WO2018223597A1 - 一种用于无人机设置的集成*** - Google Patents

一种用于无人机设置的集成*** Download PDF

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Publication number
WO2018223597A1
WO2018223597A1 PCT/CN2017/109969 CN2017109969W WO2018223597A1 WO 2018223597 A1 WO2018223597 A1 WO 2018223597A1 CN 2017109969 W CN2017109969 W CN 2017109969W WO 2018223597 A1 WO2018223597 A1 WO 2018223597A1
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Prior art keywords
drone
fixing
column
integrated system
power
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PCT/CN2017/109969
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English (en)
French (fr)
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***
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埃缇国际控股中国香港有限公司
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Publication of WO2018223597A1 publication Critical patent/WO2018223597A1/zh

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    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
    • E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
    • 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
    • B64F1/36—Other airport installations
    • 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

Definitions

  • the invention belongs to the technical field of drones, and particularly relates to an intelligent control and setting platform of a drone.
  • the drone referred to as the "unmanned aerial vehicle" is a non-manned aircraft operated by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control devices are installed. Personnel on the ground, on the ship or at the remote control station of the parent machine can track, locate, remotely control, telemetry and digitally transmit through radar and other equipment. It can take off like a normal airplane under the radio remote control or launch it with a booster rocket. It can also be brought into the air by the parent aircraft. When recycling, it can be landed automatically in the same way as a normal aircraft landing process, or it can be recovered by remote control with a parachute or block. Can be used multiple times. Widely used in aerial reconnaissance, surveillance, communication, anti-submarine, electronic interference and so on.
  • patent application No. 201620542343.5 discloses a modular combined multi-rotor drone comprising a plurality of power modules and control modules.
  • Each power module includes a housing and a drone unit disposed in the housing, the housing is a regular hexagonal prism frame structure; a connecting member is disposed on an outer side surface of the side wall of the housing, the connecting member includes an active member and a fitting; the drone unit includes Motor and propeller, motor and housing fixed connection, screw The propeller is fixed on the output shaft of the motor, and the control module is electrically connected with the motors of the plurality of power modules.
  • the combination of multiple power modules greatly improves the load capacity of the drone, and achieves the functions of multiple drones through one design, saving development and manufacturing costs. It is easy to disassemble and assemble, and easy to operate.
  • the outer casing of each power module is a regular hexagonal prism frame structure, and the neat honeycomb structure makes the combination of multiple power modules diversified.
  • the above patent application merely sets the drone in the regular hexagonal prism frame structure, thereby constituting a combination of a plurality of drones, improving the design and manufacturing cost, and improving the data transmission of the transportation and the drone. It still has the above problems that are difficult to transport, manage and maintain.
  • the space is convenient for the transportation of the drone, enabling the drone to be monitored for long distances, and it is convenient for the drone to realize long-distance shooting and surveying applications.
  • Another object of the present invention is to provide an integrated system for drone setting, which is simple in structure, easy to implement, and capable of quickly and efficiently implementing software update, upgrade or maintenance of a drone, which can be conveniently and without The man-machine is charged and maintained.
  • An integrated system for drone setting characterized in that the system comprises a column and a receiving compartment, wherein the receiving compartment is used for positioning and fixing the drone, the column is arranged in the receiving compartment, and the column is mainly used In the supporting and fixing storage compartment, the receiving compartment has a fixing device of the drone to fix the drone.
  • the storage compartment comprises a plurality of storage compartments forming a receiving area, so that the integrated system can install a plurality of drones; the plurality of storage compartments are arranged around the column to fully utilize the space and the column to reduce take up space.
  • the receiving compartment has a top plate and a base, and the base is fixed at a lower portion of the column, A fixing device is disposed on the base, and the top portion is disposed at an upper end of the column for receiving and protecting the drone.
  • the fixing device comprises a fixing component
  • the fixing component is composed of a fixing frame and a strap
  • one side of the fixing frame is provided with a strap hole for passing through the strap to The drone is fixed by the strap.
  • the fixing device further includes a fixing component 2, the fixing component 2 is composed of a strap and a fixing post, and the strap is fixedly disposed on the fixing post for fixing the drone.
  • the base is provided with a guide rail
  • the fixing post is disposed in the guide rail for adjusting the fixed post to meet the fixing requirements of the plurality of drones.
  • the column has at least one power socket disposed on an outer surface thereof, and the power socket protrudes from the surface of the pillar to facilitate connection of the power source to charge the drone.
  • the power socket is provided with a power interface, the power interface is connected to the power cable, the cable is wound on a turntable, and the turntable is driven by the motor to be able to retract the power cable, so that people can The drone is charging.
  • a control circuit is disposed in the column, the control circuit is composed of a WIFI module, a CPU, an upgrade module, a network interface, and a bus interface, wherein the CPU communicates with the background through a bus interface, and the WIFI module is connected to the CPU to implement wireless
  • the transmission and reception of data realizes intelligent control of the drone
  • the network interface is connected to the upgrade module
  • the lift module is connected to the CPU.
  • the network interface is disposed on the column and located above the power socket to facilitate connection with the drone, and the network interface may be an RJ45 interface or a USB interface.
  • the column is connected to a plurality of power sockets and a network interface, and each of the power sockets and the network interface corresponds to one storage compartment.
  • the integrated system for the setting of the drone realized by the invention can effectively collect the unmanned aerial vehicles by the structural design, and is convenient for the management and maintenance of the drone, and can effectively utilize the space, and is convenient for no
  • the transportation of man-machine enables the drone to be monitored over long distances, making it easy for the drone to achieve long distances. Applications such as shooting and surveying.
  • an integrated system is equipped with a plurality of drones to complete the functions of loading, accommodating, fixing, maintaining and charging the drone, and the software update and upgrade of the drone can be realized quickly and efficiently. Maintenance makes it easier to charge and maintain the drone.
  • Figure 1 is a schematic view of the structure of the present invention.
  • Figure 2 is a side elevational view of the implementation of the present invention.
  • FIG 3 is a schematic structural view of a base and a fixing device implemented by the present invention.
  • FIG. 4 is a schematic structural view of a fixing assembly 1 according to the present invention.
  • FIG. 5 is a schematic structural view of a fixing component 2 according to the present invention.
  • Figure 6 is a schematic view showing the structure of a column according to the present invention.
  • Fig. 7 is a schematic view showing the structure of a power supply in a column according to the present invention.
  • FIG. 8 is a diagram showing the control circuit implemented in the present invention.
  • Figure 9 is a schematic view of the application of the present invention.
  • the system includes a column 2 and a receiving area 1 including a plurality of receiving areas.
  • the hopper 11 is disposed in the accommodating chamber 11 for locating and fixing the drone 3.
  • the column 2 is disposed in the accommodating area 1.
  • the column is mainly used for supporting and fixing the accommodating chamber, and the accommodating chamber 11 is fixed by the drone. Device to fix the drone.
  • the storage compartment 11 has a plurality of, each storage compartment 11 passes through the partition wall 12 and the adjacent storage compartment 11 Distinguished, and as shown in the figure, the accommodating chamber 11 is disposed around the column 2, and the accommodating chamber 11 and the column 2 form a circular structure in a plan view to fully utilize the column 2 and the surrounding space to reduce the integrated system. Take up space.
  • the receiving compartment 11 has a top plate 111 and a base 112.
  • the base 112 is fixed to the lower part of the column 2, and the base 112 is provided with fixing means.
  • the top part 111 is disposed at the upper end of the column 2 for accommodating and protecting the drone 3 .
  • the fixing device comprises two parts: a fixing component 1 and a fixing component.
  • the fixing component 1 is composed of a fixing frame 12 and a strap 15 , and the fixing frame 12 has a supporting portion 121 .
  • the fixing portion 122, the fixing portion 122 is located at the upper end of the supporting portion 121, horizontally protrudes, and the fixing portion 122 has a strap hole 123 corresponding to the strap 15.
  • the UAV is fixed, the strap 15 is tied to the strap. Fixing the drone can be achieved by attaching the strap 15 through the strap hole 123 on the bracket of the human machine.
  • the fixing component 2 is composed of a strap 131 and a fixing post 13, wherein the strap 131 is fixedly disposed on the fixing post 13, and the strap 131 usually has a self-adhesive tape for fixing the drone.
  • the base 112 is provided with a guide rail 14 .
  • the fixed post 13 is disposed in the guide rail 14 , and the fixed post 13 can be adjusted through the guide rail 14 to meet the fixing requirements of various UAVs.
  • the strap 131 is passed through the bracket of the drone, and the drone can be fixed by self-adhesive means.
  • the column 2 has a cylindrical structure, and the inside thereof is hollow to provide a control circuit.
  • the outer surface is provided with a power socket 21 and a network interface 23, and a power source is disposed on the outer surface of the column 2 shown in the figure.
  • the seat 21 and the network interface 23 can actually be provided with a power base 21 and a network interface 23 corresponding to the position of the receiving compartment 11 on the column as needed to meet the needs of the plurality of drones.
  • the power socket 21 protrudes from the surface of the column 2, and the power socket 21 is provided with a power interface 22 for connecting the power source to charge the drone.
  • the network interface 23 is located above the power supply base 21 to facilitate connection with the drone.
  • the network interface can be an RJ45 interface or a USB interface.
  • the power supply base 21 is provided with a power interface (or a power plug) 22, and the power interface 22 is connected to the power line 24, and the cable 24 is wound on a turntable 25, and the turntable 25 passes
  • the motor shaft 26 is driven by the motor 27, and the turntable 25 can retract the power cord 25, so that people can charge the drone.
  • the column 2 is a hollow structure, and a control circuit is disposed in the column 2 , and the control circuit is composed of a WIFI module, a CPU, an upgrade module, a network interface, and a bus interface, wherein the CPU performs the bus interface and the background.
  • Communication WIFI module is connected to the CPU, realizes transmission and reception of wireless data, realizes intelligent control of the drone, the network interface is connected to the upgrade module, the lifting module is connected to the CPU, and the UAV needs to be upgraded or During maintenance, under the control of the CPU, the drone is connected through the network interface, and the upgrade module upgrades or maintains the drone.
  • the integrated system places the drone 3 in the accommodating compartment 11 when the drone 3 is installed, and then binds a bracket at the bottom of the drone 3 to the fixing bracket through the strap 15.
  • On the 12th when binding, you can pass a strap, you can also pass two straps, the binding of the two straps is fixed and more stable), and then tie the other bracket at the bottom of the drone 3 through the strap 131
  • Fixed to the fixed column 13, the structure of the fixed column 13 and the fixed frame 12, can be bound to the drone according to the actual situation, so that the drone can be firmly fixed, and the drone is not protected by other structures. Impact and collision.
  • the fixed column 13 can also adjust the distance from the fixed frame 12 in real time to meet the needs of different specifications of the drone.
  • the integrated system for the setting of the drone realized by the present invention can effectively collect the unmanned aerial vehicles by the structural design, and is convenient for the management and maintenance of the drone, and can effectively utilize the space. It facilitates the transportation of drones, enabling drones to be monitored over long distances, making it easy for drones to achieve long-distance shooting and surveying applications.
  • an integrated system is equipped with a plurality of drones to complete the functions of loading, accommodating, fixing, maintaining and charging the drone, and the software update and upgrade of the drone can be realized quickly and efficiently. Maintenance makes it easier to charge and maintain the drone.

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  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Catching Or Destruction (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

一种用于无人机设置的集成***，包括立柱（2）及容纳仓（11），立柱（2）用于支撑及固定容纳仓（11），立柱（2）设置于容纳仓（11）内，容纳仓（11）用以安置及固定无人机（3），容纳仓（11）内具有无人机（3）的固定装置，以对无人机（3）进行固定。该集成***能够有效地利用空间，便于无人机的管理和维护。

Description

一种用于无人机设置的集成*** 技术领域
本发明属于无人机技术领域，特别涉及一种无人机的智能控制及设置平台。
背景技术
无人驾驶飞机简称“无人机”，是利用无线电遥控设备和自备的程序控制装置操纵的不载人飞机。机上无驾驶舱，但安装有自动驾驶仪、程序控制装置等设备。地面、舰艇上或母机遥控站人员通过雷达等设备，对其进行跟踪、定位、遥控、遥测和数字传输。可在无线电遥控下像普通飞机一样起飞或用助推火箭发射升空，也可由母机带到空中投放飞行。回收时，可用与普通飞机着陆过程一样的方式自动着陆，也可通过遥控用降落伞或拦网回收。可反复使用多次。广泛用于空中侦察、监视、通信、反潜、电子干扰等。
虽然人们对于周边环境及交通、安全需要，无人机的应用越来越广。但是，目前的无人机通常是单个进行放飞，其放飞的时间有限，而且需要定时进行充电，无法实现长距离放飞，在对远距离区域进行拍摄、勘测等应用的情况下，难以实现，局限了无人机的应用。同时，无人机由于其造型的设计要求，难以运输，如果存在多个无人机的情况下，更容易引起混乱，而且多个无人机的充电导致接线及电源接口过多，配套设置难以跟上；还有，无人机的软件也需要定期升级、更新，目前的设计方式只能单机进行，不能进行批量升级或更新维护，效率低下。
如专利申请201620542343.5公开了一种模块化组合式多旋翼无人机，包括多个动力模块和控制模块。每个动力模块包括外壳和设置在外壳中的无人机单元，外壳为正六棱柱框架结构；外壳侧壁的外侧面上设置有连接件，连接件包括主动件和配合件；无人机单元包括电机和螺旋桨，电机与外壳固定连接，螺 旋桨固定在电机的输出轴上，控制模块与多个动力模块的电机之间电连接。通过多个动力模块组合的方式大大提高了无人机的载荷能力，通过一次设计达到了多架无人机的功能，节省了研发和制造成本。且拆卸、组装方便，操作简单。每个动力模块的外壳为正六棱柱框架结构，工整的蜂巢结构，使得多个动力模块的组合方式多样化。
但是上述的专利申请仅仅是将无人机设置在正六棱柱框架结构内，由此构成多个无人机的组合使用，提高设计和制造成本，对于运输及无人机的数据传输并无任何改进，仍然具有上述难以运输、管理及维护不方便的问题。
发明内容
基于此，因此本发明的首要目地是提供一种用于无人机设置的集成***，该***能够将无人机进行有效地归集，便于无人机的管理和维护，同时能够有效地利用空间，便于无人机的运输，使无人机能够进行长距离监控，便于无人机实现长距离拍摄及勘测等应用。
本发明的另一个目地是提供一种用于无人机设置的集成***，该***结构简单、易于实现，且能够快捷、高效地实现无人机的软件更新升级或维护，可便利地对无人机进行充电和保养。
为实现上述目的，本发明的技术方案为：
一种用于无人机设置的集成***，其特征在于该***包括有立柱及容纳仓，所述容纳仓内用以安置及固定无人机，所述立柱设置于容纳仓内，立柱主要用于支撑及固定容纳仓，所述容纳仓内具有无人机的固定装置，以对无人机进行固定。
所述容纳仓包括有复数个，复数个容纳仓形成容纳区域，使本集成***能够装设多个无人机；所述复数个容纳仓环绕于立柱设置，以充分利用空间和立柱，减小占用空间。
进一步，所述容纳仓具有顶板及底座，所述底座固定在立柱的下部，所述 底座上设置有固定装置，所述顶部设置于立柱的上端，用于容纳及保护无人机。
进一步，所述固定装置，包括有固定组件一，所述固定组件一由固定架及束带构成，所述固定架的一侧设置有束带孔，束带孔用以穿过束带，以将无人机通过束带进行固定。
更进一步，所述固定装置，还包括有固定组件二，所述固定组件二由束带及固定柱构成，所述束带固定设置在固定柱上，用以固定无人机。
更进一步，所述底座上设置有导轨，所述固定柱设置于该导轨中，用以对固定柱进行调整，可以满足多种无人机的固定需求。
所述立柱，其外表面上设置有至少一个电源座，所述电源座突出于立柱表面，以便于进行连接电源，对无人机进行充电。
进一步，所述电源座内设置有电源接口，所述电源接口连接于电源线，所述电缆线缠绕于一转盘上，且该转盘被电机带动，以能够对电源线进行收放，便于人们对无人机进行充电操作。
进一步，所述立柱中设置有控制电路，所述控制电路由WIFI模块、CPU、升级模块及网络接口、总线接口构成，其中，CPU通过总线接口与后台进行通讯，WIFI模块连接于CPU，实现无线数据的传输和接收，实现对无人机的智能控制，所述网络接口连接于升级模块，所述升降模块连接于CPU，在需要对无人机升级或维护的时候，在CPU的控制下，通过网络接口连接无人机，升级模块对无人机进行升级或维护。
更进一步，所述网络接口设置在立柱上，并位于电源座的上方，以便于与无人机进行连接，所述网络接口可以为RJ45接口或USB接口。
更进一步，所述立柱上均与复数个电源座及网络接口，每个电源座及网络接口对应于一个容纳仓。
本发明所实现的用于无人机设置的集成***，通过结构设计，该***能够将无人机进行有效地归集，便于无人机的管理和维护，同时能够有效地利用空间，便于无人机的运输，使无人机能够进行长距离监控，便于无人机实现长距 离拍摄及勘测等应用。
且可以依据实际需要，一个集成***装设有多个无人机，完成对无人机的装载、容纳、固定、维护及充电的功能，能够快捷、高效地实现无人机的软件更新升级或维护，更加便于对无人机进行充电和保养。
附图说明
图1为本发明所实施的结构示意图。
图2为本发明所实施的侧视图。
图3为本发明所实施底座及固定装置的结构示意图。
图4为本发明所实施固定组件一的结构示意图。
图5为本发明所实施固定组件二的结构示意图。
图6为本发明所实施立柱的结构示意图。
图7为本发明所实施立柱中电源结构的示意图。
图8为本发明所实施控制电路图。
图9为本发明所实施的应用示意图。
具体实施方式
为了使本发明的目的、技术方案及优点更加清楚明白，以下结合附图及实施例，对本发明进行进一步详细说明。应当理解，此处所描述的具体实施例仅仅用以解释本发明，并不用于限定本发明。
参见图1、图2所示，为本发明所实现的用于无人机设置的集成***，图中所示，该***包括有立柱2及容纳区域1，该容纳区域1包括有多个容纳仓11，容纳仓11内用以安置及固定无人机3，所述立柱2设置于容纳区域1内，立柱主要用于支撑及固定容纳仓，所述容纳仓11内具有无人机的固定装置，以对无人机进行固定。
所述容纳仓11具有复数个，每个容纳仓11通过间隔壁12与相邻容纳仓11 区别开来，且如图中所示，容纳仓11环绕于立柱2设置，容纳仓11和立柱2形成一个俯视图呈圆状的结构，以充分利用立柱2和周围的空间，减小该集成***的占用空间。
容纳仓11具有顶板111及底座112，所述底座112固定在立柱2的下部，且底座112上设置有固定装置，所述顶部111设置于立柱2的上端，用于容纳及保护无人机3。
结合图3、图4、图5所示，固定装置，包括有固定组件一和固定组件二两个部分，其中，固定组件一由固定架12及束带15构成，固定架12具有支撑部121和固定部122，固定部122位于支撑部121的上端，水平伸出，且固定部122上具有对应于束带15的束带孔123，固定无人机时，将束带15套系于无人机的支架上，然后把束带15穿过束带孔123绑紧，即可实现对无人机的固定。
固定组件二由束带131及固定柱13构成，其中，束带131固定设置在固定柱13上，束带131上通常具有自粘带，用以固定无人机。
底座112上设置有导轨14，上述固定柱13设置于该导轨14中，通过导轨14可以对固定柱13进行调整，可以满足多种无人机的固定需求。使用时，将束带131穿过无人机的支架，通过自粘的方式即可对无人机进行固定。
再如图6所示，立柱2为圆柱形结构，其内部中空，用以设置控制电路，外表面上设置电源座21和网络接口23，图中所显示立柱2的外表面上设置有一个电源座21和网络接口23，实际上可以依据需要，将立柱上对应于容纳仓11的位置都设置有电源座21和网络接口23，以满足多个无人机的需要。
电源座21突出于立柱2的表面，电源座21内设置有电源接口22，以便于进行连接电源，对无人机进行充电。
网络接口23位于电源座21的上方，以便于与无人机进行连接，一般情况下，网络接口可以为RJ45接口或USB接口。
结合图7所示，电源座21内设置有电源接口(或为电源插头)22，电源接口22连接于电源线24，所述电缆线24缠绕于一转盘25上，且该转盘25通过 电机轴26被电机27带动，转盘25能够对电源线25进行收放，便于人们对无人机进行充电操作。
结合图8所示，立柱2为中空结构，在立柱2中设置有控制电路，所述控制电路由WIFI模块、CPU、升级模块及网络接口、总线接口构成，其中，CPU通过总线接口与后台进行通讯，WIFI模块连接于CPU，实现无线数据的传输和接收，实现对无人机的智能控制，所述网络接口连接于升级模块，所述升降模块连接于CPU，在需要对无人机升级或维护的时候，在CPU的控制下，通过网络接口连接无人机，升级模块对无人机进行升级或维护。
结合图9所示，本集成***在装设无人机3时，将无人机3放置在容纳仓11中，然后通过束带15将无人机3底部的一个支架绑定固定在固定架12上(绑定时，可以通过一个束带，也可以通过两个束带，两个束带进行绑定是固定更稳固)，再通过束带131将无人机3底部的另一个支架绑定固定在固定柱13上，固定柱13和固定架12的结构设置，能够根据实际情况绑定无人机，使无人机既能稳固地固定，又保持无人机不被其它的结构所影响及碰撞。
固定柱13还可以实时调整与固定架12的间距，以满足不同规格无人机的需求。
总之，本发明所实现的用于无人机设置的集成***，通过结构设计，该***能够将无人机进行有效地归集，便于无人机的管理和维护，同时能够有效地利用空间，便于无人机的运输，使无人机能够进行长距离监控，便于无人机实现长距离拍摄及勘测等应用。
且可以依据实际需要，一个集成***装设有多个无人机，完成对无人机的装载、容纳、固定、维护及充电的功能，能够快捷、高效地实现无人机的软件更新升级或维护，更加便于对无人机进行充电和保养。
以上所述仅为本发明的较佳实施例而已，并不用以限制本发明，凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等，均应包含在本发明的保护范围之内。

Claims (10)

  1. 一种用于无人机设置的集成***，其特征在于该***包括有立柱及容纳仓，所述容纳仓内用以安置及固定无人机，所述立柱设置于容纳仓内，立柱主要用于支撑及固定容纳仓，所述容纳仓内具有无人机的固定装置，以对无人机进行固定。
  2. 如权利要求1所述的用于无人机设置的集成***，其特征在于所述容纳仓包括有复数个，所述复数个容纳仓环绕于立柱设置，以充分利用空间和立柱，减小设置空间。
  3. 如权利要求1所述的用于无人机设置的集成***，其特征在于所述容纳仓具有顶板及底座，所述底座固定在立柱的下部，所述底座上设置有固定装置，所述顶部设置于立柱的上端，用于容纳及保护无人机。
  4. 如权利要求3所述的用于无人机设置的集成***，其特征在于所述固定装置，包括有固定组件一，所述固定组件一由固定架及束带构成，所述固定架的一侧设置有束带孔，束带孔用以穿过束带，以将无人机通过束带进行固定。
  5. 如权利要求4所述的用于无人机设置的集成***，其特征在于所述固定装置，还包括有固定组件二，所述固定组件二由束带及固定柱构成，所述束带固定设置在固定柱上，用以固定无人机。
  6. 如权利要求5所述的用于无人机设置的集成***，其特征在于所述底座上设置有导轨，所述固定柱设置于该导轨中，用以对固定柱进行调整，可以满足多种无人机的固定需求。
  7. 如权利要求1所述的用于无人机设置的集成***，其特征在于所述立柱，其外表面上设置有至少一个电源座，所述电源座突出于立柱表面，以便于进行连接电源，对无人机进行充电。
  8. 如权利要求7所述的用于无人机设置的集成***，其特征在于所述电源座内设置有电源接口，所述电源接口连接于电源线，所述电缆线缠绕于一转盘上，且该转盘被电机带动，以能够对电源线进行收放，便于人们对无人机进行 充电操作。
  9. 如权利要求1所述的用于无人机设置的集成***，其特征在于所述立柱中设置有控制电路，所述控制电路由WIFI模块、CPU、升级模块及网络接口、总线接口构成，其中，CPU通过总线接口与后台进行通讯，WIFI模块连接于CPU，实现无线数据的传输和接收，实现对无人机的智能控制，所述网络接口连接于升级模块，所述升降模块连接于CPU，在需要对无人机升级或维护的时候，在CPU的控制下，通过网络接口连接无人机，升级模块对无人机进行升级或维护。
  10. 如权利要求7所述的用于无人机设置的集成***，其特征在于所述网络接口设置在立柱上，并位于电源座的上方，以便于与无人机进行连接，所述网络接口可以为RJ45接口或USB接口；所述立柱上均与复数个电源座及网络接口，每个电源座及网络接口对应于一个容纳仓。
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Publication number Priority date Publication date Assignee Title
CN107201843A (zh) * 2017-06-09 2017-09-26 东莞市晶益电子科技有限公司 一种用于无人机设置的集成***
CN110001823B (zh) * 2019-04-19 2021-10-01 南昌航空大学 一种组合式智能交通工具***
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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202410159U (zh) * 2011-11-29 2012-09-05 张耀辉 遥控飞机模型高台停机坪
CN204024112U (zh) * 2014-06-18 2014-12-17 深圳市宝联风光热能源科技有限公司 一种风光互补供电岗亭
DE202015102833U1 (de) * 2014-05-30 2015-10-28 Geola Technologies Ltd. Lade- und Wiederbereitstellungsstation für Elektro- und Hybrid UAVs
CN205239948U (zh) * 2015-12-10 2016-05-18 深圳众瑞光科技有限公司 无人机天空树及天空森林
CN105863353A (zh) * 2016-06-09 2016-08-17 徐洪军 一种小型无人机机群的起降补给机器人
CN106628219A (zh) * 2017-01-24 2017-05-10 中信戴卡股份有限公司 一种旋翼无人机停驻装置及其无人机充电套件
CN107201843A (zh) * 2017-06-09 2017-09-26 东莞市晶益电子科技有限公司 一种用于无人机设置的集成***

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202410159U (zh) * 2011-11-29 2012-09-05 张耀辉 遥控飞机模型高台停机坪
DE202015102833U1 (de) * 2014-05-30 2015-10-28 Geola Technologies Ltd. Lade- und Wiederbereitstellungsstation für Elektro- und Hybrid UAVs
CN204024112U (zh) * 2014-06-18 2014-12-17 深圳市宝联风光热能源科技有限公司 一种风光互补供电岗亭
CN205239948U (zh) * 2015-12-10 2016-05-18 深圳众瑞光科技有限公司 无人机天空树及天空森林
CN105863353A (zh) * 2016-06-09 2016-08-17 徐洪军 一种小型无人机机群的起降补给机器人
CN106628219A (zh) * 2017-01-24 2017-05-10 中信戴卡股份有限公司 一种旋翼无人机停驻装置及其无人机充电套件
CN107201843A (zh) * 2017-06-09 2017-09-26 东莞市晶益电子科技有限公司 一种用于无人机设置的集成***

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