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CN114954983A - Shutdown platform, unmanned aerial vehicle base station, and landing method and system of unmanned aerial vehicle - Google Patents

Shutdown platform, unmanned aerial vehicle base station, and landing method and system of unmanned aerial vehicle Download PDF

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Publication number
CN114954983A
CN114954983A CN202210203531.5A CN202210203531A CN114954983A CN 114954983 A CN114954983 A CN 114954983A CN 202210203531 A CN202210203531 A CN 202210203531A CN 114954983 A CN114954983 A CN 114954983A
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unmanned aerial
aerial vehicle
base station
uav
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CN114954983B (en
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张肖
高诗经
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SZ DJI Technology Co Ltd
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SZ DJI Technology Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • 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
    • B60L53/10Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14Conductive energy transfer
    • 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
    • B60L53/30Constructional details of charging stations
    • 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
    • B60L53/30Constructional details of charging stations
    • B60L53/35Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
    • B60L53/36Means for automatic or assisted adjustment of the relative position of charging devices and vehicles by positioning the vehicle
    • 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
    • B60L53/60Monitoring or controlling charging stations
    • B60L53/65Monitoring or controlling charging stations involving identification of vehicles or their battery types
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls
    • 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
    • Y02T90/12Electric charging stations

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

An unmanned aerial vehicle base station, comprising: the system comprises a shell, a shutdown platform and a radio frequency identification antenna; the shutdown platform and the shell are matched to form a relatively closed base station inner cavity, and the radio frequency identification antenna is used for verifying the identity of the unmanned aerial vehicle before the unmanned aerial vehicle lands to a shutdown area of the shutdown platform. The landing method and the landing system of the unmanned aerial vehicle base station are also provided.

Description

停机平台、无人飞行器基站、无人飞行器的降落方法及系统Parking platform, base station of unmanned aerial vehicle, landing method and system of unmanned aerial vehicle

技术领域technical field

本发明实施例属于无人飞行器技术领域,尤其涉及一种停机平台和采用该停机平台的无人飞行器基站,以及对应的无人飞行器的降落方法及系统。Embodiments of the present invention belong to the technical field of unmanned aerial vehicles, and in particular, relate to a parking platform and an unmanned aerial vehicle base station using the parking platform, as well as a corresponding landing method and system of an unmanned aerial vehicle.

背景技术Background technique

小型无人飞行器(Unmanned Aerial Vehicle,UAV)的电池续航能力有限,一般在10到30分钟之间,每次电池电量耗尽,需要更换电池或者重新充电后才能继续飞行,无法进行全自动化的远程作业。The battery life of a small unmanned aerial vehicle (UAV) is limited, usually between 10 and 30 minutes. Every time the battery is exhausted, the battery needs to be replaced or recharged before it can continue to fly. Operation.

现有实现无人飞行器自动远程作业的解决方案是为无人飞行器配置充电站,使无人飞行器可通过充电站进行自动充电,完成电量补给后再根据预先规划的航线自动进行作业,无人飞行器的电量补给方式主要包括置换电池、接触式充电和非接触式充电。The existing solution to realize automatic remote operation of unmanned aerial vehicles is to configure charging stations for unmanned aerial vehicles, so that unmanned aerial vehicles can be automatically charged through the charging station, and then automatically operate according to pre-planned routes after the power supply is completed. The power supply methods mainly include battery replacement, contact charging and non-contact charging.

置换电池的方式需要充电站配置机器臂,同时需要无人飞行器在停机平台上能够精确定位,对无人飞行器和充电站的软硬件要求高,需要通过增加设备的复杂度来提升操作精细度和定位精确度;The method of replacing the battery requires the charging station to be equipped with a robotic arm, and at the same time, the UAV needs to be able to accurately position the UAV on the parking platform. The hardware and software requirements for the UAV and the charging station are high, and it is necessary to increase the complexity of the equipment to improve the operation precision and performance. positioning accuracy;

非接触式充电主要指无线充电,无人飞行器在充电时保持悬停,在要求无人飞行器具备较高的定位精度的同时,现有无线充电方案对设备的硬件要求高,且充电效率低;Non-contact charging mainly refers to wireless charging. The unmanned aerial vehicle keeps hovering during charging. While the unmanned aerial vehicle is required to have high positioning accuracy, the existing wireless charging solution has high requirements on the hardware of the device and low charging efficiency;

接触式充电则采用无人飞行器的充电触点接触充电板的方式实现充电,然而现有的接触式充电方案存在无人飞行器定位精度低导致充电板面积过大的问题。Contact charging uses the way that the charging contacts of the unmanned aerial vehicle contact the charging board to realize charging. However, the existing contact charging scheme has the problem that the positioning accuracy of the unmanned aerial vehicle is low, resulting in an excessively large area of the charging board.

综上所述,亟需一种结构简单、定位精确的平台供无人飞行器降落。To sum up, there is an urgent need for a platform with simple structure and accurate positioning for landing of unmanned aerial vehicles.

发明内容SUMMARY OF THE INVENTION

为了解决上述问题,本发明实施例提供一种结构简单、定位精确的停机平台,此外还提供采用该停机平台的无人飞行器基站,以及对应的无人飞行器的降落方法及系统。In order to solve the above problems, the embodiments of the present invention provide a parking platform with simple structure and accurate positioning, and also provide an unmanned aerial vehicle base station using the parking platform, and a corresponding landing method and system of the unmanned aerial vehicle.

一方面,本发明提供一种无人飞行器基站,包括:壳体、停机平台,以及射频识别天线;其中,所述停机平台和所述壳体配合形成相对封闭的基站内腔,所述射频识别天线用于在所述无人飞行器降落至所述停机平台的停机区域前对所述无人飞行器进行身份验证。In one aspect, the present invention provides an unmanned aerial vehicle base station, comprising: a casing, a parking platform, and a radio frequency identification antenna; wherein, the parking platform and the casing cooperate to form a relatively closed inner cavity of the base station, and the radio frequency identification The antenna is used to authenticate the unmanned aerial vehicle before the unmanned aerial vehicle descends to the parking area of the parking platform.

另一方面,本发明还提供一种无人飞行器的降落系统,包括无人飞行器和如前述的无人飞行器基站。In another aspect, the present invention also provides a landing system for an unmanned aerial vehicle, including the unmanned aerial vehicle and the aforementioned unmanned aerial vehicle base station.

另一方面,本发明还提供一种无人飞行器的降落方法,包括:无人飞行器基站通过遥控装置发送基站位置信息至无人飞行器;所述无人飞行器根据所述位置信息飞行至所述无人飞行器基站的停机平台上方;所述无人飞行器基站通过射频识别天线对所述无人飞行器进行身份验证;在所述身份验证通过后,所述无人飞行器降落至所述停机平台。In another aspect, the present invention also provides a method for landing an unmanned aerial vehicle, comprising: the unmanned aerial vehicle base station sends the base station location information to the unmanned aerial vehicle through a remote control device; the unmanned aerial vehicle flies to the unmanned aerial vehicle according to the location information above the parking platform of the base station of the unmanned aerial vehicle; the base station of the unmanned aerial vehicle verifies the identity of the unmanned aerial vehicle through the radio frequency identification antenna; after the identity verification is passed, the unmanned aerial vehicle lands on the parking platform.

附图说明Description of drawings

为了更清楚地说明本发明或现有技术中的方案,下面将对实施例或现有技术描述中所需要使用的附图作一个简单介绍,显而易见地,下面描述中的附图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的前提下,还可以根据这些附图获得其他的附图。In order to explain the present invention or the solutions in the prior art more clearly, the following will briefly introduce the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the drawings in the following description are of the present invention. In some embodiments, for those of ordinary skill in the art, other drawings can also be obtained according to these drawings without any creative effort.

图1为本发明实施例提供的无人飞行器基站的结构示意图;FIG. 1 is a schematic structural diagram of an unmanned aerial vehicle base station provided by an embodiment of the present invention;

图2为本发明实施例提供的无人飞行器降落在基站上的结构示意图;2 is a schematic structural diagram of an unmanned aerial vehicle landing on a base station according to an embodiment of the present invention;

图3为本发明实施例提供的停机区域的一种结构示意图;3 is a schematic structural diagram of a shutdown area provided by an embodiment of the present invention;

图4为本发明实施例提供的无人飞行器基站的另一结构示意图;4 is another schematic structural diagram of an unmanned aerial vehicle base station provided by an embodiment of the present invention;

图5为本发明实施例提供的无人飞行器的降落方法的流程图。FIG. 5 is a flowchart of a method for landing an unmanned aerial vehicle according to an embodiment of the present invention.

具体实施方式Detailed ways

为了使本技术领域的人员更好地理解本发明方案,下面对本发明实施例中的技术方案进行清楚、完整地描述。除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是旨在于限制本发明。In order for those skilled in the art to better understand the solutions of the present invention, the technical solutions in the embodiments of the present invention are described clearly and completely below. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terms used herein in the description of the present invention are for the purpose of describing specific embodiments only, and are not intended to limit the present invention.

在本文中提及“实施例”意味着,结合实施例描述的特定特征、结构或特性可以包含在本发明的至少一个实施例中。在说明书中的各个位置出现该短语并不一定均是指相同的实施例,也不是与其它实施例互斥的独立的或备选的实施例。本领域技术人员显式地和隐式地理解的是,本文所描述的实施例可以与其它实施例相结合。Reference herein to an "embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the present invention. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor a separate or alternative embodiment that is mutually exclusive of other embodiments. It is explicitly and implicitly understood by those skilled in the art that the embodiments described herein may be combined with other embodiments.

本发明实施例提供一种停机平台,应用于无人飞行器,包括停机区域,与所述停机区域邻接的导向部,以及设置在所述停机区域内的定位点;其中,所述导向部环绕所述停机区域限定所述停机区域的大小,所述导向部包括面向所述停机区域的导向面,用于使无人飞行器降落至所述导向部上时沿着所述导向面滑落至所述停机区域中,同时使所述无人飞行器定位至所述定位点。An embodiment of the present invention provides a parking platform, which is applied to an unmanned aerial vehicle, and includes a parking area, a guide portion adjacent to the parking area, and a positioning point set in the parking area; wherein the guide portion surrounds the parking area. The parking area defines the size of the parking area, and the guide portion includes a guide surface facing the parking area, which is used to make the unmanned aerial vehicle slide down to the parking area along the guide surface when landing on the guide portion. In the area, the unmanned aerial vehicle is positioned to the positioning point at the same time.

本发明提供的停机平台通过导向部的配合无人飞行器进行降落,实现无人飞行器在停机区域的定位,结构简单,不需要高精度的机械臂或者定位导航模块即可实现无人飞行器在停机平台上的精确降落和定位,一方面降低了停机平台的设备成本和复杂度,另一方面降低了对无人飞行器的导航和定位设备的精度要求,通用性强,具有更广的适用范围。The parking platform provided by the present invention uses the guide part to cooperate with the unmanned aerial vehicle to land, and realizes the positioning of the unmanned aerial vehicle in the parking area. The precise landing and positioning on the UAV reduces the equipment cost and complexity of the parking platform on the one hand, and reduces the accuracy requirements for the navigation and positioning equipment of the UAV on the other hand. It has strong versatility and a wider scope of application.

基于上述停机平台,本发明实施例还提供一种无人飞行器基站,包括壳体、遥控装置,以及上述的停机平台,所述停机平台和所述壳体配合形成相对封闭的基站内腔,当无人飞行器需要降落至所述停机平台时,所述遥控装置发送基站的位置信息至所述无人飞行器,用于使无人飞行器根据所述位置信息飞行至所述停机平台上方,并降落至所述导向部上,沿着所述导向部的导向面滑落至所述停机区域中,同时在所述定位点完成定位。Based on the above-mentioned parking platform, an embodiment of the present invention further provides an unmanned aerial vehicle base station, which includes a casing, a remote control device, and the above-mentioned parking platform. The parking platform and the casing cooperate to form a relatively closed inner cavity of the base station. When the unmanned aerial vehicle needs to land on the parking platform, the remote control device sends the location information of the base station to the unmanned aerial vehicle, so that the unmanned aerial vehicle can fly above the parking platform according to the location information, and land on the ground. On the guide portion, the guide portion slides down into the parking area along the guide surface of the guide portion, and at the same time completes the positioning at the positioning point.

基于上述无人飞行器基站,本发明实施例还提供一种无人飞行器的降落系统,包括无人飞行器和无人飞行器基站,所述无人飞行器基站包括遥控装置和停机平台,其中,所述无人飞行器基站通过所述遥控装置发送基站的位置信息至所述无人飞行器,所述无人飞行器根据所述位置信息飞行至所述停机平台上方,并进一步降落至所述停机平台的导向部上,沿着所述导向部的导向面滑落至所述停机平台的停机区域中,同时在所述停机区域内设置的定位点完成定位。Based on the above unmanned aerial vehicle base station, an embodiment of the present invention further provides a landing system for an unmanned aerial vehicle, including an unmanned aerial vehicle and an unmanned aerial vehicle base station, the unmanned aerial vehicle base station includes a remote control device and a parking platform, wherein the unmanned aerial vehicle The base station of the human aircraft sends the position information of the base station to the unmanned aerial vehicle through the remote control device, and the unmanned aerial vehicle flies to the top of the parking platform according to the position information, and further lands on the guide part of the parking platform , slide down the guide surface of the guide part into the stop area of the stop platform, and at the same time complete the positioning at the positioning points set in the stop area.

无人飞行器的降落系统,本发明实施例还提供一种无人飞行器的降落方法,包括:A landing system for an unmanned aerial vehicle, an embodiment of the present invention also provides a landing method for an unmanned aerial vehicle, including:

无人飞行器基站通过遥控装置发送基站位置信息至无人飞行器;The UAV base station sends the base station location information to the UAV through the remote control device;

所述无人飞行器根据所述位置信息飞行至所述无人飞行器基站的停机平台上方;The unmanned aerial vehicle flies above the parking platform of the unmanned aerial vehicle base station according to the position information;

所述无人飞行器降落至所述停机平台的导向部上,沿着所述导向部的导向面滑落至所述停机平台的停机区域中,同时在所述停机区域内设置的定位点完成定位。The unmanned aerial vehicle landed on the guide portion of the parking platform, and slid along the guide surface of the guide portion into the parking area of the parking platform, and at the same time, the positioning points set in the parking area completed the positioning.

下面结合附图详细说明本发明的一些具体实施方式。Some specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

请一并参阅图1和图2,本发明实施例提供的无人飞行器基站10包括壳体100、遥控装置(图中未示出)和停机平台200,其中,壳体100可以是半封闭结构,停机平台200和壳体100配合形成相对封闭的基站内腔,在本实施例中,遥控装置可以安装在该基站内腔中,或者单独安装在基站外面,与基站采用有线连接。Please refer to FIG. 1 and FIG. 2 together. The unmanned aerial vehicle base station 10 provided by the embodiment of the present invention includes a casing 100, a remote control device (not shown in the figure), and a parking platform 200, wherein the casing 100 may be a semi-closed structure , the shutdown platform 200 and the housing 100 cooperate to form a relatively closed inner cavity of the base station. In this embodiment, the remote control device can be installed in the inner cavity of the base station, or separately installed outside the base station, and is connected to the base station by wire.

进一步的,停机平台200包括停机区域210,与停机区域210邻接的导向部220,以及设置在停机区域210内的定位点230;其中,所述导向部220环绕所述停机区域210以限定所述停机区域210的大小,所述导向部220包括面向所述停机区域210的导向面221,当无人飞行器20需要降落至所述停机平台200时,遥控装置发送无人飞行器基站10的位置信息至无人飞行器20,用于使无人飞行器20根据所述位置信息飞行至停机平台200上方,并降落至导向部220上,沿着导向部220的导向面221滑落至停机区域210中,同时在定位点230完成定位。在一些实施例中,所述停机平台200可以包括两个及以上所述停机区域210,所述导向部220限定整体停机区域210的大小,相邻的所述停机区域210之间设置有隔离件(图中未示出),每个所述停机区域210设置有所述定位点230。Further, the parking platform 200 includes a parking area 210, a guide portion 220 adjacent to the parking area 210, and a positioning point 230 disposed in the parking area 210; wherein, the guide portion 220 surrounds the parking area 210 to define the The size of the parking area 210, the guide part 220 includes a guide surface 221 facing the parking area 210, when the UAV 20 needs to land on the parking platform 200, the remote control device sends the location information of the UAV base station 10 to The unmanned aerial vehicle 20 is used to make the unmanned aerial vehicle 20 fly to the top of the parking platform 200 according to the position information, and land on the guide part 220, slide down to the parking area 210 along the guide surface 221 of the guide part 220, and at the same time The positioning point 230 completes the positioning. In some embodiments, the parking platform 200 may include two or more parking areas 210 , the guide portion 220 defines the size of the entire parking area 210 , and spacers are provided between adjacent parking areas 210 . (not shown in the figure), each of the parking areas 210 is provided with the positioning point 230 .

进一步的,所述定位点230上设有充电位231,充电位231用于与所述无人飞行器20的脚架电接触,以使无人飞行器基站10与所述无人飞行器20实现电连接,所述充电位231上设置成对的金属触点,其中成对设置的所述金属触点分别连接充电电源的不同电极。Further, the positioning point 230 is provided with a charging position 231, and the charging position 231 is used for making electrical contact with the tripod of the UAV 20, so that the UAV base station 10 and the UAV 20 can be electrically connected. , a pair of metal contacts are arranged on the charging position 231 , wherein the pair of metal contacts are respectively connected to different electrodes of the charging power source.

在另一些实施例中,所述停机平台200包括成对设置的定位点230,所述定位点230上设有充电位231,所述充电位231上设置金属触点,成对设置的所述定位点230上的金属触点分别连接充电电源的不同电极,即其中一个定位点230上的金属触点连接充电电源的正极,另一个定位点230上的金属触点连接充电电源的负极。In other embodiments, the stopping platform 200 includes positioning points 230 arranged in pairs, charging positions 231 are arranged on the positioning points 230, metal contacts are arranged on the charging positions 231, and the paired The metal contacts on the positioning points 230 are respectively connected to different electrodes of the charging power supply, that is, the metal contact on one positioning point 230 is connected to the positive pole of the charging power supply, and the metal contact on the other positioning point 230 is connected to the negative pole of the charging power supply.

可选的,前述实施例中所述的充电位231上设置的金属触点可以包括充电金属触点和数据传输金属触点,无人飞行器20在通过充电金属触点进行充电的同时,还可以通过数据传输金属触点实现与基站的有线通信,进行不同类型的数据交互,比如升级无人飞行器20的飞控系统。Optionally, the metal contacts provided on the charging position 231 described in the foregoing embodiments may include charging metal contacts and data transmission metal contacts, and the unmanned aerial vehicle 20 can also be charged through the charging metal contacts while charging. The wired communication with the base station is realized through the data transmission metal contacts, and different types of data interaction are carried out, such as upgrading the flight control system of the unmanned aerial vehicle 20 .

可选的,在前述定位点230上还设置有限位部232,该限位部232能够与无人飞行器20脚架上的底部配合,限定无人飞行器20在平面上的运动,比如该限位部232为限位凹槽,无人飞行器20脚架设置有凸起,当无人飞行器20降落至所述导向部220上时沿着所述导向面221滑落至所述停机区域210中时,无人飞行器20的充电触点定位至所述定位点230的同时,无人飞行器20脚架底部的凸起正好定位至该限位凹槽中,使无人飞行器20不能在停机区域210所在的平面内平移或转动;由于无人飞行器20可以在导向部220的作用下滑落至停机区域210完成精确定位,因此,即使在充电位231上的金属触点面积较小时,无人飞行器20的脚架也能精确接触充电位231上的金属触点,实现无人飞行器20与无人飞行器基站10的电连接,进而实现无人飞行器20的充电;在具体实施例中,所述充电位231位于所述限位部232中,也可以位于所述限位部232的一侧。Optionally, a limiting portion 232 is also provided on the aforementioned positioning point 230, and the limiting portion 232 can cooperate with the bottom of the tripod of the unmanned aerial vehicle 20 to limit the movement of the unmanned aerial vehicle 20 on the plane. The portion 232 is a limiting groove, and the tripod of the unmanned aerial vehicle 20 is provided with a protrusion. When the unmanned aerial vehicle 20 falls on the guide portion 220 and slides down into the parking area 210 along the guide surface 221, When the charging contact of the UAV 20 is positioned to the positioning point 230, the protrusion at the bottom of the tripod of the UAV 20 is just positioned in the limiting groove, so that the UAV 20 cannot be located where the parking area 210 is located. Translation or rotation in the plane; since the unmanned aerial vehicle 20 can slide down to the parking area 210 under the action of the guide part 220 to complete precise positioning, even when the metal contact area on the charging position 231 is small, the feet of the unmanned aerial vehicle 20 The rack can also precisely contact the metal contacts on the charging position 231 to realize the electrical connection between the unmanned aerial vehicle 20 and the unmanned aerial vehicle base station 10, thereby realizing the charging of the unmanned aerial vehicle 20; in a specific embodiment, the charging position 231 is located at The limiting portion 232 may also be located on one side of the limiting portion 232 .

在另一些实施例中,可以在所述停机区域210中临近所述定位点230设置有限位部232,参阅图3,所述定位点230包括围绕该限位部232周向设置的多个充电位231,这样可以在无人飞行器20以不同的方位降落至停机区域210时,无人飞行器20脚架均能与充电位231的金属触点接触。In other embodiments, a limiting portion 232 may be provided in the parking area 210 adjacent to the positioning point 230 . Referring to FIG. 3 , the positioning point 230 includes a plurality of charging points circumferentially arranged around the limiting portion 232 . Position 231, so that when the unmanned aerial vehicle 20 lands in the parking area 210 in different directions, the legs of the unmanned aerial vehicle 20 can all be in contact with the metal contacts of the charging position 231.

在其他实施例中,所述定位点230还设置有活动盖板(图中未示出),或者仅仅是在所述定位点230的充电位231处设置有活动盖板,该活动盖板在无人飞行器20降落时或者充电时自动打开,在无人飞行器20充电完毕或者起飞后自动关闭,以保护裸露的金属触点,该活动盖板可以设置成翻转形式,也可以设置成推拉形式。In other embodiments, the positioning point 230 is also provided with a movable cover plate (not shown in the figure), or only a movable cover plate is provided at the charging position 231 of the positioning point 230, and the movable cover plate is located at the charging position 231 of the positioning point 230. The UAV 20 is automatically opened when landing or charging, and automatically closed when the UAV 20 is fully charged or taken off to protect the exposed metal contacts.

进一步的,导向部220可以包含多个面向所述停机区域210的导向面221,每一个导向面221可以是相对停机区域210倾斜的平面或者曲面,从而在所述停机区域210上方形成一个凹陷,所述凹陷用于收容所述无人飞行器20。停机区域210的形状和大小由环绕停机区域210的导向部220来限定,比如停机区域210导向部220包括形状大小一致的四个第一导向面2210和形状大小一致的四个第二导向面2211,该四个所述第一导向面2210与所述停机区域210的对应的边连接,四个所述第二导向面2211中每一个第二导向面2211连接在对应相邻的两个第一导向面2210之间,从而限定出一矩形区域,该矩形区域即为停机区域210,一般地,停机区域210的形状和大小与无人飞行器20脚架的形状和尺寸相匹配。在一些实施例中,导向部220可以是导向板或者导向台。Further, the guide portion 220 may include a plurality of guide surfaces 221 facing the parking area 210, and each guide surface 221 may be a plane or curved surface inclined relative to the parking area 210, so as to form a depression above the parking area 210, The recess is used to accommodate the unmanned aerial vehicle 20 . The shape and size of the parking area 210 are defined by the guide parts 220 surrounding the parking area 210 . For example, the guide part 220 of the parking area 210 includes four first guide surfaces 2210 with the same shape and size and four second guide surfaces 2211 with the same shape and size , the four first guide surfaces 2210 are connected with the corresponding edges of the parking area 210 , and each of the four second guide surfaces 2211 is connected with the corresponding adjacent two first guide surfaces 2211 A rectangular area is defined between the guide surfaces 2210 , and the rectangular area is the parking area 210 . Generally, the shape and size of the parking area 210 match the shape and size of the tripod of the UAV 20 . In some embodiments, the guide portion 220 may be a guide plate or a guide table.

重新参阅图2,所述无人飞行器基站10还包括装设在所述壳体100上的防护组件300,具体的,所述防护组件300位于所述停机平台200上方,所述防护组件300与所述停机区域210、所述导向部220配合形成所述无人飞行器20的收容腔。所述防护组件300用于防护所述停机平台200以及降落在所述停机平台200上的无人飞行器20。在本实施例中,防护组件300可以实现防尘、防水、防高温暴晒等效果,形成有效保护无人飞行器20在户外长期作业时的安全存放环境。Referring back to FIG. 2 , the UAV base station 10 further includes a protective assembly 300 mounted on the housing 100 . Specifically, the protective assembly 300 is located above the parking platform 200 , and the protective assembly 300 is connected to the The parking area 210 and the guide portion 220 cooperate to form a receiving cavity of the unmanned aerial vehicle 20 . The protection assembly 300 is used to protect the parking platform 200 and the unmanned aerial vehicle 20 landing on the parking platform 200 . In this embodiment, the protective component 300 can achieve the effects of dustproof, waterproof, and high temperature exposure protection, thereby forming a safe storage environment that effectively protects the unmanned aerial vehicle 20 during long-term operation outdoors.

进一步地,参阅图4,所述防护组件300包括驱动件310和防护门320,所述驱动件310驱动所述防护门320相对于所述壳体100打开或关闭,所述防护门320可以是单开或者双开的平面门,也可以是盒状或者半球状的异形门,该异性门也可设置成单开或者双开形式;作为可选方案,所述防护门320上可设置透明视窗。在另一些可选方案中,所述防护组件300还包括设置在所述防护门320上的密封圈,所述密封圈可为橡胶圈。Further, referring to FIG. 4 , the protection assembly 300 includes a driving member 310 and a protection door 320 , the driving member 310 drives the protection door 320 to open or close relative to the housing 100 , and the protection door 320 may be The single-opening or double-opening plane door can also be a box-shaped or hemispherical special-shaped door, and the heterosexual door can also be set to a single-opening or double-opening form; as an optional solution, a transparent window can be provided on the protective door 320 . In other optional solutions, the protection assembly 300 further includes a sealing ring disposed on the protection door 320, and the sealing ring may be a rubber ring.

在一些实施例中,所述驱动件310可以为顶升气缸,所述顶升气缸的活塞杆与所述防护门320固定连接,以带动所述防护门320在竖直方向上移动,完成防护门320的开启和关闭。In some embodiments, the driving member 310 may be a jacking cylinder, and the piston rod of the jacking cylinder is fixedly connected to the protective door 320 to drive the protective door 320 to move in the vertical direction to complete the protection Opening and closing of door 320.

在另一些实施例中,所述防护组件300还包括连接组件330,所述连接组件330连接所述防护门320与所述壳体100。In other embodiments, the protective assembly 300 further includes a connecting assembly 330 , and the connecting assembly 330 connects the protective door 320 and the housing 100 .

作为可选方案,重新参阅图4,所述连接组件330为外铰链的结构,具体包括第一连接部331、第二连接部332和转轴333,所述第一连接部331和第二连接部332分别连接所述防护门320与所述壳体100的外表面,所述转轴333与所述驱动件310连接,所述第一连接部331和所述第二连接部332通过所述转轴333实现转动连接;第一连接部331和第二连接部332的连接面采用大面积连接面,通过螺丝或者铆钉将第一连接部331和第二连接部332分别固定在所述防护门320与所述壳体100的外表面上,转轴333与第一连接部331固定连接,同时转轴333通过轴承安装在第二连接部332上设置的轴承座上,通过驱动件310带动转轴333转动,从而带动在第一连接部331和防护门320整体运动,实现防护门320的开启和关闭;本实施例中,所述防护组件300包括多个连接组件330,该多个连接组件330的转轴333同轴,且其中一个所述连接组件330的转轴333与所述驱动件310连接,在本实施例中,所述连接组件330可调节,以保证多个连接组件330的转轴的同轴度;由于连接组件330采用外铰链的结构,可以展开更大的角度,使得防护门320的开合范围更大,同时采用外铰链机构,当防护门320闭合时,防护门320与壳体100完全闭合,形成相对密封的无人飞行器20收纳腔,有利于防尘和防水等,同时,第一连接部331和第二连接部332采用大面积的连接面,可以增加防护门320稳定性和侧面抗风抗冲击的能力,在大风天气保证防护门320能够安全打开和关闭。As an optional solution, referring to FIG. 4 again, the connecting assembly 330 is an external hinge structure, and specifically includes a first connecting portion 331 , a second connecting portion 332 and a rotating shaft 333 . The first connecting portion 331 and the second connecting portion 331 332 are respectively connected to the protective door 320 and the outer surface of the housing 100 , the rotating shaft 333 is connected to the driving member 310 , the first connecting part 331 and the second connecting part 332 pass through the rotating shaft 333 The connection surface of the first connection part 331 and the second connection part 332 adopts a large-area connection surface, and the first connection part 331 and the second connection part 332 are respectively fixed on the protective door 320 and the protective door 320 by screws or rivets. On the outer surface of the housing 100, the rotating shaft 333 is fixedly connected with the first connecting portion 331, and at the same time, the rotating shaft 333 is mounted on the bearing seat provided on the second connecting portion 332 through the bearing, and the rotating shaft 333 is driven to rotate by the driving member 310, thereby driving the rotating shaft 333 to rotate. The first connecting portion 331 and the protective door 320 move as a whole to realize the opening and closing of the protective door 320; in this embodiment, the protective assembly 300 includes a plurality of connecting assemblies 330, and the rotating shafts 333 of the plurality of connecting assemblies 330 are coaxial , and the rotating shaft 333 of one of the connecting assemblies 330 is connected with the driving member 310. In this embodiment, the connecting assembly 330 can be adjusted to ensure the coaxiality of the rotating shafts of the multiple connecting assemblies 330; The assembly 330 adopts the structure of the outer hinge, which can be unfolded to a larger angle, so that the opening and closing range of the protective door 320 is larger, and the outer hinge mechanism is adopted at the same time. The relatively sealed storage cavity of the unmanned aerial vehicle 20 is conducive to dustproof and waterproof, etc. At the same time, the first connecting part 331 and the second connecting part 332 adopt large-area connecting surfaces, which can increase the stability of the protective door 320 and the side wind resistance. The impact capability ensures that the protective door 320 can be opened and closed safely in windy weather.

作为可选方案,所述连接组件330包括导轨(图未示出)和滑动座(图未示出),所述导轨与所述防护门320和所述壳体100中的一个固定连接,所述滑动座与所述防护门320和所述壳体100中的另一个固定连接,所述驱动件310与所述滑动座连接。As an optional solution, the connecting assembly 330 includes a guide rail (not shown in the figure) and a sliding seat (not shown in the figure), and the guide rail is fixedly connected with one of the protective door 320 and the housing 100, so The sliding seat is fixedly connected with the other one of the protective door 320 and the housing 100 , and the driving member 310 is connected with the sliding seat.

进一步的,在另一实施例中,前述实施例所述导向部220包括多个面向所述停机区域210的所述导向面221,在部分或全部所述导向面221上设置有第一通风部2212,无人飞行器20可能由于充电导致电池升温或者在高温下作业导致机身升温,这些情况下无人飞行器20降落在停机平台200的停机区域210时,可通过导向面221设置的第一通风部2212送风,对无人飞行器20的机身或者电池进行降温;在其他实施例中,所述导向部220背离所述停机区域210的一侧设置有导流风扇(图中未示出),该导流风扇的扇叶大小与导向面221上设置的第一通风部2212的大小相适配;作为一种可选的实施例,所述第一通风部2212为网状通风口或者是栅状通风口。Further, in another embodiment, the guide portion 220 in the previous embodiment includes a plurality of the guide surfaces 221 facing the parking area 210 , and a first ventilation portion is provided on some or all of the guide surfaces 221 2212, the unmanned aerial vehicle 20 may heat up the battery due to charging or the fuselage of the unmanned aerial vehicle 20 may heat up due to operation at high temperature. In these cases, when the unmanned aerial vehicle 20 lands in the parking area 210 of the parking platform 200, the first ventilation provided by the guide surface 221 can be used. The air is supplied from the part 2212 to cool the body or the battery of the UAV 20; in other embodiments, a guide fan (not shown in the figure) is provided on the side of the guide part 220 away from the parking area 210 , the size of the blades of the guide fan is adapted to the size of the first ventilation portion 2212 provided on the guide surface 221; as an optional embodiment, the first ventilation portion 2212 is a mesh vent or a Grille vents.

进一步地,所述停机区域210设置有第二通风部211,作为一种可选的实施例,停机区域210设置的第二通风部211包括若干有序排列的通孔,这些通孔可以环绕定位点230设置。当然,停机区域210设置的第二通风部211也可以为网状通风口或者是栅状通风口,可选的,在所述停机区域210的背部也可以装设导流风扇。Further, the stop area 210 is provided with a second ventilation part 211. As an optional embodiment, the second ventilation part 211 provided in the stop area 210 includes a plurality of through holes arranged in an orderly manner, and these through holes can be positioned around Point 230 Settings. Of course, the second ventilation part 211 provided in the shutdown area 210 may also be a mesh ventilation port or a grid ventilation port. Optionally, a guide fan may also be installed at the back of the shutdown area 210 .

进一步地,无人飞行器基站10对应设置有温度调节装置(图中未示出),所述温度调节装置可以是风扇或者空调,温度调节装置可以调节基站内部的温度,当无人飞行器20降落在停机平台200上,且在停机平台200上方设置的防护组件300的防护门320关闭时,由上述的基站内腔、第一通风部2212和第二通风部211、收容腔共同组成循环的空气流道,在导流风扇的作用下,无人飞行器基站10的温度调节装置吹出的冷风在该空气流道中流动,重新参阅图1,图中的黑色空心箭头标识了空气流动方向,具体的,在导流风扇的作用下,温度调节装置输出的冷风从基站内腔通过第一通风部2212进入收容腔,冷却无人飞行器20后的热风再从收容腔通过第二通风部211回到基站内腔由温度调节装置进行冷却,如此循环,可有效降低无人飞行器20的机身或电池温度。当然,在低温环境中,也可以是由无人飞行器基站10的温度调节装置吹出暖风在该空气流道中流动,提高无人飞行器20的机身温度。Further, the unmanned aerial vehicle base station 10 is correspondingly provided with a temperature adjustment device (not shown in the figure), the temperature adjustment device can be a fan or an air conditioner, and the temperature adjustment device can adjust the temperature inside the base station. On the shutdown platform 200, and when the protective door 320 of the protective assembly 300 provided above the shutdown platform 200 is closed, the above-mentioned base station inner cavity, the first ventilation part 2212, the second ventilation part 211, and the receiving cavity together form a circulating air flow. Under the action of the diversion fan, the cold air blown by the temperature adjustment device of the unmanned aerial vehicle base station 10 flows in the air flow channel. Referring to FIG. 1 again, the black hollow arrow in the figure indicates the air flow direction. Under the action of the guide fan, the cold air output by the temperature adjustment device enters the receiving cavity from the inner cavity of the base station through the first ventilation part 2212, and the hot air after cooling the UAV 20 returns to the inner cavity of the base station from the receiving cavity through the second ventilation part 211. The temperature adjustment device is used for cooling, and such a cycle can effectively reduce the temperature of the body or the battery of the UAV 20 . Of course, in a low temperature environment, warm air may also be blown by the temperature adjustment device of the base station 10 of the unmanned aerial vehicle to flow in the air channel, thereby increasing the temperature of the body of the unmanned aerial vehicle 20 .

在其他实施例中,所述遥控装置包括射频识别天线(图中未示出),所述射频识别天线设置在所述定位点230的下方,用于对需降落的无人飞行器20进行身份验证。In other embodiments, the remote control device includes a radio frequency identification antenna (not shown in the figure), and the radio frequency identification antenna is disposed below the positioning point 230 and is used to authenticate the unmanned aerial vehicle 20 to be landed .

进一步的,所述无人飞行器基站10还设置有环境监测装置(图中未示出),所述环境监测装置采集的环境数据信息通过所述遥控装置传输至后台服务器,其中,所述环境数据信息包括温度信息、湿度信息、光照强度信息、降雨量信息、风速信息等。无人飞行器20的飞行需要满足一定的飞行条件,比如无人飞行器20室外工作的温度范围为-20℃至45℃,室外工作的风速范围为0m/s至12m/s,当温度或风速等超出工作范围时,或者在降雨天气,则不利于无人飞行器20的飞行,因此通过对环境数据信息的采集,并判断温度信息、湿度信息、光照强度信息、降雨量信息、风速信息等环境数据信息是否在正常范围之内,若任意一项超出正常范围,则认为环境数据信息出现异常,此时需尽快控制无人飞行器20返航或者停止无人飞行器20起飞,确保无人飞行器20在适宜的环境条件下执行飞行任务,保证无人飞行器20在户外长期存放或者工作时的安全性和可靠性。Further, the UAV base station 10 is also provided with an environmental monitoring device (not shown in the figure), and the environmental data information collected by the environmental monitoring device is transmitted to the background server through the remote control device, wherein the environmental data The information includes temperature information, humidity information, light intensity information, rainfall information, wind speed information, and the like. The flight of the UAV 20 needs to meet certain flight conditions. For example, the temperature range of the UAV 20 for outdoor operation is -20°C to 45°C, and the wind speed range for outdoor operation is 0m/s to 12m/s. When the temperature or wind speed, etc. When it exceeds the working range or in rainy weather, it is not conducive to the flight of the UAV 20. Therefore, through the collection of environmental data information, environmental data such as temperature information, humidity information, light intensity information, rainfall information, and wind speed information are judged. Whether the information is within the normal range, if any item exceeds the normal range, it is considered that the environmental data information is abnormal. At this time, it is necessary to control the unmanned aerial vehicle 20 to return as soon as possible or stop the unmanned aerial vehicle 20 from taking off to ensure that the unmanned aerial vehicle 20 is in a suitable The flight mission can be performed under environmental conditions to ensure the safety and reliability of the unmanned aerial vehicle 20 during long-term storage or work outdoors.

进一步的,所述无人飞行器基站10还设置有显示装置(图中未示出),用于显示无人飞行器基站10的状态信息、环境监测装置采集的环境数据信息以及无人飞行器20的状态信息,可以更加方便地面工作人员对基站各设备仪器进行维护。在其他实施例中,为方便维护,所述壳体100上开设有操作门110,以用于调试所述壳体100内部的器件。Further, the UAV base station 10 is also provided with a display device (not shown in the figure) for displaying the status information of the UAV base station 10, the environmental data information collected by the environmental monitoring device and the state of the UAV 20. The information can be more convenient for the ground staff to maintain the equipment and instruments of the base station. In other embodiments, in order to facilitate maintenance, the housing 100 is provided with an operation door 110 for debugging the devices inside the housing 100 .

进一步的,所述无人飞行器基站10还设置有备用电源(图中未示出),在无人飞行器基站10外部供电不稳定或者中断时,所述无人飞行器基站10自动切换至备用电源供电,保证无人飞行器20能够持续与无人飞行器基站10建立连接,自动继续执行作业操作和安全返航,防止因无人飞行器基站10供电不稳定或者中断导致无人飞行器20失去遥控信息而出现事故或者作业中断的情况发生;可选的,所述备用电源为蓄电池,可以通过太阳能电池板对该蓄电池进行充电,也可以采用无人飞行器基站10外部的电源对蓄电池进行充电;在一些实施例中,当无人飞行器基站10切换到备用电源后,且备用电源电量降至一定范围时,无人飞行器基站10将发送返航命令至无人飞行器20,在备用电源电量不足之前保证无人飞行器20安全返航并降落至无人飞行器基站10的停机平台200。Further, the unmanned aerial vehicle base station 10 is also provided with a backup power supply (not shown in the figure), and when the external power supply of the unmanned aerial vehicle base station 10 is unstable or interrupted, the unmanned aerial vehicle base station 10 automatically switches to the backup power supply for power supply. , to ensure that the unmanned aerial vehicle 20 can continue to establish a connection with the unmanned aerial vehicle base station 10, automatically continue to perform operation operations and return home safely, and prevent the unmanned aerial vehicle 20 from losing remote control information due to unstable or interrupted power supply of the unmanned aerial vehicle base station 10. The operation is interrupted; optionally, the backup power source is a battery, which can be charged by a solar panel, or a power source outside the UAV base station 10 can be used to charge the battery; in some embodiments, After the UAV base station 10 is switched to the backup power supply and the power of the backup power supply drops to a certain range, the UAV base station 10 will send a return command to the UAV 20 to ensure that the UAV 20 returns home safely before the backup power supply is insufficient. And land on the parking platform 200 of the base station 10 of the unmanned aerial vehicle.

相对于现有的无人飞行器基站10,上述实施例提供的无人飞行器基站10至少具有如下优点:Compared with the existing unmanned aerial vehicle base station 10, the unmanned aerial vehicle base station 10 provided by the above embodiments has at least the following advantages:

(1)所述无人飞行器基站10的停机平台200结构简单,不需要高精度的机械臂或者定位导航模块即可实现无人飞行器20在停机平台200上的精确降落和定位,一方面降低了停机平台200的设备成本和复杂度,另一方面降低了对无人飞行器20的导航和定位设备的精度要求,通用性强,具有更广的适用范围;(1) The parking platform 200 of the UAV base station 10 has a simple structure, and does not require a high-precision mechanical arm or a positioning and navigation module to realize the precise landing and positioning of the UAV 20 on the parking platform 200. On the one hand, it reduces the The equipment cost and complexity of the parking platform 200, on the other hand, reduces the accuracy requirements for the navigation and positioning equipment of the unmanned aerial vehicle 20, has strong versatility, and has a wider scope of application;

(2)当无人飞行器20降落至停机平台200时,可在停机平台200上对无人飞行器20进行自动充电,由于高精度的定位,充电位231的金属触点的面积可以做到很小,可有效避免大面积裸露的金属触点所存在的安全隐患;(2) When the UAV 20 lands on the parking platform 200, the UAV 20 can be automatically charged on the parking platform 200. Due to the high-precision positioning, the area of the metal contact of the charging position 231 can be made very small. , which can effectively avoid the potential safety hazards of large-area exposed metal contacts;

(3)在对无人飞行器20进行自动充电时,可对无人飞行器20的电池进行有效降温,提升安全性;(3) When the unmanned aerial vehicle 20 is automatically charged, the battery of the unmanned aerial vehicle 20 can be effectively cooled to improve safety;

(4)无人飞行器20降落在停机平台200上存放或者充电时,通过防护组件300对无人飞行器20进行防护,可有效防水、防尘、防高温暴晒等,保证无人飞行器20在户外长期存放时的安全性和可靠性;(4) When the unmanned aerial vehicle 20 is landed on the parking platform 200 for storage or charging, the unmanned aerial vehicle 20 is protected by the protection component 300, which can effectively prevent water, dust, high temperature exposure, etc., to ensure that the unmanned aerial vehicle 20 can be used outdoors for a long time. safety and reliability in storage;

(5)通过采集环境数据信息,可以保证无人飞行器20在适宜的环境条件下自动执行作业,保证无人飞行器20的安全性。(5) By collecting environmental data information, it can be ensured that the unmanned aerial vehicle 20 can automatically perform operations under suitable environmental conditions, and the safety of the unmanned aerial vehicle 20 can be ensured.

(6)通过对基站设置备用电池,可以避免基站因电源不稳定或者断电情况下与无人飞行器20失去联络,保证无人飞行器20能够持续执行作业并安全返航。(6) By setting a backup battery for the base station, it can prevent the base station from losing contact with the UAV 20 due to unstable power supply or power failure, and ensure that the UAV 20 can continue to perform operations and return home safely.

基于上述实施例提供的无人飞行器基站10,本发明实施例还提供一种无人飞行器的降落系统,重新参阅图2,所述无人飞行器20的降落系统包括无人飞行器20和无人飞行器基站10,所述无人飞行器基站10包括遥控装置和停机平台200,其中,所述无人飞行器基站10通过所述遥控装置发送基站的位置信息至所述无人飞行器20,所述无人飞行器20根据所述位置信息飞行至所述停机平台200上方,并进一步降落至所述停机平台200的导向部220上,沿着所述导向部220的导向面221滑落至所述停机平台200的停机区域210中,同时在所述停机区域210内设置的定位点230完成定位。在本实施例中,所述无人飞行器20上装设有RTK(Real-time kinematic)定位模块,所述无人飞行器20通过所述RTK定位模块接收并处理所述位置信息,以获得精准定位信息。Based on the unmanned aerial vehicle base station 10 provided in the above embodiment, the embodiment of the present invention further provides a landing system for an unmanned aerial vehicle. Referring to FIG. 2 again, the landing system for the unmanned aerial vehicle 20 includes an unmanned aerial vehicle 20 and an unmanned aerial vehicle. The base station 10, the unmanned aerial vehicle base station 10 includes a remote control device and a parking platform 200, wherein the unmanned aerial vehicle base station 10 sends the location information of the base station to the unmanned aerial vehicle 20 through the remote control device, and the unmanned aerial vehicle 20 flies to the top of the parking platform 200 according to the position information, and further descends on the guide portion 220 of the parking platform 200, and slides down along the guide surface 221 of the guide portion 220 to the stop of the parking platform 200 In the area 210, at the same time, the positioning point 230 set in the parking area 210 completes the positioning. In this embodiment, an RTK (Real-time kinematic) positioning module is installed on the UAV 20, and the UAV 20 receives and processes the position information through the RTK positioning module to obtain precise positioning information .

进一步的,停机平台200包括停机区域210,与停机区域210邻接的导向部220,以及设置在停机区域210内的定位点230;其中,所述导向部220环绕所述停机区域210以限定所述停机区域210的大小,所述导向部220包括面向所述停机区域210的导向面221,当无人飞行器20需要降落至所述停机平台200时,遥控装置发送无人飞行器基站10的位置信息至无人飞行器20,用于使无人飞行器20根据所述位置信息飞行至停机平台200上方,并降落至导向部220上,沿着导向部220的导向面221滑落至停机区域210中,同时在定位点230完成定位。当所述无人飞行器20根据所述位置信息飞行至所述停机平台200的上方时,所述无人飞行器20的脚架在所述停机平台200上的投影位于所述导向部220所在的区域和/或所述停机区域210中。Further, the parking platform 200 includes a parking area 210, a guide portion 220 adjacent to the parking area 210, and a positioning point 230 disposed in the parking area 210; wherein, the guide portion 220 surrounds the parking area 210 to define the The size of the parking area 210, the guide part 220 includes a guide surface 221 facing the parking area 210, when the UAV 20 needs to land on the parking platform 200, the remote control device sends the location information of the UAV base station 10 to The unmanned aerial vehicle 20 is used to make the unmanned aerial vehicle 20 fly to the top of the parking platform 200 according to the position information, and land on the guide part 220, slide down to the parking area 210 along the guide surface 221 of the guide part 220, and at the same time The positioning point 230 completes the positioning. When the UAV 20 flies above the parking platform 200 according to the position information, the projection of the tripod of the UAV 20 on the parking platform 200 is located in the area where the guide portion 220 is located and/or in the shutdown area 210 .

在一些实施例中,所述停机平台200可以包括两个及以上所述停机区域210,所述导向部220限定整体停机区域210的大小,相邻的所述停机区域210之间设置有隔离件(图中未示出),每个所述停机区域210设置有所述定位点230。In some embodiments, the parking platform 200 may include two or more parking areas 210 , the guide portion 220 defines the size of the entire parking area 210 , and spacers are provided between adjacent parking areas 210 . (not shown in the figure), each of the parking areas 210 is provided with the positioning point 230 .

进一步的,所述定位点230上设有充电位231,所述无人飞行器20在所述定位点230完成定位后,所述充电位231与所述无人飞行器20的脚架电接触,实现所述无人飞行器基站10与所述无人飞行器20的电连接。Further, the positioning point 230 is provided with a charging position 231. After the unmanned aerial vehicle 20 is positioned at the positioning point 230, the charging position 231 is in electrical contact with the tripod of the unmanned aerial vehicle 20. Electrical connection between the UAV base station 10 and the UAV 20 .

在一些实施例中,所述充电位231上设置成对的金属触点,其中成对设置的所述金属触点分别连接充电电源的不同电极。In some embodiments, the charging position 231 is provided with a pair of metal contacts, wherein the pair of metal contacts are respectively connected to different electrodes of the charging power source.

在另一些实施例中,所述停机平台200包括成对设置的定位点230,所述定位点230上设有充电位231,所述充电位231上设置金属触点,成对设置的所述定位点230上的金属触点分别连接充电电源的不同电极,即其中一个定位点230上的金属触点连接充电电源的正极,另一个定位点230上的金属触点连接充电电源的负极。In other embodiments, the stopping platform 200 includes positioning points 230 arranged in pairs, charging positions 231 are arranged on the positioning points 230, metal contacts are arranged on the charging positions 231, and the paired The metal contacts on the positioning points 230 are respectively connected to different electrodes of the charging power supply, that is, the metal contact on one positioning point 230 is connected to the positive pole of the charging power supply, and the metal contact on the other positioning point 230 is connected to the negative pole of the charging power supply.

可选的,前述实施例中所述的充电位231上设置的金属触点可以包括充电金属触点和数据传输金属触点,无人飞行器20在通过充电金属触点进行充电的同时,还可以通过数据传输金属触点实现与基站的有线通信,进行不同类型的数据交互,比如升级无人飞行器20飞控系统。Optionally, the metal contacts provided on the charging position 231 described in the foregoing embodiments may include charging metal contacts and data transmission metal contacts, and the unmanned aerial vehicle 20 can also be charged through the charging metal contacts while charging. The wired communication with the base station is realized through the data transmission metal contacts, and different types of data interaction are carried out, such as upgrading the flight control system of the unmanned aerial vehicle 20.

可选的,在前述定位点230上还设置有限位部232,该限位部232能够与无人飞行器20脚架上的底部配合,限定无人飞行器20在平面上的运动,比如该限位部232为限位凹槽,无人飞行器20脚架设置有凸起,当无人飞行器20降落至所述导向部220上时沿着所述导向面221滑落至所述停机区域210中时,无人飞行器20的充电触点定位至所述定位点230的同时,无人飞行器20脚架底部的凸起正好定位至该限位凹槽中,使无人飞行器20不能在停机区域210所在的平面内平移或转动;由于无人飞行器20可以在导向部220的作用下滑落至停机区域210完成精确定位,因此,即使在充电位231上的金属触点面积较小时,无人飞行器20的脚架也能精确接触充电位231上的金属触点,实现无人飞行器20与无人飞行器基站10的点连接,进而实现无人飞行器20的充电;在具体实施例中,所述充电位231位于所述限位部232中,也可以位于所述限位部232的一侧。Optionally, a limiting portion 232 is also provided on the aforementioned positioning point 230, and the limiting portion 232 can cooperate with the bottom of the tripod of the unmanned aerial vehicle 20 to limit the movement of the unmanned aerial vehicle 20 on the plane. The portion 232 is a limiting groove, and the tripod of the unmanned aerial vehicle 20 is provided with a protrusion. When the unmanned aerial vehicle 20 falls on the guide portion 220 and slides down into the parking area 210 along the guide surface 221, When the charging contact of the UAV 20 is positioned to the positioning point 230, the protrusion at the bottom of the tripod of the UAV 20 is just positioned in the limiting groove, so that the UAV 20 cannot be located where the parking area 210 is located. Translation or rotation in the plane; since the unmanned aerial vehicle 20 can slide down to the parking area 210 under the action of the guide part 220 to complete precise positioning, even when the metal contact area on the charging position 231 is small, the feet of the unmanned aerial vehicle 20 The rack can also precisely contact the metal contacts on the charging position 231 to realize the point connection between the unmanned aerial vehicle 20 and the unmanned aerial vehicle base station 10, thereby realizing the charging of the unmanned aerial vehicle 20; in a specific embodiment, the charging position 231 is located at The limiting portion 232 may also be located on one side of the limiting portion 232 .

在另一些实施例中,可以在所述停机区域210中临近所述定位点230设置有限位部232,参阅图3,所述定位点230包括围绕该限位部232周向设置的多个充电位231,这样可以在无人飞行器20以不同的方位降落至停机区域210时,无人飞行器20脚架均能与充电位231的金属触点接触。In other embodiments, a limiting portion 232 may be provided in the parking area 210 adjacent to the positioning point 230 . Referring to FIG. 3 , the positioning point 230 includes a plurality of charging points circumferentially arranged around the limiting portion 232 . Position 231, so that when the unmanned aerial vehicle 20 lands in the parking area 210 in different directions, the legs of the unmanned aerial vehicle 20 can all be in contact with the metal contacts of the charging position 231.

在其他实施例中,所述定位点230还设置有活动盖板(图中未示出),或者仅仅是在所述定位点230的充电位231处设置有活动盖板,该活动盖板在无人飞行器20降落时或者充电时自动打开,在无人飞行器20充电完毕或者起飞后自动关闭,以保护裸露的金属触点,该活动盖板可以设置成翻转形式,也可以设置成推拉形式。In other embodiments, the positioning point 230 is also provided with a movable cover plate (not shown in the figure), or only a movable cover plate is provided at the charging position 231 of the positioning point 230, and the movable cover plate is located at the charging position 231 of the positioning point 230. The UAV 20 is automatically opened when landing or charging, and automatically closed when the UAV 20 is fully charged or taken off to protect the exposed metal contacts.

在一些实施例中,导向部220可以包含多个面向所述停机区域210的导向面221,每一个导向面221可以是相对停机区域210倾斜的平面或者曲面,从而在所述停机区域210上方形成一个凹陷,所述凹陷用于收容所述无人飞行器20。停机区域210的形状和大小由环绕停机区域210的导向部220来限定,比如停机区域210导向部220包括形状大小一致的四个第一导向面2210和形状大小一致的四个第二导向面2211,该四个所述第一导向面2210与所述停机区域210的对应的边连接,四个所述第二导向面2211中每一个第二导向面2211连接在对应相邻的两个第一导向面2210之间,从而限定出一矩形区域,该矩形区域即为停机区域210,一般地,停机区域210的形状和大小与无人飞行器20脚架的形状和尺寸相匹配。在一些实施例中,导向部220可以是导向板或者导向台。In some embodiments, the guide portion 220 may include a plurality of guide surfaces 221 facing the parking area 210 , and each guide surface 221 may be a plane or curved surface inclined relative to the parking area 210 , so as to be formed above the parking area 210 A recess for receiving the UAV 20 . The shape and size of the parking area 210 are defined by the guide parts 220 surrounding the parking area 210 . For example, the guide part 220 of the parking area 210 includes four first guide surfaces 2210 with the same shape and size and four second guide surfaces 2211 with the same shape and size , the four first guide surfaces 2210 are connected with the corresponding edges of the parking area 210 , and each of the four second guide surfaces 2211 is connected with the corresponding adjacent two first guide surfaces 2211 A rectangular area is defined between the guide surfaces 2210 , and the rectangular area is the parking area 210 . Generally, the shape and size of the parking area 210 match the shape and size of the tripod of the UAV 20 . In some embodiments, the guide portion 220 may be a guide plate or a guide table.

进一步的,所述无人飞行器基站10还包括防护组件300,所述防护组件300用于防护所述停机平台200以及降落在所述停机平台200上的所述无人飞行器20。其中,所述防护组件300位于所述停机平台200上方,所述防护组件300与所述停机平台200配合形成所述无人飞行器20的收容腔。所述防护组件300用于防护所述停机平台200以及降落在所述停机平台200上的无人飞行器20。在本实施例中,防护组件300可以实现防尘、防水、防高温暴晒等效果,形成有效保护无人飞行器20在户外长期作业时的安全存放环境。Further, the UAV base station 10 further includes a protection component 300 for protecting the parking platform 200 and the UAV 20 landing on the parking platform 200 . Wherein, the protective assembly 300 is located above the parking platform 200 , and the protective assembly 300 cooperates with the parking platform 200 to form a receiving cavity of the unmanned aerial vehicle 20 . The protection assembly 300 is used to protect the parking platform 200 and the unmanned aerial vehicle 20 landing on the parking platform 200 . In this embodiment, the protective component 300 can achieve the effects of dustproof, waterproof, and high temperature exposure protection, thereby forming a safe storage environment that effectively protects the unmanned aerial vehicle 20 during long-term operation outdoors.

在一些实施例中,所述防护组件300包括驱动件310和防护门320,所述防护组件300在所述无人飞行器20降落至所述停机平台200前通过所述驱动件310打开所述防护门320,并在所述无人飞行器20降落至所述停机平台200后通过所述驱动件310关闭所述防护门320。所述防护门320可以是单开或者双开的平面门,也可以是盒状或者半球状的异形门,该异性门也可设置成单开或者双开形式;作为可选方案,所述防护门320上可设置透明视窗。在另一些可选方案中,所述防护组件300还包括设置在所述防护门320上的密封圈,所述密封圈可为橡胶圈。In some embodiments, the guard assembly 300 includes a drive member 310 and a guard door 320 , and the guard assembly 300 opens the guard through the drive member 310 before the UAV 20 descends to the parking platform 200 . The protective door 320 is closed by the driving member 310 after the UAV 20 descends to the parking platform 200 . The protective door 320 can be a single-opening or double-opening plane door, or a box-shaped or hemispherical special-shaped door, and the heterosexual door can also be set to a single-opening or double-opening form; as an optional solution, the protective door 320 Transparent windows can be set on the top. In other optional solutions, the protection assembly 300 further includes a sealing ring disposed on the protection door 320, and the sealing ring may be a rubber ring.

在一些实施例中,所述驱动件310可以为顶升气缸,所述顶升气缸的活塞杆与所述防护门320固定连接,以带动所述防护门320在竖直方向上移动,完成防护门320的开启和关闭。In some embodiments, the driving member 310 may be a jacking cylinder, and the piston rod of the jacking cylinder is fixedly connected to the protective door 320 to drive the protective door 320 to move in the vertical direction to complete the protection Opening and closing of door 320.

在另一些实施例中,所述防护组件300还包括连接组件330,所述连接组件330连接所述防护门320与所述壳体100。In other embodiments, the protective assembly 300 further includes a connecting assembly 330 , and the connecting assembly 330 connects the protective door 320 and the housing 100 .

作为可选方案,重新参阅图4,所述连接组件330为外铰链的结构,具体包括第一连接部331、第二连接部332和转轴333,所述第一连接部331和第二连接部332分别连接所述防护门320与所述壳体100的外表面,所述转轴333与所述驱动件310连接,所述第一连接部331和所述第二连接部332通过所述转轴333实现转动连接;第一连接部331和第二连接部332的连接面采用大面积连接面,通过螺丝或者铆钉将第一连接部331和第二连接部332分别固定在所述防护门320与所述壳体100的外表面上,转轴333与第一连接部331固定连接,同时转轴333通过轴承安装在第二连接部332上设置的轴承座上,通过驱动件310带动转轴333转动,从而带动在第一连接部331和防护门320整体运动,实现防护门320的开启和关闭;本实施例中,所述防护组件300包括多个连接组件330,该多个连接组件330的转轴333同轴,且其中一个所述连接组件330的转轴333与所述驱动件310连接,在本实施例中,所述连接组件330可调节,以保证多个连接组件330的转轴的同轴度;由于连接组件330采用外铰链的结构,可以展开更大的角度,使得防护门320的开合范围更大,同时采用外铰链机构,当防护门320闭合时,防护门320与壳体100完全闭合,形成相对密封的无人飞行器20收纳腔,有利于防尘和防水等,同时,第一连接部331和第二连接部332采用大面积的连接面,可以增加防护门320稳定性和侧面抗风抗冲击的能力,在大风天气保证防护门320能够安全打开和关闭。As an optional solution, referring to FIG. 4 again, the connecting assembly 330 is an external hinge structure, and specifically includes a first connecting portion 331 , a second connecting portion 332 and a rotating shaft 333 . The first connecting portion 331 and the second connecting portion 331 332 are respectively connected to the protective door 320 and the outer surface of the housing 100 , the rotating shaft 333 is connected to the driving member 310 , the first connecting part 331 and the second connecting part 332 pass through the rotating shaft 333 The connection surface of the first connection part 331 and the second connection part 332 adopts a large-area connection surface, and the first connection part 331 and the second connection part 332 are respectively fixed on the protective door 320 and the protective door 320 by screws or rivets. On the outer surface of the housing 100, the rotating shaft 333 is fixedly connected with the first connecting portion 331, and at the same time, the rotating shaft 333 is mounted on the bearing seat provided on the second connecting portion 332 through the bearing, and the rotating shaft 333 is driven to rotate by the driving member 310, thereby driving the rotating shaft 333 to rotate. The first connecting portion 331 and the protective door 320 move as a whole to realize the opening and closing of the protective door 320; in this embodiment, the protective assembly 300 includes a plurality of connecting assemblies 330, and the rotating shafts 333 of the plurality of connecting assemblies 330 are coaxial , and the rotating shaft 333 of one of the connecting assemblies 330 is connected with the driving member 310. In this embodiment, the connecting assembly 330 can be adjusted to ensure the coaxiality of the rotating shafts of the multiple connecting assemblies 330; The assembly 330 adopts the structure of the outer hinge, which can be unfolded to a larger angle, so that the opening and closing range of the protective door 320 is larger, and the outer hinge mechanism is adopted at the same time. The relatively sealed storage cavity of the unmanned aerial vehicle 20 is conducive to dustproof and waterproof, etc. At the same time, the first connecting part 331 and the second connecting part 332 adopt large-area connecting surfaces, which can increase the stability of the protective door 320 and the side wind resistance. The impact capability ensures that the protective door 320 can be opened and closed safely in windy weather.

作为可选方案,所述连接组件330包括导轨(图未示出)和滑动座(图未示出),所述导轨与所述防护门320和所述壳体100中的一个固定连接,所述滑动座与所述防护门320和所述壳体100中的另一个固定连接,所述驱动件310与所述滑动座连接。As an optional solution, the connecting assembly 330 includes a guide rail (not shown in the figure) and a sliding seat (not shown in the figure), and the guide rail is fixedly connected with one of the protective door 320 and the housing 100, so The sliding seat is fixedly connected with the other one of the protective door 320 and the housing 100 , and the driving member 310 is connected with the sliding seat.

进一步的,所述无人飞行器基站10装设有射频识别天线,所述射频识别天线设置在所述定位点230的下方,在所述无人飞行器20降落至所述停机平台200前,所述无人飞行器基站10通过所述射频识别天线对所述无人飞行器20进行身份验证。Further, the unmanned aerial vehicle base station 10 is equipped with a radio frequency identification antenna, and the radio frequency identification antenna is arranged below the positioning point 230 . The UAV base station 10 authenticates the UAV 20 through the radio frequency identification antenna.

进一步的,所述无人飞行器基站10还设置有环境监测装置,所述环境监测装置采集的环境数据信息通过所述遥控装置传输至后台服务器,当所述后台服务器判定所述环境数据信息出现异常时,所述无人飞行器基站10通过遥控装置向所述无人飞行器20发送返航命令。具体的,所述环境监测装置采集的环境数据信息通过所述遥控装置传输至后台服务器,其中,所述环境数据信息包括温度信息、湿度信息、光照强度信息、降雨量信息、风速信息等。无人飞行器20的飞行需要满足一定的飞行条件,比如无人飞行器20室外工作的温度范围为-20℃至45℃,室外工作的风速范围为0m/s至12m/s,当温度或风速等超出工作范围时,或者在降雨天气,则不利于无人飞行器20的飞行,因此通过对环境数据信息的采集,并判断温度信息、湿度信息、光照强度信息、降雨量信息、风速信息等环境数据信息是否在正常范围之内,若任意一项超出正常范围,则认为环境数据信息出现异常,此时需尽快控制无人飞行器20返航或者停止无人飞行器20起飞,确保无人飞行器20在适宜的环境条件下执行飞行任务,保证无人飞行器20在户外长期存放或者工作时的安全性和可靠性。Further, the UAV base station 10 is also provided with an environmental monitoring device, and the environmental data information collected by the environmental monitoring device is transmitted to the background server through the remote control device. When the background server determines that the environmental data information is abnormal , the UAV base station 10 sends a return command to the UAV 20 through a remote control device. Specifically, the environmental data information collected by the environmental monitoring device is transmitted to the background server through the remote control device, wherein the environmental data information includes temperature information, humidity information, light intensity information, rainfall information, wind speed information, and the like. The flight of the UAV 20 needs to meet certain flight conditions. For example, the temperature range of the UAV 20 for outdoor operation is -20°C to 45°C, and the wind speed range for outdoor operation is 0m/s to 12m/s. When the temperature or wind speed, etc. When it exceeds the working range or in rainy weather, it is not conducive to the flight of the UAV 20. Therefore, through the collection of environmental data information, environmental data such as temperature information, humidity information, light intensity information, rainfall information, and wind speed information are judged. Whether the information is within the normal range, if any item exceeds the normal range, it is considered that the environmental data information is abnormal. At this time, it is necessary to control the unmanned aerial vehicle 20 to return as soon as possible or stop the unmanned aerial vehicle 20 from taking off to ensure that the unmanned aerial vehicle 20 is in a suitable The flight mission can be performed under environmental conditions to ensure the safety and reliability of the unmanned aerial vehicle 20 during long-term storage or work outdoors.

进一步的,所述无人飞行器基站10还设置有温度调节装置,所述无人飞行器20降落至所述停机平台200后,所述无人飞行器基站10启动所述温度调节装置以调节基站内部的温度。可选的,在无人飞行器基站10的导向部220包括多个面向所述停机区域210的所述导向面221,在部分或全部所述导向面221上设置有第一通风部2212,无人飞行器20可能由于充电导致电池升温或者在高温下作业导致机身升温,这些情况下无人飞行器20降落在停机平台200的停机区域210时,可通过导向面221设置的第一通风部2212送风,对无人飞行器20的机身或者电池进行降温;在其他实施例中,所述导向部220背离所述停机区域210的一侧设置有导流风扇(图中未示出),该导流风扇的扇叶大小与导向面221上设置的第一通风部2212的大小相适配;作为一种可选的实施例,所述第一通风部2212为网状通风口或者是栅状通风口。Further, the unmanned aerial vehicle base station 10 is further provided with a temperature adjustment device, after the unmanned aerial vehicle 20 landed on the parking platform 200, the unmanned aerial vehicle base station 10 activates the temperature adjustment device to adjust the temperature inside the base station. temperature. Optionally, the guide portion 220 of the UAV base station 10 includes a plurality of the guide surfaces 221 facing the parking area 210, and a first ventilation portion 2212 is provided on some or all of the guide surfaces 221, so that there is no unmanned aerial vehicle. The battery of the aircraft 20 may heat up due to charging or the fuselage may heat up due to operation at high temperature. In these cases, when the unmanned aircraft 20 lands in the parking area 210 of the parking platform 200 , the air can be supplied through the first ventilation portion 2212 provided on the guide surface 221 . , to cool the fuselage or battery of the unmanned aerial vehicle 20; in other embodiments, a diversion fan (not shown in the figure) is provided on the side of the guide portion 220 away from the parking area 210. The size of the fan blades of the fan is adapted to the size of the first ventilation portion 2212 provided on the guide surface 221; as an optional embodiment, the first ventilation portion 2212 is a mesh-shaped ventilation port or a grid-shaped ventilation port .

进一步地,所述停机区域210设置有第二通风部211,作为一种可选的实施例,停机区域210设置的第二通风部211包括若干有序排列的通孔,这些通孔可以环绕定位点230设置。当然,停机区域210设置的第二通风部211也可以为网状通风口或者是栅状通风口,可选的,在所述停机区域210的背部也可以装设导流风扇。Further, the stop area 210 is provided with a second ventilation part 211. As an optional embodiment, the second ventilation part 211 provided in the stop area 210 includes a plurality of through holes arranged in an orderly manner, and these through holes can be positioned around Point 230 Settings. Of course, the second ventilation part 211 provided in the shutdown area 210 may also be a mesh ventilation port or a grid ventilation port. Optionally, a guide fan may also be installed at the back of the shutdown area 210 .

当无人飞行器20降落在停机平台200上,且在停机平台200上方设置的防护组件300的防护门320关闭时,由上述的基站内腔、第一通风部2212和第二通风部211、收容腔共同组成循环的空气流道,在导流风扇的作用下,无人飞行器基站10的温度调节装置吹出的冷风在该空气流道中流动,重新参阅图1,图中的黑色空心箭头标识了空气流动方向,具体的,在导流风扇的作用下,温度调节装置输出的冷风从基站内腔通过第一通风部2212进入收容腔,冷却无人飞行器20后的热风再从收容腔通过第二通风部211回到基站内腔由温度调节装置进行冷却,如此循环,可有效降低无人飞行器20的机身或电池温度。当然,在低温环境中,也可以是由无人飞行器基站10的温度调节装置吹出暖风在该空气流道中流动,提高无人飞行器20的机身温度。When the UAV 20 lands on the parking platform 200 and the protective door 320 of the protective assembly 300 provided above the parking platform 200 is closed, the above-mentioned base station inner cavity, the first ventilation part 2212 and the second ventilation part 211 , contain The cavities together form a circulating air flow channel. Under the action of the diversion fan, the cold air blown by the temperature adjustment device of the UAV base station 10 flows in the air flow channel. Referring to Figure 1 again, the black hollow arrow in the figure marks the air flow. The flow direction, specifically, under the action of the guide fan, the cold air output by the temperature adjustment device enters the receiving cavity from the inner cavity of the base station through the first ventilation part 2212, and the hot air after cooling the UAV 20 passes through the second ventilation from the receiving cavity. The part 211 is returned to the inner cavity of the base station to be cooled by the temperature adjusting device, and such a cycle can effectively reduce the temperature of the body or the battery of the UAV 20 . Of course, in a low temperature environment, warm air may also be blown by the temperature adjustment device of the base station 10 of the unmanned aerial vehicle to flow in the air channel, thereby increasing the temperature of the body of the unmanned aerial vehicle 20 .

基于上述实施例提供的无人飞行器基站10和无人飞行器的降落系统,本发明实施例还提供一种无人飞行器的降落方法,参阅图5,所述方法包括:Based on the unmanned aerial vehicle base station 10 and the landing system of the unmanned aerial vehicle provided by the above-mentioned embodiments, the embodiment of the present invention also provides a landing method of the unmanned aerial vehicle. Referring to FIG. 5 , the method includes:

S101、无人飞行器基站10通过遥控装置发送基站位置信息至无人飞行器20;可选的,在S101之前,所述无人飞行器基站10通过环境监测装置采集的环境数据信息,并在所述环境数据信息出现异常时发送返航命令至所述无人飞行器20,其中,所述环境数据信息包括如下的一种或多种:温度信息、湿度信息、光照强度信息、降雨量信息和风速信息。S101. The UAV base station 10 sends the base station location information to the UAV 20 through the remote control device; optionally, before S101, the UAV base station 10 collects the environmental data information through the environment monitoring device, and sends the information to the UAV 20 in the environment. Send a return command to the UAV 20 when the data information is abnormal, wherein the environmental data information includes one or more of the following: temperature information, humidity information, light intensity information, rainfall information and wind speed information.

S102、所述无人飞行器20根据所述位置信息飞行至所述无人飞行器基站10的停机平台200上方;具体的,所述无人飞行器20的脚架在所述停机平台200上的投影位于所述导向部220所在的区域和/或所述停机区域210中。S102, the UAV 20 flies to the top of the parking platform 200 of the UAV base station 10 according to the position information; specifically, the projection of the tripod of the UAV 20 on the parking platform 200 is at In the area where the guide portion 220 is located and/or the parking area 210 .

S103、所述无人飞行器20降落至所述停机平台200的导向部220上,沿着所述导向部220的导向面221滑落至所述停机平台200的停机区域210中,同时在所述停机区域210内设置的定位点230完成定位。S103. The unmanned aerial vehicle 20 is landed on the guide portion 220 of the parking platform 200, and slides down to the parking area 210 of the parking platform 200 along the guide surface 221 of the guide portion 220. The positioning point 230 set in the area 210 completes the positioning.

进一步的,在步骤S102之前还包括:Further, before step S102, it also includes:

所述无人飞行器基站10打开位于所述停机平台200上方的防护组件300的防护门320;相对应的,在步骤S103之后所述无人飞行器基站10关闭位于所述停机平台200上方的防护组件300的防护门320。The UAV base station 10 opens the protective door 320 of the protective assembly 300 located above the parking platform 200; correspondingly, after step S103, the UAV base station 10 closes the protective assembly located above the parking platform 200 300 of the protective door 320.

进一步的,在步骤S103之后还包括:所述无人飞行器基站10通过所述定位点230上设置的充电位231对所述无人飞行器20进行充电。Further, after step S103 , the method further includes: the unmanned aerial vehicle base station 10 charges the unmanned aerial vehicle 20 through the charging position 231 set on the positioning point 230 .

进一步的,在在步骤S103之后还包括:所述无人飞行器基站10开启温度调节装置。Further, after step S103, the method further includes: the UAV base station 10 turns on the temperature adjustment device.

本发明实施例提供的无人飞行器的降落方法中所涉及的硬件设备的结构和功能可参阅前述实施例中有关的技术内容,在此不再赘述。For the structure and function of the hardware device involved in the landing method of the unmanned aerial vehicle provided by the embodiment of the present invention, reference may be made to the related technical content in the foregoing embodiment, and details are not repeated here.

显然,以上所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例,附图中给出了本发明的较佳实施例,但并不限制本发明的专利范围。本发明可以以许多不同的形式来实现,相反地,提供这些实施例的目的是使对本发明的公开内容的理解更加透彻全面。尽管参照前述实施例对本发明进行了详细的说明,对于本领域的技术人员来而言,其依然可以对前述各具体实施方式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效替换。凡是利用本发明说明书及附图内容所做的等效结构,直接或间接运用在其他相关的技术领域,均同理在本发明专利保护范围之内。Obviously, the above-described embodiments are only a part of the embodiments of the present invention, not all of the embodiments. The accompanying drawings show the preferred embodiments of the present invention, but do not limit the patent scope of the present invention. The present invention may be embodied in many different forms, rather, these embodiments are provided so that a thorough and complete understanding of the present disclosure will be provided. Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing specific embodiments, or perform equivalent replacements for some of the technical features. . Any equivalent structures made by using the contents of the description and the accompanying drawings of the present invention, which are directly or indirectly applied in other related technical fields, are all within the protection scope of the patent of the present invention.

Claims (14)

1. An unmanned aerial vehicle base station, comprising:
the system comprises a shell, a shutdown platform and a radio frequency identification antenna; the shutdown platform and the shell are matched to form a relatively closed base station inner cavity, and the radio frequency identification antenna is used for verifying the identity of the unmanned aerial vehicle before the unmanned aerial vehicle lands to a shutdown area of the shutdown platform.
2. The UAV base station of claim 1, wherein the outage area has a location point disposed therein, and wherein the RFID antenna is disposed below the location point.
3. The unmanned aerial vehicle base station of claim 1, further comprising an environment monitoring device and a remote control device, wherein the environment data information collected by the environment monitoring device is transmitted to the background server through the remote control device.
4. The UAV base station of claim 3, wherein the environment data information includes one or more of: temperature information, humidity information, illumination intensity information, rainfall information, and wind speed information.
5. The UAV base station according to claim 3 or 4, wherein when the background server determines that the environmental data information is abnormal, the UAV base station sends a return command to the UAV through the remote control device.
6. The UAV base station of claim 1 further provided with a temperature regulation device for regulating the temperature inside the base station.
7. The UAV base station of claim 6 wherein a plurality of first vents are provided in the UAV base station facing the outage area, the thermostat blowing air to the UAV via the first vents when the UAV is to be dropped into the outage area.
8. An unmanned aerial vehicle base station according to claim 6 or 7, wherein a second vent is provided in the outage area.
9. The UAV base station of claim 8 wherein a plurality of induced draft fans are further disposed therein, at least some of the induced draft fans being disposed on a side of the first vent portion facing away from the parking area.
10. The UAV base station of any one of claims 6-9 further comprising a guard assembly positioned above the shut-down platform and cooperating with the shut-down platform to form a receiving cavity for the UAV.
11. The UAV base station of claim 10 wherein the base station cavity, the receiving cavity, the first vent and the second vent collectively comprise a circulating air flow path.
12. The UAV base station of claim 11, wherein the cold air from the thermostat enters the receiving cavity from the base station cavity via the first vent to cool the UAV, and the hot air from the base station cavity is returned to the base station cavity via the second vent and cooled by the thermostat.
13. A landing system for an unmanned aerial vehicle, comprising an unmanned aerial vehicle and an unmanned aerial vehicle base station as claimed in any one of claims 1 to 12.
14. A method of landing an unmanned aerial vehicle, comprising:
the unmanned aerial vehicle base station sends base station position information to the unmanned aerial vehicle through the remote control device;
the unmanned aerial vehicle flies above a shutdown platform of the unmanned aerial vehicle base station according to the position information;
the unmanned aerial vehicle base station carries out identity verification on the unmanned aerial vehicle through a radio frequency identification antenna;
after the identity authentication is passed, the unmanned aerial vehicle lands on the shutdown platform.
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