WO2020238137A1 - 无人机驻停装置及无人机停机系统 - Google Patents

无人机驻停装置及无人机停机系统 Download PDF

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Publication number
WO2020238137A1
WO2020238137A1 PCT/CN2019/123411 CN2019123411W WO2020238137A1 WO 2020238137 A1 WO2020238137 A1 WO 2020238137A1 CN 2019123411 W CN2019123411 W CN 2019123411W WO 2020238137 A1 WO2020238137 A1 WO 2020238137A1
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WO
WIPO (PCT)
Prior art keywords
drone
blades
parking device
frame
supporting member
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PCT/CN2019/123411
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English (en)
French (fr)
Inventor
崔鹏
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北京三快在线科技有限公司
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Application filed by 北京三快在线科技有限公司 filed Critical 北京三快在线科技有限公司
Publication of WO2020238137A1 publication Critical patent/WO2020238137A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND 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
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/007—Helicopter portable landing pads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND 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
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells

Definitions

  • This application relates to the technical field of drones, in particular to a drone parking device and a drone parking system.
  • UAVs have been widely used in civil, industrial and military fields.
  • UAVs can be used for aerial photography, firefighting, surveying and mapping, detection, express delivery, takeaway delivery, etc., but not limited to this.
  • drones are used for express delivery and takeaway delivery, in order to facilitate the direct delivery of goods to the user's home, it is usually necessary to install a drone parking device outside the user.
  • the existing UAV parking device has a complicated structure and high cost.
  • the purpose of this application is to provide a drone parking device and a drone parking system.
  • the UAV parking device is installed on the wall of the building.
  • the UAV parking device includes: a driving device; a traction assembly, including a reel fixedly connected to the output end of the driving device and wound around the reel The rope; a support member for supporting the drone, the support member includes a connecting end and a movable end, the connecting end is rotatably connected with the wall, the movable end is connected with the rope; and a controller, By controlling the driving device, the movable end is switched between the first position and the second position under the action of the rope. When the movable end is in the first position, the supporting member is in an open state, When the movable end is in the second position, the supporting member is in a closed state.
  • the drone parking system includes a drone, including a flight controller; and a drone parking device installed on the wall of a building, the drone parking device including a driving device, a traction component, and a supporting component And a controller, the traction assembly includes a reel fixedly connected to the output end of the driving device and a rope wound around the reel, the support member is used to support the drone, and the support member includes a connecting end and a movable The connecting end is rotatably connected to the wall, the movable end is connected to the rope, the controller is communicatively connected to the flight controller, and the controller is in accordance with instructions from the flight controller.
  • the movable end is switched between the first position and the second position under the action of the rope.
  • the supporting member is in an open state
  • the supporting member is in a closed state.
  • the unmanned aerial vehicle parking device of the present application can realize the switching between the open state and the closed state of the supporting member through a driving device. In this way, the unmanned aerial vehicle parking device has a simple, reliable structure and low cost.
  • Figure 1 is a three-dimensional schematic diagram of the drone parking device of the present application, in which the supporting member is in a closed state;
  • Figure 2 is a three-dimensional schematic diagram of the unmanned aerial vehicle shutdown system of the present application, in which the supporting member is in an open state;
  • Figure 3 is a longitudinal cross-sectional view of the drone parking device shown in Figure 1, wherein the supporting member is in an open state;
  • Figure 4 is a front view of the drone parking device shown in Figure 1, in which the supporting member is in an open state;
  • Fig. 5 is an enlarged view of A shown in Fig. 4;
  • Fig. 6 is a perspective schematic view of the blade shown in Fig. 1;
  • Figure 7 is an enlarged view of B shown in Figure 6;
  • Fig. 8 is a three-dimensional schematic diagram of the drone parking device shown in Fig. 1, in which the supporting member is in an open state, and some of the blades rotate at a certain angle.
  • first, second, third, etc. may be used in this application to describe various information, such information should not be limited to these terms. These terms are only used to distinguish the same type of information from each other.
  • first information may also be referred to as second information, and similarly, the second information may also be referred to as first information.
  • word “if” as used herein can be interpreted as "when” or “when” or "in response to determination”.
  • an embodiment of the present invention provides an unmanned aerial vehicle parking system 1.
  • the unmanned aerial vehicle parking system 1 includes an unmanned aerial vehicle 100 and an unmanned aerial vehicle parking device 600.
  • the drone 100 is used to transport goods, such as express delivery, takeaway, and so on.
  • the drone parking device 600 is used for parking the drone 100 for unloading or loading.
  • the drone 100 includes a fuselage 10, an arm 20, a power unit 30, and a flight controller (not shown).
  • the arm 20 is connected to the body 10.
  • the power device 30 is installed on the arm 20.
  • the power device 30 includes a propeller 31 and a motor 32 for driving the propeller 31 to rotate.
  • the motor 32 drives the propeller 31 to rotate to provide flight power.
  • the flight controller is electrically connected to each functional module of the UAV 100 and coordinates the work of each functional module.
  • the drone parking device 600 is installed on the wall 900 of the building.
  • the drone parking device 600 includes a driving device 40, a traction assembly 50, a supporting member 60, and a controller (not shown).
  • the driving device 40 includes a motor, a hydraulic system, a pneumatic system, and the like. In the illustrated embodiment, the driving device 40 is a motor.
  • the traction assembly 50 includes a reel 51 fixedly connected to the output end of the driving device 40 and a rope 52 wound around the reel 51.
  • the supporting member 60 is used to support the drone 100.
  • the supporting member 60 includes a connecting end 61 and a movable end 62.
  • the connecting end 61 is rotatably connected to the wall.
  • the movable end 62 is connected to the rope 52.
  • the controller communicates with the flight controller, and the controller controls the driving device 40 so that the movable end 62 is between the first position and the second position under the action of the rope 52.
  • the controller controls the drive device 40 to start, and the reel 51 rotates with the output end of the drive device 40, and the rope 52 arranged around the reel 51 is gradually released ,
  • the movable end 62 of the supporting member 60 is switched from the second position to the first position.
  • the supporting member 60 is in an open state, and the drone 100 can be parked on the supporting member 60.
  • the controller controls the driving device 40 to rotate in the reverse direction, so that the rope 52 is wound around the reel 51 again, so that the movable end 62 of the support member 60 is switched from the first position to In the second position, at this time, the supporting member 60 is in a closed state.
  • the controller controls the opening, closing and rotating directions of the driving device 40 based on instructions from the flight controller. In other embodiments, the user controls the opening, closing, and rotating directions of the driving device 40 by directly operating the controller.
  • the support member 60 can be switched between the open state and the closed state through one driving device 40. In this way, the drone parking device 600 has a simple, reliable structure and low cost.
  • the supporting member 60 is switched between the open state and the closed state by rotating.
  • the wall is provided with a through hole that matches the support member 60, and the support member 60 moves back and forth through the through hole to switch between the open state and the closed state.
  • the driving device 40 drives the supporting member 60 to move back and forth through a transmission mechanism, and the transmission mechanism includes a gear fixed to the output end of the driving device 40 and a rack fixed to the supporting member 60.
  • the controller controls the driving device 40 to start, the gear rotates with the output end of the driving device 40, and the rack drives the supporting member 60 to extend out of the through hole.
  • the support member 60 is switched to the open state.
  • the controller controls the driving device 40 to rotate in reverse, and the rack drives the supporting member 60 to retract inward through the through hole, so that the supporting member 60 is switched to the closed state.
  • the drone 100 includes an image sensor
  • the support member 60 includes a frame 64, a blade 65 installed in the frame 64, and a blade motor 66 that drives the blade 65 to rotate.
  • the controller controls
  • the blade motor 66 controls the angle of rotation of the blade 65 so that the blade 65 forms an image that can be recognized by the image sensor, and the flight controller uses the image information recognized by the image sensor to control the
  • the drone 100 is landed on the supporting member 60. In this way, the drone 100 can determine the position of the support member 60 based on the image recognized by the image sensor, thereby accurately landing on the drone parking device 600.
  • the supporting member 60 includes a plurality of blades 65 of the same size. In other embodiments, the supporting member 60 includes a plurality of blades 65 of different sizes. All the blades 65 are driven by the corresponding blade motor 66 to rotate the same or different angles to form an image that can be recognized by the image sensor; or, some of the blades 65 are driven by the corresponding blade motor 66 to rotate the same or different angles , To form an image that can be recognized by the image sensor.
  • the UAV 100 also includes positioning sensors, such as GPS (Global Positioning System, Global Positioning System), IMU (Inertial Measurement Unit, Inertial Measurement Unit), and so on.
  • positioning sensors such as GPS (Global Positioning System, Global Positioning System), IMU (Inertial Measurement Unit, Inertial Measurement Unit), and so on.
  • the navigation and landing steps of the drone are as follows: 1.
  • the real-time position, speed and direction of the drone 100 are measured by the positioning sensor and fed back to the flight controller, so as to navigate the flight process of the drone 100 , Making the UAV 100 fly to the vicinity of the UAV parking device 600; 2.
  • the flight controller of the UAV 100 communicates with the controller of the UAV parking device 600. Based on the instructions of the flight controller, the controller
  • the supporting member 60 is opened by controlling the driving device 40, and the blade 65 is controlled to form an image that can be recognized by the image sensor by controlling the blade motor 66; 3.
  • the image sensor is recognized by the image sensor, and the flight controller determines that the drone is stationed.
  • the flight controller controls the drone 100 to land on the drone parking device 600.
  • the wall 900 includes an opening 910, the drone parking device 600 is disposed at the opening 910, and the size of the supporting member 60 matches the opening 910.
  • the supporting The component 60 covers the opening 910.
  • the driving device 40 and the reel 51 are installed in the opening 910.
  • the driving device 40 and the traction assembly 50 are both arranged inside the opening 910, and will not be corroded or deformed due to factors such as weather and temperature, avoiding jamming and poor safety, so that good performance can always be maintained.
  • the supporting member 60 when the supporting member 60 is in the closed state, it can be used as a guardrail, or as a blind or blind.
  • the user can control the blade motor 66 to drive the blade 65 to rotate by operating the controller to adjust the indoor light.
  • the vane motor 66 includes a stator and a rotor, the rotor is fixed to the frame 64, one end of the vane 65 is rotatably connected to the frame 64 through a rotating shaft 68, and the other end is fixed to the stator . In this way, the blade motor 66 drives the blade 65 to rotate in the frame 64.
  • the blade motor 66 includes a stator and a rotor, the stator is fixed to the frame 64, one end of the blade 65 is rotatably connected to the frame 64, and the other end is fixed to the rotor. In this way, the blade motor 66 can also be used to drive the blade 65 to rotate in the frame 64.
  • the upper surface of the blade 65 is provided with a solar panel 67; and/or, the lower surface of the blade 65 is provided with a solar panel 67. In the illustrated embodiment, both the upper surface and the lower surface of the blade 65 are provided with solar panels 67. In other embodiments, only the upper surface of the blade 65 is provided with a solar panel 67, or only the lower surface of the blade 65 is provided with a solar panel 67.
  • the unmanned parking device 600 further includes an energy storage device, and the solar panel 67 is connected to the energy storage device through a cable.
  • the solar panel 67 converts solar radiation energy into electrical energy, and then transmits the electrical energy to the energy storage device through a cable.
  • the electrical energy stored in the energy storage device can directly provide energy for the drive device 40 or the blade motor 66, and can also provide energy for other electronic devices in the user's room.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

一种无人机驻停装置（600）及无人机停机系统（1），无人机驻停装置（600）包括：驱动装置（40）；牵引组件（50），包括与驱动装置（40）输出端固定连接的卷轴（51）及绕设于卷轴（51）的绳索（52）；支撑部件（60），用于支撑无人机（100），支撑部件（60）包括连接端（61）和活动端（62），连接端（61）与墙体（900）可转动地连接，活动端（62）与绳索（52）连接；及控制器，通过控制驱动装置（40），使得活动端（62）在绳索（52）的作用下在第一位置与第二位置之间切换，当活动端（62）处于第一位置时，支撑部件（60）处于打开状态，当活动端（62）处于第二位置时，支撑部件（60）处于关闭状态。

Description

无人机驻停装置及无人机停机系统 技术领域
本申请涉及无人机技术领域，尤其涉及一种无人机驻停装置及无人机停机系统。
背景技术
近些年来，无人机已经广泛应用于民用、工业及军事领域。无人机可用于航拍、消防、测绘、检测、快递投放、外卖投放等，不限于此。当无人机用于快递、外卖投放时，为方便将货物直接投放到用户家中，通常需要在用户室外安装无人机驻停装置。然而，现有的无人机驻停装置结构复杂、成本高。
发明内容
本申请的目的在于提供一种无人机驻停装置及无人机停机系统。
本申请的一个方面提供一种无人机驻停装置。该无人机驻停装置，安装于建筑物的墙体，该无人机驻停装置包括：驱动装置；牵引组件，包括与所述驱动装置输出端固定连接的卷轴及绕设于所述卷轴的绳索；支撑部件，用于支撑无人机，所述支撑部件包括连接端和活动端，所述连接端与墙体可转动地连接，所述活动端与所述绳索连接；及控制器，通过控制所述驱动装置，使得所述活动端在所述绳索的作用下在第一位置与第二位置之间切换，当所述活动端处于第一位置时，所述支撑部件处于打开状态，当所述活动端处于第二位置时，所述支撑部件处于关闭状态。
本申请的另一个方面提供一种无人机停机系统。该无人机停机系统包括，无人机，包括飞行控制器；及无人机驻停装置，安装于建筑物的墙体，所述无人机驻停装置包括驱动装置、牵引组件、支撑部件及控制器，所述牵引组件包括与所述驱动装置输出端固定连接的卷轴及绕设于所述卷轴的绳索，所述支撑部件用于支撑无人机，所述支撑部件包括连接端和活动端，所述连接端与墙体可转动地连接，所述活动端与所述绳索连接，所述控制器与所述飞行控制器通信连接，所述控制器根据所述飞行控制器的指令来通过控制所述驱动装置，使得所述活动端在所述绳索的作用下在第一位置与第二位置之间切 换，当所述活动端处于第一位置时，所述支撑部件处于打开状态，当所述活动端处于第二位置时，所述支撑部件处于关闭状态。
本申请无人机驻停装置，通过一个驱动装置即可实现支撑部件在打开状态和关闭状态之间切换，如此，无人机驻停装置结构简单可靠、成本低。
附图说明
图1是本申请无人机驻停装置的立体示意图，其中支撑部件处于关闭状态；
图2是本申请无人机停机系统的立体示意图，其中支撑部件处于打开状态；
图3是图1所示的无人机驻停装置的纵向剖面图，其中支撑部件处于打开状态；
图4是图1所示的无人机驻停装置的主视图，其中支撑部件处于打开状态；
图5是图4所示的A处放大图；
图6是图1所示的叶片的立体示意图；
图7是图6所示的B处放大图；
图8是图1所示的无人机驻停装置的立体示意图，其中支撑部件处于打开状态，且部分叶片转动一定的角度。
具体实施方式
此处将详细地对示例性实施例进行说明，其示例表示在附图中。下面的描述涉及附图时，除非另有表示，不同附图中的相同数字表示相同或相似的要素。以下示例性实施例中所描述的实施方式并不代表与本申请相一致的所有实施方式。相反，它们仅是与如所附权利要求书中所详述的、本申请的一些方面相一致的装置和方法的例子。
在本申请使用的术语是仅仅出于描述特定实施例的目的，而非旨在限制本申请。在本申请和所附权利要求书中所使用的单数形式的“一种”、“所述”和“该”也旨在包括多数形式，除非上下文清楚地表示其他含义。还应当理解，本文中使用的术语“和/或”是指并包含一个或多个相关联的列出项目的任何或所有可能组合。
应当理解，尽管在本申请可能采用术语第一、第二、第三等来描述各种信息，但这 些信息不应限于这些术语。这些术语仅用来将同一类型的信息彼此区分开。例如，在不脱离本申请范围的情况下，第一信息也可以被称为第二信息，类似地，第二信息也可以被称为第一信息。取决于语境，如在此所使用的词语“如果”可以被解释成为“在……时”或“当……时”或“响应于确定”。
下面结合附图，对本申请的无人机驻停装置进行详细说明。在不冲突的情况下，下述的实施例及实施方式中的特征可以相互组合。
请参阅图1至图8，本发明实施例提供一种无人机停机系统1，该无人机停机系统1包括无人机100和无人机驻停装置600。无人机100用于运送货物，比如：快递、外卖等等。无人机驻停装置600用于供无人机100驻停以卸货或装货。
无人机100包括机身10、机臂20、动力装置30和飞行控制器(图未示)。机臂20与所述机身10连接。动力装置30安装在所述机臂20上，所述动力装置30包括螺旋桨31以及用于驱动所述螺旋桨31转动的电机32，所述电机32驱动所述螺旋桨31转动，以提供飞行动力。飞行控制器与无人机100的各个功能模块电性连接且协调配合各个功能模块的工作。
无人机驻停装置600安装于建筑物的墙体900，所述无人机驻停装置600包括驱动装置40、牵引组件50、支撑部件60及控制器(图未示)。
所述驱动装置40包括电机、液压系统、气压系统等。在图示实施例中，所述驱动装置40为电机。
所述牵引组件50包括与所述驱动装置40输出端固定连接的卷轴51及绕设于所述卷轴51的绳索52。所述支撑部件60用于支撑无人机100，所述支撑部件60包括连接端61和活动端62，所述连接端61与墙体可转动地连接，所述活动端62与所述绳索52连接，所述控制器与所述飞行控制器通信连接，所述控制器通过控制所述驱动装置40，使得所述活动端62在所述绳索52的作用下在第一位置与第二位置之间切换，当所述活动端62处于第一位置时，所述支撑部件60处于打开状态，当所述活动端62处于第二位置时，所述支撑部件60处于关闭状态。
当无人机100需要停落在无人机驻停装置600上时，控制器控制驱动装置40启动，卷轴51随着驱动装置40的输出端的转动，绕设于卷轴51的绳索52被逐步放出，使得支撑部件60的活动端62从第二位置切换至第一位置，此时，支撑部件60处于打开状态，无人机100可以停落在支撑部件60上。当无人机100离开无人机驻停装置600后， 控制器控制驱动装置40反向转动，使得绳索52再次绕设于卷轴51，进而使得支撑部件60的活动端62从第一位置切换至第二位置，此时，支撑部件60处于关闭状态。
在一些实施例中，控制器基于飞行控制器的指令来控制所述驱动装置40的开启、关闭以及转动的方向。在另一些实施例中，用户通过直接操作控制器，来控制驱动装置40的开启、关闭以及转动的方向。
通过一个驱动装置40即可实现支撑部件60在打开状态和关闭状态之间切换，如此，无人机驻停装置600结构简单可靠、成本低。
在图示实施例中，所述支撑部件60通过转动实现在打开状态和关闭状态之间切换。在另一些实施例中，墙体设有与支撑部件60匹配的通孔，所述支撑部件60通过所述通孔来回移动实现在打开状态和关闭状态之间切换。具体地，驱动装置40通过传动机构驱动支撑部件60来回移动，所述传动机构包括固定于所述驱动装置40输出端的齿轮和固定于所述支撑部件60的齿条。当无人机100需要停落在无人机驻停装置600上时，控制器控制驱动装置40启动，齿轮随着驱动装置40输出端的转动，齿条带动支撑部件60向外伸出通孔，使得支撑部件60切换到打开状态。当无人机100离开无人机驻停装置600后，控制器控制驱动装置40反向转动，齿条带动支撑部件60向内缩回通孔，使得支撑部件60切换到关闭状态。
进一步地，所述无人机100包括图像传感器，所述支撑部件60包括框架64、安装于所述框架64内的叶片65和驱动所述叶片65转动的叶片电机66，所述控制器通过控制所述叶片电机66，以控制所述叶片65转动的角度，使得所述叶片65形成能够被所述图像传感器识别的图像，所述飞行控制器通过所述图像传感器所识别的图像信息控制所述无人机100降落在所述支撑部件60上。如此，无人机100能够通过图像传感器识别的图像判断支撑部件60的位置，从而准确地降落在无人机驻停装置600上。
在图示实施例中，所述支撑部件60包括多个相同尺寸的叶片65。在另一些实施例中，所述支撑部件60包括多个不同尺寸的叶片65。所有的叶片65在对应叶片电机66的驱动下转动相同或不同的角度，以形成能够被所述图像传感器识别的图像；或者，部分叶片65在对应叶片电机66的驱动下转动相同或不同的角度，以形成能够被所述图像传感器识别的图像。
无人机100还包括定位传感器，例如GPS(Global Positioning System，全球定位系统)、IMU(Inertial measurement unit，惯性测量单元)，等等。
无人机的导航降落步骤如下：1、通过所述定位传感器测量所述无人机100的实时位置、速度和方向并反馈至所述飞行控制器，从而对无人机100的飞行过程进行导航，使得无人机100飞行至无人机驻停装置600附近；2、无人机100的飞行控制器与无人机驻停装置600的控制器进行通信，基于飞行控制器的指令，控制器通过控制驱动装置40使得支撑部件60处于打开状态，并且通过控制叶片电机66使得叶片65形成能够被所述图像传感器识别的图像；3、通过图像传感器识别上述图像，飞行控制器确定无人机驻停装置600相对于无人机100的位置坐标；4、飞行控制器控制无人机100降落在无人机驻停装置600上。
所述墙体900包括开口910，所述无人机驻停装置600设置于所述开口910处，支撑部件60的尺寸与开口910匹配，当所述支撑部件60处于关闭状态时，所述支撑部件60将所述开口910覆盖。所述驱动装置40和所述卷轴51安装于所述开口910内。如此，驱动装置40和牵引组件50均设置于开口910内侧，不会受到天气、气温等因素影响而发生腐蚀、变形，避免了卡死、安全性差等情况，从而能够始终保持良好的性能。同时，支撑部件60处于关闭状态时能够作为护栏，也可以作为百叶窗或百叶帘，用户可以通过操作控制器来控制叶片电机66带动叶片65转动，从而调节室内光线。
在一个实施例中，所述叶片电机66包括定子和转子，所述转子与所述框架64固定，所述叶片65一端通过转轴68与所述框架64可转动连接，另一端与所述定子固定。如此，实现通过叶片电机66带动叶片65在框架64内转动。
在另一个实施例中，所述叶片电机66包括定子和转子，所述定子与所述框架64固定，所述叶片65一端与所述框架64可转动连接，另一端与所述转子固定。如此，同样可以实现通过叶片电机66带动叶片65在框架64内转动。
所述叶片65的上表面设有太阳能板67；和/或，所述叶片65的下表面设有太阳能板67。在图示实施例中，所述叶片65的上表面和下表面均设有太阳能板67。在其他实施例中，只有叶片65的上表面设有太阳能板67，或者，只有叶片65的下表面设有太阳能板67。
在图示实施例中，所述无人驻停装置600还包括储能装置，所述太阳能板67通过电缆连接至所述储能装置。所述太阳能板67将太阳辐射能转换成电能，然后通过电缆将电能传送至储能装置中。储存在储能装置中的电能能够直接为驱动装置40或叶片电机66提供能量，也可以为用户室内的其他电子设备提供能量。
以上所述仅为本申请的较佳实施例而已，并不用以限制本申请，凡在本申请的精神和原则之内，所做的任何修改、等同替换、改进等，均应包含在本申请保护的范围之内。

Claims (14)

  1. 一种无人机驻停装置，安装于建筑物的墙体，包括：
    驱动装置；
    牵引组件，包括与所述驱动装置输出端固定连接的卷轴及绕设于所述卷轴的绳索；
    支撑部件，用于支撑无人机，所述支撑部件包括连接端和活动端，所述连接端与所述墙体可转动地连接，所述活动端与所述绳索连接；及
    控制器，通过控制所述驱动装置，使得所述活动端在所述绳索的作用下在第一位置与第二位置之间切换，当所述活动端处于所述第一位置时，所述支撑部件处于打开状态，当所述活动端处于所述第二位置时，所述支撑部件处于关闭状态。
  2. 根据权利要求1所述的无人机驻停装置，其特征在于，所述支撑部件包括框架、安装于所述框架内的多个叶片和驱动所述多个叶片转动的叶片电机，所述控制器通过控制所述叶片电机，以控制所述多个叶片转动的角度。
  3. 根据权利要求2所述的无人机驻停装置，其特征在于，所述叶片电机包括定子和转子，所述转子与所述框架固定，所述多个叶片一端与所述框架可转动连接，另一端与所述定子固定；或者，
    所述叶片电机包括定子和转子，所述定子与所述框架固定，所述多个叶片一端与所述框架可转动连接，另一端与所述转子固定。
  4. 根据权利要求2所述的无人机驻停装置，其特征在于，所述叶片的上表面设有太阳能板；和/或，所述叶片的下表面设有太阳能板。
  5. 根据权利要求4所述的无人机驻停装置，其特征在于，还包括储能装置，所述太阳能板通过电缆连接至所述储能装置。
  6. 根据权利要求2所述的无人机驻停装置，其特征在于，所述多个叶片具有相同或不同的尺寸。
  7. 根据权利要求1至6任一项所述的无人机驻停装置，其特征在于，所述墙体包括开口，所述无人机驻停装置设置于所述开口处，所述支撑部件的尺寸与所述开口匹配，当所述支撑部件处于关闭状态时，所述支撑部件将所述开口覆盖。
  8. 根据权利要求7所述的无人机驻停装置，其特征在于，所述驱动装置和所述卷轴安装于所述开口内。
  9. 一种无人机停机系统，包括，
    无人机，包括飞行控制器；及
    无人机驻停装置，安装于建筑物的墙体，包括：
    驱动装置；
    牵引组件，包括与所述驱动装置输出端固定连接的卷轴及绕设于所述卷轴的绳索；
    支撑部件，用于支撑所述无人机，所述支撑部件包括连接端和活动端，所述连接端与所述墙体可转动地连接，所述活动端与所述绳索连接；及
    控制器，与所述飞行控制器通信连接，所述控制器根据所述飞行控制器的指令来通过控制所述驱动装置，使得所述活动端在所述绳索的作用下在第一位置与第二位置之间切换，当所述活动端处于所述第一位置时，所述支撑部件处于打开状态，当所述活动端处于所述第二位置时，所述支撑部件处于关闭状态。
  10. 根据权利要求9所述的无人机停机系统，其特征在于，所述无人机包括定位传感器和图像传感器，所述支撑部件包括框架、安装于所述框架内的多个叶片和驱动所述多个叶片转动的叶片电机，所述控制器通过控制所述叶片电机，以控制所述多个叶片转动的角度，使得所述多个叶片形成能够被所述图像传感器识别的图像，所述飞行控制器通过所述图像传感器所识别的图像信息控制所述无人机降落在所述支撑部件上。
  11. 根据权利要求10所述的无人机停机系统，其特征在于，所述叶片电机包括定子和转子，所述转子与所述框架固定，所述多个叶片一端与所述框架可转动连接，另一端与所述定子固定；或者，
    所述叶片电机包括定子和转子，所述定子与所述框架固定，所述多个叶片一端与所述框架可转动连接，另一端与所述转子固定。
  12. 根据权利要求10或11所述的无人机停机系统，其特征在于，所述多个叶片具有相同或不同的尺寸。
  13. 根据权利要求10-12中任一项所述的无人机停机系统，其特征在于，所述墙体包括开口，所述无人机驻停装置设置于所述开口处，所述支撑部件的尺寸与所述开口匹配，当所述支撑部件处于关闭状态，所述支撑部件将所述开口覆盖。
  14. 根据权利要求13所述的无人机停机系统，其特征在于，所述驱动装置和所述卷轴安装于所述开口内。
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