WO2019127105A1 - 用于拆装无人飞行器电源的设备 - Google Patents

用于拆装无人飞行器电源的设备 Download PDF

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Publication number
WO2019127105A1
WO2019127105A1 PCT/CN2017/119018 CN2017119018W WO2019127105A1 WO 2019127105 A1 WO2019127105 A1 WO 2019127105A1 CN 2017119018 W CN2017119018 W CN 2017119018W WO 2019127105 A1 WO2019127105 A1 WO 2019127105A1
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WIPO (PCT)
Prior art keywords
unmanned aerial
aerial vehicle
power
power source
disassembling
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PCT/CN2017/119018
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English (en)
French (fr)
Inventor
张顺
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深圳市大疆创新科技有限公司
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Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to CN201780020288.0A priority Critical patent/CN108883508A/zh
Priority to PCT/CN2017/119018 priority patent/WO2019127105A1/zh
Publication of WO2019127105A1 publication Critical patent/WO2019127105A1/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
    • B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
    • B64F1/0299—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables characterized by the use of multiple devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • 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
    • 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
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • 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
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components

Definitions

  • the technical solution disclosed in the present application relates to the field of unmanned aerial vehicles, and particularly relates to an apparatus for disassembling an unmanned aerial vehicle power supply.
  • the unmanned aerial vehicle needs to be replaced during the long flight test.
  • the technical solution disclosed in the present application can solve at least the following technical problems: in the prior art, it is difficult to adjust the position of the unmanned aerial vehicle when disassembling the power supply of the unmanned aerial vehicle, and the disassembly and assembly efficiency is low.
  • One or more embodiments of the present application disclose apparatus for disassembling an unmanned aerial vehicle power source, including:
  • Position adjustment unit for adjusting the position of the unmanned aerial vehicle on the parking platform after the UAV is lowered
  • a power storage unit for storing one or more power sources of the unmanned aerial vehicle
  • the power disassembly department is used to remove the power of the unmanned aerial vehicle and install the power supply of the unmanned aerial vehicle on the power storage unit on the unmanned aerial vehicle.
  • the device for disassembling the unmanned aerial vehicle power source disclosed in the present application comprises: an parking platform, a position adjusting portion, a power storage portion, and a power dismounting portion. After the UAV landed on the parking platform, the position adjusting portion adjusts the unmanned person.
  • the position of the aircraft on the parking platform allows the UAV to be parked at a designated location on the parking platform, facilitating the power disassembly to remove the power of the UAV and installing the UAV power supply on the UAV in the UAV This will help improve disassembly efficiency.
  • the power storage unit stores one or more power sources of the unmanned aerial vehicle to meet the long-term flight test of the unmanned aerial vehicle.
  • FIG. 1 is a configuration diagram of an apparatus for disassembling a power supply of an unmanned aerial vehicle according to an embodiment of the present application
  • FIG. 2 is a configuration diagram of a position adjustment unit in an embodiment of the present application.
  • Fig. 3 is a structural diagram of a power storage unit in an embodiment of the present application.
  • Position adjustment unit 1 Position adjustment unit 2 Power storage 3 Power Disassembly Department 4 window 11 First position adjustment mechanism twenty one Second position adjustment mechanism twenty two Drive mechanism twenty three Baffle 221 Transmission structure 222 Motor 223,232 Putt 224,225 Rail structure 231 Transmission structure 233 Long opening 2211, 2212 guide 2311, 2312 skateboard 2313, 2314
  • First drive module 31 Storage board 32 Charging stand 33 Second drive module 41 Third drive module 42 Action mechanism 43
  • FIG. 1 a configuration diagram of an apparatus for disassembling an unmanned aerial vehicle power supply according to an embodiment of the present application.
  • the equipment for disassembling the UAV power supply includes:
  • the parking platform 1 is used to park the unmanned aerial vehicle after landing;
  • the position adjusting unit 2 is configured to adjust the position of the unmanned aerial vehicle on the parking platform 1 after the UAV is lowered;
  • a power storage unit 3 for storing one or more power sources of the unmanned aerial vehicle
  • the power dismounting unit 4 is configured to remove the power of the unmanned aerial vehicle and install the power supply of the unmanned aerial vehicle on the power storage unit 3 on the unmanned aerial vehicle.
  • the position adjusting unit 2 adjusts the position of the UAV on the parking platform 1, so that the UAV is parked at a designated position on the parking platform 1, so that the power dismantling unit 4 can be removed.
  • the power supply of the aircraft and the power supply of the unmanned aerial vehicle on the power storage unit 3 are installed on the unmanned aerial vehicle, which is advantageous for improving the disassembly efficiency.
  • the power storage unit 3 stores one or more power sources of the unmanned aerial vehicle, and can satisfy the long-term flight test of the unmanned aerial vehicle.
  • the position adjusting portion 2 includes: a first position adjusting mechanism 21, a second position adjusting mechanism 22, and a driving mechanism 23; the driving mechanism 23 drives the first position adjusting mechanism 21 and the second position adjusting mechanism 22 to face each other. Movement to push the UAV to the designated area of the parking platform 1; the first position adjustment mechanism 21 and the second position adjustment mechanism 22 are respectively clamped to the UAV to clamp the UAV to the designated position of the parking platform 1. .
  • the direction in which the first position adjusting mechanism 21 and the second position adjusting mechanism 22 move toward each other is perpendicular to the direction in which the first position adjusting mechanism 21 and the second position adjusting mechanism 22 are clamped to the unmanned aerial vehicle, and thus When the first position adjusting mechanism 21 and the second position adjusting mechanism 22 are clamped to the unmanned aerial vehicle, the position of the unmanned aerial vehicle in the moving direction of the first position adjusting mechanism 21 and the second position adjusting mechanism 22 is not easily affected, which is advantageous for improving the position. The accuracy of the adjustment.
  • the driving mechanism 23 includes a rail structure 231 for sliding the first position adjusting mechanism 21 and the second position adjusting mechanism 22, a motor 232, and a transmission structure 233 driven by the motor 232; the transmission structure 233 is in the motor
  • the driving of 232 drives the first position adjusting mechanism 21 and the second position adjusting mechanism 22 to move toward each other.
  • the motor 232 is disposed at one end of the rail structure 231, the other end of the rail structure 231 is provided with one pulley of the transmission structure 233, and the other pulley of the transmission structure 233 is disposed at the motor 232.
  • the driving belt of the transmission structure 233 pulls the first position adjusting mechanism 21 and the second position adjusting mechanism 22 to move toward each other on the rail structure 231.
  • the two rails (2311, 2312) of the rail structure 231 are arranged in parallel.
  • One slide 2313 of the rail structure 231 is transferred to the first position adjusting mechanism 21, and the other slide 2314 of the rail structure 231 is turned.
  • the drive belt of the transmission structure 233 is coupled to the two slide plates (2313, 2314) of the rail structure 231.
  • the first position adjustment mechanism 21 or the second position adjustment mechanism 22 includes, or the first position adjustment mechanism 21 and the second position adjustment mechanism 22 respectively include: a baffle for pushing the unmanned aerial vehicle 221, a transmission structure 222 mounted on the baffle 221, a motor 223 driving the transmission structure 222, and two push rods (224, 225) mounted on the transmission structure 222; the motor 223 drives the transmission structure 222 to drive the two push rods (224, 225) move in opposite directions to clamp the unmanned aerial vehicle, and the shutter 221 is transferred to the slider 2314 of the rail structure 231.
  • the baffle 221 is formed with two elongated openings (2211, 2212) for defining the range of motion of the two push rods (224, 225) so that the push rod 224 does not go over Within the range of motion of the push rod 225, the push rod 225 does not fall out of the range of motion of the push rod 224.
  • the power storage unit 3 includes a first drive module 31 and a storage plate 32 driven by the first drive module 31.
  • the storage plate 32 is used to store one or more power sources of the UAV.
  • the storage plate 32 is provided with one or more charging seats 33 for charging the power of the unmanned aerial vehicle.
  • the power dismounting unit 4 mounts the power source detached from the unmanned aerial vehicle in the charging stand 33, and installs the power source that has been charged on the unmanned aerial vehicle, so that the air power is used in the flight test of the unmanned aerial vehicle.
  • Equipment that disassembles the UAV's power supply can charge the UAV's power supply with greater automation.
  • the power dismounting unit 4 includes a second driving module 41 , a third driving module 42 vertically disposed on the second driving module 41 and driven by the second driving module 41 , and The action mechanism 43 driven by the third drive module 42; the second drive module 41 drives the third drive module 42 and the action mechanism 43 to approach the unmanned aerial vehicle on the parking platform 1 so that the action mechanism 43 will move the unmanned aerial vehicle
  • the power supply is removed and the power is installed for the unmanned aerial vehicle;
  • the second driving module 41 drives the third driving module 42 and the action mechanism 43 away from the unmanned aerial vehicle on the parking platform 1, and the third driving module 42 drives the operating mechanism 43.
  • the power storage unit 3 is placed close to the power storage unit 3 so that the power unit of the unmanned aerial vehicle is placed in the power storage unit 3.
  • the action mechanism 43 includes at least one grip for holding the power source of the unmanned aerial vehicle.
  • the clamping member is a jaw cylinder.
  • the action mechanism 43 further includes at least one fixing device for fixing the position of the unmanned aerial vehicle, so that during the process of disassembling the power supply of the unmanned aerial vehicle, and During the installation of the power source of the human aircraft, the position of the unmanned aerial vehicle can be fixed.
  • the fixing device may be a jaw cylinder, or may be a fixture composed of a cylinder, a pressing rod or the like.
  • the second driving module 41 and the third driving module 42 are perpendicular to the first driving module 31 of the power storage unit 3, respectively, to facilitate the first driving module 31,
  • the second driving module 41 and the third driving module 42 cooperate with each other, so that the action mechanism 43 can accurately place the battery of the UAV in the power storage unit 3 and accurately pick up from the power storage unit 3.
  • the battery of the unmanned aerial vehicle is perpendicular to the first driving module 31 of the power storage unit 3, respectively, to facilitate the first driving module 31,
  • the second driving module 41 and the third driving module 42 cooperate with each other, so that the action mechanism 43 can accurately place the battery of the UAV in the power storage unit 3 and accurately pick up from the power storage unit 3.
  • the battery of the unmanned aerial vehicle are perpendicular to the first driving module 31 of the power storage unit 3, respectively, to facilitate the first driving module 31,
  • the second driving module 41 and the third driving module 42 cooperate with each other, so that the action mechanism 43 can accurately place the battery of the UAV in the power storage unit 3 and accurately pick up from the power storage
  • the parking platform 1 is provided with a window 11 through which the action mechanism 43 passes, facilitating the action mechanism 43 to approach the unmanned aerial vehicle on the parking platform 1.

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

Abstract

一种用于拆装无人飞行器电源的设备，包括：停机平台（1），用于停放降落后的无人飞行器；位置调整部（2），用于无人飞行器降落后调整无人飞行器在所述停机平台上的位置；电源贮存部（3），用于贮存无人飞行器的一个或者多个电源；电源拆装部（4），用于拆除无人飞行器的电源并将所述电源贮存部上的无人飞行器的电源装设在无人飞行器上。该设备能够提高拆装无人飞行器电源的效率，满足无人飞行器长时间的飞行测试。

Description

用于拆装无人飞行器电源的设备 【技术领域】
本申请公开的技术方案涉及无人飞行器技术领域，尤其涉及用于拆装无人飞行器电源的设备。
【背景技术】
无人飞行器长时间的飞行测试过程中需要更换电源。
发明人在研究本申请的过程中，发现现有技术中拆装无人飞行器的电源时难以对无人飞行器的位置进行调整，拆装效率低。
【发明内容】
本申请公开的技术方案至少能够解决以下技术问题：现有技术中拆装无人飞行器的电源时难以对无人飞行器的位置进行调整，拆装效率低。
本申请的一个或者多个实施例公开了用于拆装无人飞行器电源的设备，包括：
停机平台，用于停放降落后的无人飞行器；
位置调整部，用于无人飞行器降落后调整无人飞行器在停机平台上的位置；
电源贮存部，用于贮存无人飞行器的一个或者多个电源；
电源拆装部，用于拆除无人飞行器的电源并将电源贮存部上的无人飞行器的电源装设在无人飞行器上。
与现有技术相比，本申请公开的技术方案主要有以下有益效果：
在本申请公开的用于拆装无人飞行器电源的设备，包括：停机平台、位置调整部、电源贮存部以及电源拆装部，无人飞行器降落在停机平台上后，位置调整部调整无人飞行器在停机平台上的位置，使得无人飞行器停放在停机平台上指定的位置，便于电源拆装部拆除无人飞行器的电源并将电源贮存部上的无人飞行器的电源装设在无人飞行器上，有利于提高拆装效率。电源贮存部贮存 无人飞行器的一个或者多个电源，能够满足无人飞行器长时间的飞行测试。
【附图说明】
为了更清楚地说明本申请实施例的技术方案，下面将对实施例中所需要使用的附图作简单地介绍，显而易见地，下面描述中的附图仅仅是本申请的一些实施例，对于本领域普通技术人员来讲，在不付出创造性劳动性的前提下，还可以根据这些附图获得其它的附图。
图1为本申请的一实施例中一种用于拆装无人飞行器电源的设备的构造图；
图2为本申请的一实施例中位置调整部的构造图；
图3为本申请的一实施例中电源贮存部的构造图。
主要附图标记说明
停机平台 1
位置调整部 2
电源贮存部 3
电源拆装部 4
窗口 11
第一位置调整机构 21
第二位置调整机构 22
驱动机构 23
挡板 221
传动结构 222
电机 223、232
推杆 224、225
导轨结构 231
传动结构 233
长条形开口 2211、2212
导轨 2311、2312
滑板 2313、2314
第一驱动模组 31
贮存板 32
充电座 33
第二驱动模组 41
第三驱动模组 42
动作机构 43
【具体实施方式】
为了便于理解本申请，下面将参照相关附图对本申请进行更全面的描述。附图中给出了本申请的较佳实施例。但是，本申请可以以许多不同的形式来实现，并不限于本文所描述的实施例。相反地，提供这些实施例的目的是使对本申请的公开内容的理解更加透彻全面。
除非另有定义，本文所使用的所有的技术和科学术语与本申请的技术领域的技术人员通常理解的含义相同。本文中在本申请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，不是旨在于限制本申请。本申请的权利要求书、说明书以及说明书附图中的术语“第一”、“第二”、“第三”等是用于区别不同对象，而不是用于描述特定顺序。
参考图1，为本申请的一实施例中一种用于拆装无人飞行器电源的设备的构造图。如图1中所示意的，用于拆装无人飞行器电源的设备包括：
停机平台1，用于停放降落后的无人飞行器；
位置调整部2，用于无人飞行器降落后调整无人飞行器在停机平台1上的位置；
电源贮存部3，用于贮存无人飞行器的一个或者多个电源；
电源拆装部4，用于拆除无人飞行器的电源并将电源贮存部3上的无人飞行器的电源装设在无人飞行器上。
无人飞行器降落在停机平台1上后，位置调整部2调整无人飞行器在停机平台1上的位置，使得无人飞行器停放在停机平台1上指定的位置，便于电源拆装部4拆除无人飞行器的电源并将电源贮存部3上的无人飞行器的电源装设 在无人飞行器上，有利于提高拆装效率。电源贮存部3贮存无人飞行器的一个或者多个电源，能够满足无人飞行器长时间的飞行测试。
参考图2，为本申请的一实施例中位置调整部2的构造图。如图2中所示意的，位置调整部2包括：第一位置调整机构21、第二位置调整机构22以及驱动机构23；驱动机构23驱动第一位置调整机构21和第二位置调整机构22相向运动，以便将无人飞行器推送至停机平台1指定的区域；第一位置调整机构21和第二位置调整机构22分别夹向无人飞行器，以便将无人飞行器夹定在停机平台1指定的位置。
在一种可能的实施方式中，第一位置调整机构21和第二位置调整机构22相向运动的方向与第一位置调整机构21和第二位置调整机构22夹向无人飞行器的方向垂直，因此在第一位置调整机构21和第二位置调整机构22夹向无人飞行器时不易影响无人飞行器在第一位置调整机构21和第二位置调整机构22相向运动方向上的位置，有利于提高位置调整的精准度。
在一种可能的实施方式中，驱动机构23包括供第一位置调整机构21和第二位置调整机构22滑动的导轨结构231、电机232以及由电机232驱动的传动结构233；传动结构233在电机232的驱动下带动第一位置调整机构21和第二位置调整机构22相向运动。
在一种可能的实施方式中，电机232设置在导轨结构231的一端，导轨结构231的另一端装设有传动结构233的一个带轮，传动结构233的另一个带轮装设在电机232的转轴上；传动结构233的传动带拉动第一位置调整机构21和第二位置调整机构22在所述导轨结构231上相向运动。
在一种可能的实施方式中，导轨结构231的两根导轨(2311、2312)平行设置，导轨结构231的一块滑板2313转接至第一位置调整机构21，导轨结构231的另一块滑板2314转接至第二位置调整机构22，传动结构233的传动带与所述导轨结构231的两块滑板(2313、2314)连接。
在一种可能的实施方式中，第一位置调整机构21或者第二位置调整机构22包括，或者第一位置调整机构21和第二位置调整机构22分别包括：用于推动无人飞行器的挡板221、安装在挡板221上的传动结构222、驱动传动结构222的电机223以及装设在传动结构222上的两根推杆(224、225)；电机223驱动 传动结构222带动两根推杆(224、225)相向运动以夹持无人飞行器，挡板221转接在导轨结构231的滑板2314上。
在一种可能的实施方式中，挡板221上形成有用于限定两根推杆(224、225)的运动范围的两个长条形开口(2211、2212)，使得推杆224不会越位到推杆225的运动范围内，推杆225不会越位到推杆224的运动范围内。
参考图3，为本申请的一实施例中电源贮存部3的构造图。如图3中所示意的，电源贮存部3包括第一驱动模组31和由第一驱动模组31驱动的贮存板32，贮存板32用于贮存无人飞行器的一个或者多个电源。
在一种可能的实施方式中，贮存板32上设置有一个或者多个用于给无人飞行器的电源充电的充电座33。电源拆装部4将从无人飞行器上拆卸下来的电源安放在充电座33内，将已经充电完成的电源装设在无人飞行器上，因此在无人飞行器的飞行测试过程中所述用于拆装无人飞行器电源的设备能够为无人飞行器的电源充电，自动化程度更高。
如图1中所示意的，电源拆装部4包括第二驱动模组41、垂直设置在第二驱动模组41上并由所述第二驱动模组41驱动的第三驱动模组42以及由所述第三驱动模组42驱动的动作机构43；第二驱动模组41驱动第三驱动模组42和动作机构43靠近停机平台1上的无人飞行器，以便动作机构43将无人飞行器的电源拆除以及为所述无人飞行器安装电源；第二驱动模组41驱动第三驱动模组42和动作机构43远离停机平台1上的无人飞行器，第三驱动模组42驱动动作机构43靠近电源贮存部3，以便动作机构43将无人飞行器的电源放置在所述电源贮存部3。
在一种可能的实施方式中，动作机构43至少包括一个用于夹持无人飞行器的电源的夹持件。具体的，所述夹持件为夹爪气缸。
在一种可能的实施方式中，动作机构43还包括至少一个用于固定无人飞行器的位置的固定装置，使得在所述动作机构43将无人飞行器的电源拆除的过程中以及为所述无人飞行器安装电源的过程中，所述无人飞行器的位置能够固定。具体的，所述固定装置可以是夹爪气缸，也可以是由气缸、压杆等组成的治具。
在一种可能的实施方式中，第二驱动模组41和第三驱动模组42分别垂直于电源贮存部3的第一驱动模组31，有利于所述第一驱动模组31、所述第二驱 动模组41以及所述第三驱动模组42相互配合，以便动作机构43能够精准地将无人飞行器的电池放置在电源贮存部3，以及精准地从所述电源贮存部3上拾取无人飞行器的电池。
在一种可能的实施方式中，停机平台1设置有供动作机构43通过的窗口11，有利于所述动作机构43靠近所述停机平台1上的无人飞行器。
最后应说明的是：以上实施例仅用以说明本申请的技术方案，而非对其限制。尽管参照前述实施例对本申请进行了详细的说明，本领域的普通技术人员应当理解，其依然可以对前述各实施例所记载的技术方案进行修改，或者对其中部分技术特征进行等同替换。而这些修改或者替换，并不使相应技术方案的本质脱离本申请各实施例技术方案的精神和范围。

Claims (15)

  1. 用于拆装无人飞行器电源的设备，其特征在于，包括：
    停机平台，用于停放降落后的无人飞行器；
    位置调整部，用于无人飞行器降落后调整无人飞行器在所述停机平台上的位置；
    电源贮存部，用于贮存无人飞行器的一个或者多个电源；
    电源拆装部，用于拆除无人飞行器的电源并将所述电源贮存部上的无人飞行器的电源装设在无人飞行器上。
  2. 根据权利要求1所述的用于拆装无人飞行器电源的设备，其特征在于，所述位置调整部包括：第一位置调整机构、第二位置调整机构以及驱动机构；所述驱动机构驱动所述第一位置调整机构和第二位置调整机构相向运动，以便将无人飞行器推送至所述停机平台指定的区域；所述第一位置调整机构和所述第二位置调整机构分别夹向所述无人飞行器，以便将所述无人飞行器夹定在所述停机平台指定的位置。
  3. 根据权利要求2所述的用于拆装无人飞行器电源的设备，其特征在于，所述驱动机构包括供所述第一位置调整机构和第二位置调整机构滑动的导轨结构、电机以及由所述电机驱动的传动结构；所述传动结构在所述电机的驱动下带动所述第一位置调整机构和第二位置调整机构相向运动。
  4. 根据权利要求3所述的用于拆装无人飞行器电源的设备，其特征在于，所述电机设置在所述导轨结构的一端，所述导轨结构的另一端装设有所述传动结构的一个带轮，所述传动结构的另一个带轮装设在所述电机的转轴上；所述传动结构的传动带拉动所述第一位置调整机构和所述第二位置调整机构在所述导轨结构上相向运动。
  5. 根据权利要求3所述的用于拆装无人飞行器电源的设备，其特征在于，所述导轨结构的两根导轨平行设置，所述导轨结构的一块滑板转接至所述第一位置调整机构，所述导轨结构的另一块滑板转接至所述第二位置调整机构，所述传动结构的传动带与所述导轨结构的两块滑板连接。
  6. 根据权利要求2所述的用于拆装无人飞行器电源的设备，其特征在于，所述第一位置调整机构或者所述第二位置调整机构包括，或者所述第一位置调整机构和所述第二位置调整机构分别包括：用于推动无人飞行器的挡板、安装在所述挡板上的传动结构、驱动所述传动结构的电机以及装设在所述传动结构上的两根推杆；所述电机驱动所述传动结构带动所述两根推杆相向运动以夹持无人飞行器，所述挡板转接在导轨结构的滑板上。
  7. 根据权利要求6所述的用于拆装无人飞行器电源的设备，其特征在于，所述挡板上形成有用于限定所述两根推杆的运动范围的两个长条形开口。
  8. 根据权利要求1所述的用于拆装无人飞行器电源的设备，其特征在于，所述电源贮存部包括第一驱动模组和由所述第一驱动模组驱动的贮存板，所述贮存板用于贮存无人飞行器的一个或者多个电源。
  9. 根据权利要求8所述的用于拆装无人飞行器电源的设备，其特征在于，所述贮存板上设置有一个或者多个用于给无人飞行器的电源充电的充电座。
  10. 根据权利要求1所述的用于拆装无人飞行器电源的设备，其特征在于，所述电源拆装部包括第二驱动模组、垂直设置在所述第二驱动模组上并由所述第二驱动模组驱动的第三驱动模组以及由所述第三驱动模组驱动的动作机构；所述第二驱动模组驱动所述第三驱动模组和所述动作机构靠近所述停机平台上的无人飞行器，以便所述动作机构将所述无人飞行器的电源拆除以及为所述无人飞行器安装电源；所述第二驱动模组驱动所述第三驱动模组和所述动作机构远离所述停机平台上的无人飞行器，所述第三驱动模组驱动所述动作机构靠近所述电源贮存部，以便所述动作机构将无人飞行器的电源放置在所述电源贮存部。
  11. 根据权利要求10所述的用于拆装无人飞行器电源的设备，其特征在于，所述动作机构至少包括一个用于夹持无人飞行器的电源的夹持件。
  12. 根据权利要求11所述的用于拆装无人飞行器电源的设备，其特征在于，所述夹持件为夹爪气缸。
  13. 根据权利要求11所述的用于拆装无人飞行器电源的设备，其特征在于，所述动作机构还包括至少一个用于固定无人飞行器的位置的固定装置，使得所述动作机构将所述无人飞行器的电源拆除以及为所述无人飞行器安装电源的过 程中所述无人飞行器的位置固定。
  14. 根据权利要求10所述的用于拆装无人飞行器电源的设备，其特征在于，所述第二驱动模组和所述第三驱动模组分别垂直于所述电源贮存部的第一驱动模组。
  15. 根据权利要求10所述的用于拆装无人飞行器电源的设备，其特征在于，所述停机平台设置有供所述动作机构通过的窗口。
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