the power transmitted from the centering motor 401 is input to the screw 499 through the first coupling 491.
  • the rotation of the screw 499 drives the slide block 495 to slide along the slide rail 496 to achieve rotation to translation movement.
  • the first travel switch 494 and the second travel switch 498 mainly detect whether the slider 495 reaches the set position. After reaching the designated position, the return motor 401 stops operating.
  • the hangar door drive module 3 includes a rotating motor 301, a second reducer 302, a third one-to-two synchronous coupling 303, and a shaft 304 connected in sequence. and second coupling 305.
  • One end of the shaft 304 is connected to the left flip cover 201 through the second coupling 305, and the other end is connected to the right flip cover 202 through the second coupling 305. Due to the gravitational moment of the flip cover, the output torque of the motor needs to match the torque corresponding to the rotation angle of the flip cover. The size of the output torque needs to match the change of the gravitational moment to achieve stable rotation of the flip cover.
  • the flip structure of the hangar door 2 can be smoothly rotated, thereby realizing the opening and closing of the hangar door 2.
  • the hangar door 2 is opened when the UAV 5 takes off and lands, and the hangar door 2 is closed during the rest of the time to protect the UAV 5 and the internal equipment of the hangar.
  • the drone automatic charging hangar in order to realize automatic control of the above-mentioned recentering motor 401 and rotation motor 301, the drone automatic charging hangar also includes a corresponding motor controller 11 to realize stability control of the corresponding motor.
  • the automatic drone charging hangar further includes an air conditioner 7 ; the air conditioner 7 is provided in the hangar shell 1 and connected to the control module 9 .
  • the air conditioner 7 can adjust the internal temperature of the hangar to avoid failures caused by temperature factors.
  • the UAV automatic charging hangar is also equipped with a power adapter module 8 and a UPS power supply 10.
  • the power adapter module 8 mainly converts the input voltage into the voltage level corresponding to each device, so that each device can be adapted.
  • the UPS power supply 10 is a buffer power supply inside the hangar and can provide emergency power when external power is cut off.
  • control module 9 is adjacent to the access door 102 , and the control module 9 is carried by a support bottom plate 103 , and guide rails 104 are slidingly connected to both sides of the support bottom plate 103 .
  • the supporting bottom plate 103 is also used to carry the above-mentioned power adapter module 8, UPS power supply 10 and motor controller 11.
  • the support bottom plate 103 can be moved along the guide rail 104 by pushing and pulling the support bottom plate 103, thereby facilitating maintenance personnel to repair the devices on the support bottom plate 103 and achieving rapid positioning and maintenance work.
  • the present invention also provides an automatic charging system for UAV 5, which includes a weather monitoring device and an automatic UAV charging hangar as described in any of the above embodiments.
  • Figure 6 shows a schematic structural diagram of a weather monitoring device provided by an optional embodiment of the present invention.
  • the weather monitoring device of the embodiment of the present invention is connected to the control module 9 through communication.
  • the weather monitoring device includes a signal enhancement and power supply box 12, a weather station support plate 13, a weather station 14, an antenna 14 and a support column 16.
  • the signal enhancement device The power box 12 , the weather station support plate 13 and the antenna 15 are arranged on the pillar 16 , wherein the antenna 15 is located on the top of the pillar 16 , and the weather station 14 is arranged on the weather station support plate 13 .
  • the UAV automatic charging hangar and the signal weather station 14 are connected using optical fiber, wireless and other communication methods to realize the communication connection between the hangar and the signal weather station 14.
  • the weather station 14 is installed on the weather station support plate 13 and can detect the meteorological conditions of the surrounding environment, and then determine whether the ambient weather is suitable for the flight of the UAV 5 to avoid malfunction and damage of the UAV 5 caused by weather.
  • the signal enhancement and power supply box 12 mainly provides power for the weather station 14 and a signal enhancement device for the antenna 15 .
  • the present invention also provides an inspection method for an automatic UAV charging hangar, which method is based on the automatic UAV charging hangar described in any of the above embodiments.
  • Figure 7 shows a flow chart of an inspection method for an automatic drone charging hangar provided by an optional embodiment of the present invention.
  • An embodiment of the present invention provides an inspection method for an automatic drone charging hangar, including:
  • Step S1 the control module 9 receives the route information of the UAV 5 inspection sent by the UAV 5 dispatching system.
  • the route information includes take-off time, inspection task information and return time;
  • Step S2 when the take-off time is reached, the control module 9 sends a flight command to the UAV 5 on the landing board 413 according to the inspection task information, and sends a door opening command to the hangar door drive module 3 to open the door. Open the hangar door 2 and simultaneously send an opening command to the re-centering device to separate the drone 5 from the charging device 405;
  • Step S3 after the drone 5 flies out of the hangar shell 1, the control module 9 sends a closing command to the hangar door drive module 3 to close the hangar door 2;
  • Step S4 when the return time is reached, the control module 9 sends an opening instruction to the hangar door driving module 3 to open the hangar door 2, and at the same time sends a centering instruction to the centering device to cause the hangar door to open.
  • the drone 5 is docked with the charging device 405 to charge the drone 5;
  • Step S5 After the re-centering device completes executing the re-centering instruction, the control module 9 sends a closing instruction to the hangar door driving module 3 to close the hangar door 2.
  • the method also includes:
  • the control module 9 receives the inspection results uploaded by the drone 5;
  • the control module 9 sends the inspection results to the UAV 5 dispatching system.
  • the above embodiments of the present invention realize the precise positioning and automatic charging of the UAV 5, and communicate with the weather monitoring device through the control module 9 to control the flight of the UAV 5 according to the meteorological conditions of the surrounding environment, thereby improving the efficiency of the UAV 5.
  • the control module 9 is also connected to the UAV 5 dispatching system, which can realize the automatic inspection of the UAV 5.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Environmental & Geological Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Atmospheric Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Ecology (AREA)
  • Environmental Sciences (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

公开了一种无人机自动充电机库、系统及巡检方法。该无人机自动充电机库包括机库外壳（1）、机库门（2）、机库门驱动模块（3）、回中模块（4）和控制模块（9），机库门驱动模块用于根据控制模块的指令驱动机库门的开闭，回中模块包括用于承载无人机（5）的降落停机板（413）、回中装置以及充电装置（405），降落停机板上设有供无人机进行视觉识别定位的标签，回中装置用于根据控制模块的指令，将降落停机板上的无人机回中移动至预设位置，以使无人机与充电装置对接。该机库实现了无人机的精准定位及自动充电，且通过控制模块与气象监测装置通讯，提高了无人机巡检的稳定性，通过控制模块与无人机调度系统连接，能够实现无人机的自动巡检。

Description

一种无人机自动充电机库、系统及巡检方法
本申请要求于2022年03月29日提交中国专利局、申请号为202210318866.1、发明名称为“一种无人机自动充电机库、系统及巡检方法”的中国专利申请的优先权，其全部内容通过引用结合在本申请中。
技术领域
本发明涉及无人机技术领域，尤其涉及一种无人机自动充电机库、系统及巡检方法。
背景技术
无人机应用于电力、测绘、林业、农业等领域，具有广阔的应用前景。目前人工操作无人机巡检方式需要投入对飞手培养的时间和成本，无人机操作门槛较高，限制了无人机技术的推广。
现有技术中利用无人机自动巡检技术解决人工操作无人机巡检方式的弊端。无人机自动巡检是指无人机能够按照预先设定的时间、路线和工作任务等参数进行自行起飞、自行完成户外巡线工作和自行降落的过程。然而，无人机自动巡检技术所需用到的基础设施即无人机机库的发展还比较缓慢，不能实现无人机的精准定位及自动充电。
发明内容
本发明提供了一种无人机自动充电机库、系统及巡检方法，解决了现有无人机机库不能实现无人机的精准定位及自动充电的技术问题。
本发明第一方面提供一种无人机自动充电机库，包括机库外壳、机库门、机库门驱动模块、回中模块和控制模块；
所述机库门设置于所述机库外壳的顶部，其与机库门驱动模块连接；所述机库门驱动模块连接所述控制模块，用于根据所述控制模块的指令驱动所述机库门的开闭；
所述回中模块设置于所述机库外壳的内部，其包括用于承载无人机的降落停机板、回中装置以及充电装置；所述降落停机板上设有供无人机进 行视觉识别定位的标签；所述回中装置用于根据所述控制模块的指令，将所述降落停机板上的无人机回中移动至预设位置，以使所述降落停机板上的无人机与所述充电装置对接。
根据本发明第一方面的一种能够实现的方式，所述回中装置包括四个回中轴，所述四个回中轴分别为第一回中X轴、第二回中X轴、第一回中Y轴和第二回中Y轴，每个所述回中轴的一端连接一滑动单元，每个所述回中轴的另一端连接另一滑动单元；两相邻滑动单元之间连接驱动单元，以在驱动单元的驱动下对相应的回中轴进行回中移动。
根据本发明第一方面的一种能够实现的方式，所述滑动单元包括第一联轴器、固定块、第一行程开关、滑块、滑轨、第二行程开关以及螺杆，所述滑块通过连接块与对应的回中轴连接；所述第一联轴器的动力输入端与对应的驱动单元连接，所述第一联轴器的动力输出端连接所述螺杆；所述滑块设置于所述滑轨上并与所述螺杆连接，以在所述螺杆的旋转带动下沿所述滑轨滑动；所述第一行程开关以及所述第二行程开关用于检测所述滑块是否到达设定位置，并在到达设定位置后控制相应的驱动单元停止动作。
根据本发明第一方面的一种能够实现的方式，所述驱动单元包括依次连接的回中电机、第一减速器、第一一分二同步联轴器和第二一分二同步联轴器，所述第二一分二同步联轴器与所述联轴器连接。
根据本发明第一方面的一种能够实现的方式，所述机库门包括翻盖，所述机库门驱动模块包括依次连接的转动电机、第二减速器、第三一分二同步联轴器、轴和第二联轴器，所述第二联轴器与所述翻盖连接。
根据本发明第一方面的一种能够实现的方式，所述无人机自动充电机库还包括空调；所述空调设置于所述机库外壳内，并与所述控制模块连接。
根据本发明第一方面的一种能够实现的方式，所述机库外壳的侧部设有检修门，所述控制模块临近所述检修门，所述控制模块由支撑底板承载，所述支撑底板两侧滑动连接有导轨。
本发明第二方面提供一种无人机自动充电系统，包括气象监测装置以及如上任意一项能够实现的方式所述的无人机自动充电机库；
所述气象监测装置与所述控制模块通讯连接，所述气象监测装置包括信号增强及电源箱、气象站支撑板、气象站、天线以及支柱，所述信号增强及电源箱、气象站支撑板和天线设置于所述支柱上，其中所述天线位于所述支柱的顶部，所述气象站设置于所述气象站支撑板上。
本发明第三方面提供一种无人机自动充电机库的巡检方法，所述方法基于如上任意一项能够实现的方式所述的无人机自动充电机库，所述方法包括：
控制模块接收无人机调度系统发送的无人机巡检的航线信息，所述航线信息包括起飞时间、巡检任务信息以及返回时间；
在达到起飞时间时，所述控制模块根据所述巡检任务信息向降落停机板上的无人机发送飞行指令，并向所述机库门驱动模块发送开门指令以开启所述机库门，同时向所述回中装置发送打开指令以使所述无人机与充电装置分离；
在所述无人机飞出机库外壳后，所述控制模块向所述机库门驱动模块发送关门指令以关闭所述机库门；
在达到返回时间时，所述控制模块向所述机库门驱动模块发送开门指令以开启所述机库门，同时向所述回中装置发送回中指令以使所述无人机与充电装置对接，从而为无人机充电；
在所述回中装置执行所述回中指令完毕后，所述控制模块向所述机库门驱动模块发送关门指令以关闭所述机库门。
根据本发明第三方面的一种能够实现的方式，所述方法还包括：
所述控制模块接收所述无人机上传的巡检结果；
所述控制模块将所述巡检结果发送至所述无人机调度系统。
从以上技术方案可以看出，本发明具有以下优点：
本发明的无人机自动充电机库包括机库外壳、机库门、机库门驱动模块、回中模块和控制模块；机库门设置于所述机库外壳的顶部，其与机库门驱动模块连接；所述机库门驱动模块连接所述控制模块，用于根据所述控制模块的指令驱动所述机库门的开闭；所述回中模块设置于所述机库外壳的内部，其包括用于承载无人机的降落停机板、回中装置以及充电装置； 所述降落停机板上设有供无人机进行视觉识别定位的标签；所述回中装置用于根据所述控制模块的指令，将所述降落停机板上的无人机回中移动至预设位置，以使所述降落停机板上的无人机与所述充电装置对接；本发明实现了无人机的精准定位及自动充电，且通过控制模块与气象监测装置通讯，以根据周围环境的气象条件控制无人机飞行，提高了无人机巡检的稳定性，该控制模块还与无人机调度系统连接，能够实现无人机的自动巡检。
附图说明
为了更清楚地说明本发明实施例或现有技术中的技术方案，下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本发明的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动性的前提下，还可以根据这些附图获得其它的附图。
图1为本发明一个可选实施例提供的一种无人机自动充电机库的外部结构示意图(带有无人机)；
图2为本发明一个可选实施例提供的一种无人机自动充电机库的内部结构示意图(带有无人机)；
图3为本发明一个可选实施例提供的回中模块的结构示意图；
图4为本发明一个可选实施例提供的滑动单元的结构示意图；
图5为本发明一个可选实施例提供的机库门驱动模块的结构示意图；
图6为本发明一个可选实施例提供的气象监测装置的结构示意图；
图7为本发明一个可选实施例提供的一种无人机自动充电机库的巡检方法的流程图。
附图标记：
1-机库外壳；2-机库门；3-机库门驱动模块；4-回中模块；5-无人机；6-骨架；7-空调；8-电源适配模块；9-控制模块；10-UPS电源；11-电机控制器；12-信号增强及电源箱；13-气象站支撑板；14-气象站；15-天线；16-支柱；101-脚架；102-检修门；103-支撑底板；104-导轨；201-左翻盖；202-右翻盖；301-转动电机；302-第二减速器；303-第三一分二同步联轴器；304- 轴；305-第二联轴器；401-回中电机；402-第一一分二同步联轴器；403-第二一分二同步联轴器；404-驱动单元；405-充电装置；406-第一回中X轴；407-第二回中X轴；408-连接块；409-滑动单元；410-第一回中Y轴；411-第二回中Y轴；412-第一减速器；413-降落停机板；491-第一联轴器；492-固定块；493-第一行程开关支座；494-第一行程开关；495-滑块；496-滑轨；497-第二行程开关支座；498-第二行程开关；499-螺杆。
具体实施方式
本发明实施例提供了一种无人机自动充电机库、系统及巡检方法，用于解决现有无人机机库不能实现无人机的精准定位及自动充电的技术问题。
为使得本发明的发明目的、特征、优点能够更加的明显和易懂，下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，下面所描述的实施例仅仅是本发明一部分实施例，而非全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其它实施例，都属于本发明保护的范围。
本发明提供了一种无人机自动充电机库。
请参阅图1，图1示出了本发明实施例提供的一种无人机自动充电机库的外部结构示意图(带有无人机5)。
本发明实施例提供的一种无人机自动充电机库，包括机库外壳1、机库门2、机库门驱动模块3、回中模块4和控制模块9。
机库外壳1的底部设有脚架101，其侧面还设有检修门102。机库外壳1由骨架6进行支撑。
所述机库门2设置于所述机库外壳1的顶部，其包括左翻盖201和右翻盖202。所述机库门2与机库门驱动模块3连接，所述机库门驱动模块3连接所述控制模块9，用于根据所述控制模块9的指令驱动所述机库门2的开闭。
如图2、图3所示，所述回中模块4设置于所述机库外壳1的内部，其包括用于承载无人机5的降落停机板413、回中装置以及充电装置405； 所述降落停机板413上设有供无人机5进行视觉识别定位的标签。
作为优选的实施方式，该标签为二维码。
通过在降落停机板413上设置供无人机5进行视觉识别定位的标签，能够确保无人机5正确无误停在板上。
所述回中装置用于根据所述控制模块9的指令，将所述降落停机板413上的无人机5回中移动至预设位置，以使所述降落停机板413上的无人机5与所述充电装置405对接。
所述回中装置包括四个回中轴，所述四个回中轴分别为第一回中X轴406、第二回中X轴407、第一回中Y轴410和第二回中Y轴411，每个所述回中轴的一端连接一滑动单元409，每个所述回中轴的另一端连接另一滑动单元409；两相邻滑动单元409之间连接驱动单元404，以在驱动单元404的驱动下对相应的回中轴进行回中移动。
如图4所示，所述滑动单元409包括第一联轴器491、固定块492、第一行程开关494、滑块495、滑轨496、第二行程开关498以及螺杆499，所述滑块495通过连接块408与对应的回中轴连接；所述第一联轴器491的动力输入端与对应的驱动单元404连接，所述第一联轴器491的动力输出端连接所述螺杆499；所述滑块495设置于所述滑轨496上并与所述螺杆499连接，以在所述螺杆499的旋转带动下沿所述滑轨496滑动；所述第一行程开关494以及所述第二行程开关498用于检测所述滑块495是否到达设定位置，并在到达设定位置后控制相应的驱动单元404停止动作。
进一步地，滑动单元409还包括用于承载第一行程开关494的第一行程开关支座493，以及用于承载第二行程开关498的第二行程开关支座497。
所述驱动单元404包括依次连接的回中电机401、第一减速器412、第一一分二同步联轴器402和第二一分二同步联轴器403，所述第二一分二同步联轴器403与所述联轴器连接。
具体实施时，回中电机401传输过来的动力，通过第一联轴器491输入至螺杆499。螺杆499的旋转带动滑块495沿着滑轨496滑动，实现旋转至平移运动。第一行程开关494和第二行程开关498主要检测滑块495是否达到设定的位置，到达指定位置后回中电机401停止动作。
在一种能够实现的方式中，如图5所示，所述机库门驱动模块3包括依次连接的转动电机301、第二减速器302、第三一分二同步联轴器303、轴304和第二联轴器305。其中轴304的一端通过第二联轴器305连接左翻盖201，另一端通过第二联轴器305连接右翻盖202。因翻盖的重力力矩的原因，电机输出力矩需要与翻盖的旋转角度对应的力矩相匹配，输出力矩的大小需要与重力力矩变化相匹配，方可稳定实现翻盖的平稳旋转。
本实施例中，通过设置翻盖式的机库门2，配合机库门驱动模块3，能够实现机库门2翻盖结构的平滑旋转，从而实现机库门2的开合。无人机5起飞、降落时打开机库门2，其余时间机库门2为关闭状态，保护无人机5及机库的内部设备。
其中，为实现对上述回中电机401以及转动电机301的自动控制，所述无人机自动充电机库还包括相应的电机控制器11，以实现对相应的电机的稳定性控制。
在一种能够实现的方式中，所述无人机自动充电机库还包括空调7；所述空调7设置于所述机库外壳1内，并与所述控制模块9连接。
本实施例中，空调7能够调节机库内部温度，避免温度因素引起的故障。
进一步地，所述无人机自动充电机库还设置电源适配模块8以及UPS电源10，该电源适配模块8主要将输入电压转换成各个器件对应的电压等级，使得各个器件可在适配的电压下工作。该UPS电源10为机库内部的缓冲电源，当外部断电时可提供应急电源。
在一种能够实现的方式中，所述控制模块9临近所述检修门102，所述控制模块9由支撑底板103承载，所述支撑底板103两侧滑动连接有导轨104。
进一步地，该支撑底板103还用于承载上述的电源适配模块8、UPS电源10以及电机控制器11。
本发明实施例，能够通过推拉支撑底板103，使支撑底板103沿导轨104移动，从而便于维修人员对支撑底板103上的器件进行维修，实现快速定位及维修工作。
本发明还提供一种无人机5自动充电系统，包括气象监测装置以及如上任意一项实施例所述的无人机自动充电机库。
图6示出了本发明一个可选实施例提供的气象监测装置的结构示意图。
本发明实施例的气象监测装置与所述控制模块9通讯连接，所述气象监测装置包括信号增强及电源箱12、气象站支撑板13、气象站14、天线14以及支柱16，所述信号增强及电源箱12、气象站支撑板13和天线15设置于所述支柱16上，其中所述天线15位于所述支柱16的顶部，所述气象站14设置于所述气象站支撑板13上。
无人机自动充电机库与信号气象站14之间采用光纤、无线等通讯方式连接，实现机库与信号气象站14之间的通讯连接。气象站14安装于气象站支撑板13上，可检测周围环境的气象条件，进而判断环境天气是否适合无人机5的飞行，避免天气原因引起的无人机5故障和损坏。信号增强及电源箱12主要为气象站14提供电源、为天线15提供增强信号的装置。
本发明还提供一种无人机自动充电机库的巡检方法，所述方法基于如上任意一项实施例所述的无人机自动充电机库。
图7示出了本发明一个可选实施例提供的一种无人机自动充电机库的巡检方法的流程图。
本发明实施例提供的一种无人机自动充电机库的巡检方法，包括：
步骤S1，控制模块9接收无人机5调度系统发送的无人机5巡检的航线信息，所述航线信息包括起飞时间、巡检任务信息以及返回时间；
步骤S2，在达到起飞时间时，所述控制模块9根据所述巡检任务信息向降落停机板413上的无人机5发送飞行指令，并向所述机库门驱动模块3发送开门指令以开启所述机库门2，同时向所述回中装置发送打开指令以使所述无人机5与充电装置405分离；
步骤S3，在所述无人机5飞出机库外壳1后，所述控制模块9向所述机库门驱动模块3发送关门指令以关闭所述机库门2；
步骤S4，在达到返回时间时，所述控制模块9向所述机库门驱动模块3发送开门指令以开启所述机库门2，同时向所述回中装置发送回中指令以 使所述无人机5与充电装置405对接，从而为无人机5充电；
步骤S5，在所述回中装置执行所述回中指令完毕后，所述控制模块9向所述机库门驱动模块3发送关门指令以关闭所述机库门2。
进一步地，所述方法还包括：
所述控制模块9接收所述无人机5上传的巡检结果；
所述控制模块9将所述巡检结果发送至所述无人机5调度系统。
本发明上述实施例，实现了无人机5的精准定位及自动充电，且通过控制模块9与气象监测装置通讯，以根据周围环境的气象条件控制无人机5飞行，提高了无人机5巡检的稳定性，该控制模块9还与无人机5调度系统连接，能够实现无人机5的自动巡检。
以上所述，以上实施例仅用以说明本发明的技术方案，而非对其限制；尽管参照前述实施例对本发明进行了详细的说明，本领域的普通技术人员应当理解：其依然可以对前述各实施例所记载的技术方案进行修改，或者对其中部分技术特征进行等同替换；而这些修改或者替换，并不使相应技术方案的本质脱离本发明各实施例技术方案的精神和范围。

Claims (10)

  1. 一种无人机自动充电机库，其特征在于，包括机库外壳、机库门、机库门驱动模块、回中模块和控制模块；
    所述机库门设置于所述机库外壳的顶部，其与机库门驱动模块连接；所述机库门驱动模块连接所述控制模块，用于根据所述控制模块的指令驱动所述机库门的开闭；
    所述回中模块设置于所述机库外壳的内部，其包括用于承载无人机的降落停机板、回中装置以及充电装置；所述降落停机板上设有供无人机进行视觉识别定位的标签；所述回中装置用于根据所述控制模块的指令，将所述降落停机板上的无人机回中移动至预设位置，以使所述降落停机板上的无人机与所述充电装置对接。
  2. 根据权利要求1所述的无人机自动充电机库，其特征在于，所述回中装置包括四个回中轴，所述四个回中轴分别为第一回中X轴、第二回中X轴、第一回中Y轴和第二回中Y轴，每个所述回中轴的一端连接一滑动单元，每个所述回中轴的另一端连接另一滑动单元；两相邻滑动单元之间连接驱动单元，以在驱动单元的驱动下对相应的回中轴进行回中移动。
  3. 根据权利要求2所述的无人机自动充电机库，其特征在于，所述滑动单元包括第一联轴器、固定块、第一行程开关、滑块、滑轨、第二行程开关以及螺杆，所述滑块通过连接块与对应的回中轴连接；所述第一联轴器的动力输入端与对应的驱动单元连接，所述第一联轴器的动力输出端连接所述螺杆；所述滑块设置于所述滑轨上并与所述螺杆连接，以在所述螺杆的旋转带动下沿所述滑轨滑动；所述第一行程开关以及所述第二行程开关用于检测所述滑块是否到达设定位置，并在到达设定位置后控制相应的驱动单元停止动作。
  4. 根据权利要求3所述的无人机自动充电机库，其特征在于，所述驱动单元包括依次连接的回中电机、第一减速器、第一一分二同步联轴器和第二一分二同步联轴器，所述第二一分二同步联轴器与所述联轴器连接。
  5. 根据权利要求1所述的无人机自动充电机库，其特征在于，所述机库门包括翻盖，所述机库门驱动模块包括依次连接的转动电机、第二减速 器、第三一分二同步联轴器、轴和第二联轴器，所述第二联轴器与所述翻盖连接。
  6. 根据权利要求1所述的无人机自动充电机库，其特征在于，还包括空调；所述空调设置于所述机库外壳内，并与所述控制模块连接。
  7. 根据权利要求1所述的无人机自动充电机库，其特征在于，所述机库外壳的侧部设有检修门，所述控制模块临近所述检修门，所述控制模块由支撑底板承载，所述支撑底板两侧滑动连接有导轨。
  8. 一种无人机自动充电系统，其特征在于，包括气象监测装置以及如权利要求1-7任意一项所述的无人机自动充电机库；
    所述气象监测装置与所述控制模块通讯连接，所述气象监测装置包括信号增强及电源箱、气象站支撑板、气象站、天线以及支柱，所述信号增强及电源箱、气象站支撑板和天线设置于所述支柱上，其中所述天线位于所述支柱的顶部，所述气象站设置于所述气象站支撑板上。
  9. 一种无人机自动充电机库的巡检方法，其特征在于，所述方法基于如权利要求1-7任意一项所述的无人机自动充电机库，所述方法包括：
    控制模块接收无人机调度系统发送的无人机巡检的航线信息，所述航线信息包括起飞时间、巡检任务信息以及返回时间；
    在达到起飞时间时，所述控制模块根据所述巡检任务信息向降落停机板上的无人机发送飞行指令，并向所述机库门驱动模块发送开门指令以开启所述机库门，同时向所述回中装置发送打开指令以使所述无人机与充电装置分离；
    在所述无人机飞出机库外壳后，所述控制模块向所述机库门驱动模块发送关门指令以关闭所述机库门；
    在达到返回时间时，所述控制模块向所述机库门驱动模块发送开门指令以开启所述机库门，同时向所述回中装置发送回中指令以使所述无人机与充电装置对接，从而为无人机充电；
    在所述回中装置执行所述回中指令完毕后，所述控制模块向所述机库门驱动模块发送关门指令以关闭所述机库门。
  10. 根据权利要求1所述的无人机自动充电机库的巡检方法，其特征 在于，所述方法还包括：
    所述控制模块接收所述无人机上传的巡检结果；
    所述控制模块将所述巡检结果发送至所述无人机调度系统。
PCT/CN2022/129173 2022-03-29 2022-11-02 一种无人机自动充电机库、系统及巡检方法 WO2023184975A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202210318866.1A CN114559833B (zh) 2022-03-29 2022-03-29 一种无人机自动充电机库、系统及巡检方法
CN202210318866.1 2022-03-29

Publications (1)

Publication Number Publication Date
WO2023184975A1 true WO2023184975A1 (zh) 2023-10-05

Family

ID=81720548

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2022/129173 WO2023184975A1 (zh) 2022-03-29 2022-11-02 一种无人机自动充电机库、系统及巡检方法

Country Status (2)

Country Link
CN (1) CN114559833B (zh)
WO (1) WO2023184975A1 (zh)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114559833B (zh) * 2022-03-29 2024-01-26 南方电网电力科技股份有限公司 一种无人机自动充电机库、系统及巡检方法
CN115946862A (zh) * 2022-12-27 2023-04-11 广州优飞智能设备有限公司 一种无人机自动换电机场

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018219226A1 (zh) * 2017-05-27 2018-12-06 星逻智能科技(苏州)有限公司 无人机停机库
CN108995823A (zh) * 2018-07-26 2018-12-14 上海楚山电子科技有限公司 无人机无线共享充电停机坪及具有优先级的无线充电方法
US20190002127A1 (en) * 2015-12-21 2019-01-03 Airscort Ltd. Autonomous docking station for drones
CN109131922A (zh) * 2018-08-30 2019-01-04 上海复亚智能科技有限公司 一种无人机自动机场系统
CN110871902A (zh) * 2018-08-30 2020-03-10 一飞智控(天津)科技有限公司 小体积式物流无人机用停机装置以及其控制方法
WO2021082794A1 (zh) * 2019-10-28 2021-05-06 北京京东乾石科技有限公司 无人机机场、无人机系统、巡检系统、方法、控制装置、设备和存储介质以及无人机巡航系统
CN112803556A (zh) * 2021-03-22 2021-05-14 国网江西省电力有限公司电力科学研究院 一种无线充电机巢、无线充电系统及方法
CN114559833A (zh) * 2022-03-29 2022-05-31 南方电网电力科技股份有限公司 一种无人机自动充电机库、系统及巡检方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103824340B (zh) * 2014-03-07 2015-12-02 山东鲁能智能技术有限公司 无人机输电线路智能巡检系统及巡检方法
CN210882679U (zh) * 2019-09-29 2020-06-30 北京京东乾石科技有限公司 一种充电站
CN111026156A (zh) * 2019-12-17 2020-04-17 北京京东乾石科技有限公司 一种巡检系统、方法、控制装置、设备和存储介质
CN111056032B (zh) * 2020-01-20 2021-07-20 上海交通大学 一种无人船载的无人机充电升降系统及实现方法
CN112711265B (zh) * 2020-04-08 2022-01-07 江苏方天电力技术有限公司 移动式多无人机智能巡检成套装备及巡检方法
CN214689064U (zh) * 2021-01-18 2021-11-12 河海大学 一种用于电力巡检无人机无线充电的机库

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190002127A1 (en) * 2015-12-21 2019-01-03 Airscort Ltd. Autonomous docking station for drones
WO2018219226A1 (zh) * 2017-05-27 2018-12-06 星逻智能科技(苏州)有限公司 无人机停机库
CN108995823A (zh) * 2018-07-26 2018-12-14 上海楚山电子科技有限公司 无人机无线共享充电停机坪及具有优先级的无线充电方法
CN109131922A (zh) * 2018-08-30 2019-01-04 上海复亚智能科技有限公司 一种无人机自动机场系统
CN110871902A (zh) * 2018-08-30 2020-03-10 一飞智控(天津)科技有限公司 小体积式物流无人机用停机装置以及其控制方法
WO2021082794A1 (zh) * 2019-10-28 2021-05-06 北京京东乾石科技有限公司 无人机机场、无人机系统、巡检系统、方法、控制装置、设备和存储介质以及无人机巡航系统
CN112803556A (zh) * 2021-03-22 2021-05-14 国网江西省电力有限公司电力科学研究院 一种无线充电机巢、无线充电系统及方法
CN114559833A (zh) * 2022-03-29 2022-05-31 南方电网电力科技股份有限公司 一种无人机自动充电机库、系统及巡检方法

Also Published As

Publication number Publication date
CN114559833B (zh) 2024-01-26
CN114559833A (zh) 2022-05-31

Similar Documents

Publication Publication Date Title
WO2023184975A1 (zh) 一种无人机自动充电机库、系统及巡检方法
WO2021068576A1 (zh) 基于太阳能供电的无人机自主起降换电池的能源自治基站
CN207360291U (zh) 无人机取电池系统
CN112061412B (zh) 适用于多种安装需求的无人机智能机库
US12084211B2 (en) Automatic recycling and charging nest for vertical take-off and landing unmanned aerial vehicle
CN212195683U (zh) 一种配电巡检机器人
CN110589007B (zh) 重载工业级多旋翼无人机机库
CN108572661A (zh) 一种无人机控制系统及无人机控制方法
CN102570345B (zh) 一种无人机输电线路航巡系统
CN112706649B (zh) 无人机电池组自动化换装系统
CN111438677A (zh) 一种无人值守机房巡检机器人
CN207157515U (zh) 一种巡检无人机控制系统
CN214062518U (zh) 一种无人机自动机场
CN208506595U (zh) 一种无人机控制系统
CN203405734U (zh) 四旋翼航拍定位无人飞行器
US8393901B2 (en) Group of flight simulators and associated structure
CN210214608U (zh) 一种无人机监管平台
CN213566539U (zh) 一种适用于多种安装需求的无人机智能机库
CN105667631A (zh) 自主弹跳越障的遥控小车
CN216734816U (zh) 一种无人机机巢
CN216231718U (zh) 一种用于无人机精准定位及充换电的智能方舱
CN108557108B (zh) 陆空安防机器人及其应用方法
CN110700668B (zh) 一种太阳能智能无人机机库
CN215752012U (zh) 一种无人机自动归中结构
CN215155758U (zh) 一种无人机自主收放基站

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 22934793

Country of ref document: EP

Kind code of ref document: A1