CN111439143A - A UAV recycling system and recycling method thereof - Google Patents
A UAV recycling system and recycling method thereof Download PDFInfo
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- CN111439143A CN111439143A CN202010397282.9A CN202010397282A CN111439143A CN 111439143 A CN111439143 A CN 111439143A CN 202010397282 A CN202010397282 A CN 202010397282A CN 111439143 A CN111439143 A CN 111439143A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/35—Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
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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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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Abstract
Description
技术领域technical field
本发明涉及无人机技术领域,特别涉及一种无人机回收系统及其回收方法。The present invention relates to the technical field of unmanned aerial vehicles, and in particular, to an unmanned aerial vehicle recovery system and a recovery method thereof.
背景技术Background technique
无人机是无人驾驶飞机的简称,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,或者由车载计算机完全地或间歇地自主地操作。无人机在执行任务时,一般搭载在移动的回收母体上(如车辆、轮船等运输设备)。由于无人机的续航时间受限制,在执行一定时长的任务后,需要对无人机进行充电。而此时回收母体处于高速行驶状态,无人机飞回运输设备时,受二者时速差的影响,无人机很难与移动的回收母体上的充电装置对接。而且无人机在充电时,若有紧急任务,无法及时脱离充电装置进行起飞。UAV is the abbreviation of unmanned aircraft, which is an unmanned aircraft operated by radio remote control equipment and self-provided program control device, or operated completely or intermittently autonomously by on-board computer. When UAVs perform tasks, they are generally carried on mobile recycling mothers (such as vehicles, ships and other transportation equipment). Due to the limited battery life of the UAV, the UAV needs to be recharged after performing a certain period of tasks. At this time, the recycling matrix is in a high-speed driving state, and when the drone flies back to the transport equipment, it is difficult for the drone to dock with the charging device on the moving recycling matrix due to the speed difference between the two. Moreover, when the drone is charging, if there is an emergency task, it cannot be separated from the charging device in time to take off.
因此,现有技术有待发展。Therefore, the existing technology needs to be developed.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于克服现有技术中存在的缺点,提供一种无人机回收系统及其回收方法,使得本发明的无人机能够自动与无人机回收站精准对接以进行充电,同时能够及时解除充电状态以快速进行再次飞行任务,也能回收至无人机回收站内。The purpose of the present invention is to overcome the shortcomings in the prior art, and to provide a UAV recycling system and a recycling method thereof, so that the UAV of the present invention can be automatically and accurately docked with the UAV recycling station for charging, and at the same time it can The charging state can be released in time to quickly perform another flight mission, and it can also be recycled to the drone recycling station.
为了实现上述目的,本发明提供如下技术方案:In order to achieve the above object, the present invention provides the following technical solutions:
本发明提供了一种无人机回收系统,包括无人机、无人机回收站和回收控制器,其中The present invention provides an unmanned aerial vehicle recycling system, including an unmanned aerial vehicle, an unmanned aerial vehicle recycling station and a recycling controller, wherein
所述无人机包括无人机主体、以及与无人机主体电性连接的可升降充电装置,所述可升降充电装置包括驱动装置、充电体以及电性连接无人机主体、充电体的牵引线缆,所述驱动装置驱动所述充电体上升或下降,所述充电体的外侧壁设置有两个极性相反且与所述牵引线缆电性连接的第一电极,所述充电体的底部设置有第一磁铁;The drone includes a drone body and a liftable charging device that is electrically connected to the drone body, the liftable charging device includes a drive device, a charging body, and a device that is electrically connected to the drone body and the charging body. A traction cable, the driving device drives the charging body to ascend or descend, the outer side wall of the charging body is provided with two first electrodes with opposite polarities and electrically connected to the traction cable, the charging body The bottom is provided with a first magnet;
所述无人机回收站包括壳体,所述壳体的上端设置有开口,所述壳体靠近底部的内侧壁间隔设置有两个极性相反且可与所述第一电极电性导通的第二电极,所述第二电极与外部的供电电源电性连接,所述壳体的底部设置有定位装置、以及可与所述第一磁铁吸附的第二磁铁;The UAV recycling station includes a casing, the upper end of the casing is provided with an opening, and the inner sidewall of the casing close to the bottom is spaced with two opposite polarities and can be electrically connected to the first electrode. the second electrode, the second electrode is electrically connected with the external power supply, the bottom of the casing is provided with a positioning device, and a second magnet that can be adsorbed with the first magnet;
所述回收控制器分别与所述无人机、无人机回收站通信连接。The recycling controller is connected in communication with the drone and the drone recycling station, respectively.
进一步地,所述无人机本体设置有充电端口,所述充电端口的正负极分别通过所述牵引线缆与对应的所述第一电极电性连接,所述供电电源的正负极分别与对应的所述第二电极电性连接。Further, the drone body is provided with a charging port, the positive and negative electrodes of the charging port are respectively electrically connected to the corresponding first electrodes through the traction cable, and the positive and negative electrodes of the power supply are respectively is electrically connected to the corresponding second electrode.
进一步地,所述无人机主体的外围设置有保护装置,所述保护装置包括设置于所述无人机主体上端的上护板、设置于所述无人机主体下端的下护板、以及连接所述上护板、下护板的固定件,所述下护板开设有对应所述充电体的通孔。Further, a protection device is provided on the periphery of the drone body, and the protection device includes an upper guard plate arranged at the upper end of the drone body, a lower shield plate arranged at the lower end of the drone body, and A fixing piece connecting the upper guard plate and the lower guard plate, and the lower guard plate is provided with a through hole corresponding to the charging body.
进一步地,所述可升降充电装置还包括支架结构,所述支架结构包括两个分别设置于所述下护板的立柱、以及连接两个立柱的横柱,所述驱动装置包括设置于所述横柱一端的电机,所述牵引线缆缠绕于所述横柱上。Further, the liftable charging device further includes a support structure, the support structure includes two uprights respectively disposed on the lower guard plate, and a transverse column connecting the two uprights, and the driving device includes a The motor at one end of the horizontal column, and the traction cable is wound on the horizontal column.
进一步地,所述充电体为倒圆锥体结构,两个所述第一电极分别间隔环设于倒圆锥体结构的斜面,且所述第一电极的电极面朝下,所述第一磁铁设置于倒圆锥体结构的顶点位置。Further, the charging body is an inverted cone structure, the two first electrodes are respectively arranged on the inclined surface of the inverted cone structure at intervals, and the electrodes of the first electrodes face downwards, and the first magnet is provided at the vertex position of the inverted cone structure.
进一步地,所述壳体为漏斗结构,其直径由下往上逐渐增大,所述第二电极分别间隔环设于漏斗结构的斜面,且所述第二电极的电极面朝上与所述第一电极的电极面配合。Further, the casing is a funnel structure, and its diameter gradually increases from bottom to top, the second electrodes are respectively arranged on the inclined surface of the funnel structure at intervals, and the electrodes of the second electrodes face upwards and the The electrode surfaces of the first electrodes are matched.
进一步地,所述无人机回收站还包括固定结构和卡合结构,所述固定结构包括安装板和若干个设置于安装板上的支撑柱,所述支撑柱支撑所述壳体,所述卡合结构包括若干个水平穿设于所述支撑柱上的卡接件,所述壳体的侧壁开设有对应所述卡接件的卡槽,所述卡接件可穿过所述卡槽以限制所述充电体的活动范围。Further, the unmanned aerial vehicle recycling station further includes a fixing structure and a snap-fit structure, the fixing structure includes a mounting plate and a plurality of supporting columns arranged on the mounting plate, the supporting columns support the casing, and the The clamping structure includes a plurality of clamping pieces horizontally penetrated on the support column, the side wall of the casing is provided with a clamping slot corresponding to the clamping pieces, and the clamping pieces can pass through the clamping pieces. slot to limit the range of motion of the charging body.
进一步地,所述上护板、下护板及固定件采用树脂材质。Further, the upper guard plate, the lower guard plate and the fixing piece are made of resin material.
本发明还提供了一种无人机回收方法,应用于如上述所述的无人机回收系统,包括以下步骤:The present invention also provides a UAV recovery method, which is applied to the UAV recovery system as described above, comprising the following steps:
步骤A:所述无人机控制器向所述无人机发送回收指令,使所述无人机朝所述定位装置方向飞行;Step A: the UAV controller sends a recovery instruction to the UAV, so that the UAV flies in the direction of the positioning device;
步骤B:所述无人机飞行至所述无人机回收站的开口范围内,所述驱动装置运行并带动所述充电体下降,所述充电体沿着所述无人机回收站的内侧壁滑动;Step B: the drone flies to the opening of the drone recycling station, the driving device operates and drives the charging body to descend, and the charging body is along the inner side of the drone recycling station wall sliding;
步骤C:所述充电体滑动至无人机回收站的底部,所述第一磁铁和所述第二磁铁吸附固定所述充电体和所述无人机回收站,所述第一电极与所述第二电极相贴合电性导通。Step C: The charging body slides to the bottom of the drone recycling station, the first magnet and the second magnet adsorb and fix the charging body and the drone recycling station, and the first electrode is connected to the drone recycling station. The second electrodes are in contact with each other and are electrically connected.
进一步地,还包括步骤D:所述卡接件穿过所述卡槽抵住所述充电体的上端面,所述无人机向下飞行降落至所述无人机回收站中。Further, the method further includes step D: the clamping piece passes through the clamping slot and abuts against the upper end surface of the charging body, and the drone flies downward and landed in the drone recycling station.
本发明技术方案具有的有益效果:The beneficial effects that the technical solution of the present invention has:
本发明的无人机回收系统及其回收方法,通过设置无人机和无人机回收站,无人机主体电性连接有可升降充电装置,并由驱动装置驱动充电体上升或下降,同时无人机回收站包括上端开口的壳体,充电体设置有第一电极和第一磁铁,壳体设置有第二电极、定位装置和第二磁铁,当无人机朝着定位装置方向飞行至壳体开口的范围内,驱动装置运行并带动充电体下降至壳体的底部内,此时第一磁铁和第二磁铁磁吸固定,第一电极和第二电极贴合连通以对无人机进行充电,如果无人机需要再次执行任务时,驱动装置运行带动充电体上升收回即可,如果无人机需要回收时,无人机下降至壳体内即可,使得本发明的无人机能够自动与无人机回收站精准对接以进行充电,同时能够及时解除充电状态以快速进行再次飞行任务,也能回收至无人机回收站内。In the UAV recycling system and the recycling method of the present invention, by setting up the UAV and the UAV recycling station, the main body of the UAV is electrically connected with a liftable charging device, and the driving device drives the charging body to ascend or descend, and at the same time The UAV recycling station includes a casing with an open upper end, the charging body is provided with a first electrode and a first magnet, and the casing is provided with a second electrode, a positioning device and a second magnet. Within the range of the opening of the casing, the driving device operates and drives the charging body to descend to the bottom of the casing. At this time, the first magnet and the second magnet are magnetically fixed, and the first electrode and the second electrode are connected to each other to connect the drone to the drone. For charging, if the drone needs to perform the task again, the driving device can run to drive the charging body to rise and retract. If the drone needs to be recovered, the drone can be lowered into the housing, so that the drone of the present invention can It can be automatically docked with the UAV recycling station for charging, and at the same time, the charging state can be released in time to quickly perform another flight mission, and it can also be recycled to the UAV recycling station.
附图说明Description of drawings
图1是本发明无人机的结构示意图;Fig. 1 is the structural representation of unmanned aerial vehicle of the present invention;
图2是本发明充电体的结构示意图;2 is a schematic structural diagram of a charging body of the present invention;
图3是本发明无人机回收站的结构示意图;Fig. 3 is the structural representation of the UAV recycling station of the present invention;
图4是图3中A的放大图;Fig. 4 is the enlarged view of A in Fig. 3;
图5是本发明无人机回收站另一角度的结构示意图;5 is a schematic structural diagram of another angle of the UAV recycling station of the present invention;
图6是图5中B的放大图;Fig. 6 is the enlarged view of B in Fig. 5;
图7是本发明无人机回收方法的流程图;Fig. 7 is the flow chart of the UAV recovery method of the present invention;
图8是本发明无人机飞行至无人机回收站上方的示意图;8 is a schematic diagram of the drone of the present invention flying to the top of the drone recycling station;
图9是本发明无人机下放充电体的示意图;Fig. 9 is the schematic diagram of the unmanned aerial vehicle of the present invention lowering the charging body;
图10是本发明充电体沿无人机回收站滑落的示意图;10 is a schematic diagram of the charging body of the present invention sliding down along the UAV recycling station;
图11是本发明无人机在无人机回收站内充电的示意图;Fig. 11 is the schematic diagram of the unmanned aerial vehicle of the present invention charging in the unmanned aerial vehicle recycling station;
图12是本发明卡接件抵住充电体的示意图;Fig. 12 is a schematic diagram of the present invention's clip against the charging body;
图13是本发明无人机收容于无人机回收站中的示意图;13 is a schematic diagram of the drone of the present invention being accommodated in a drone recycling station;
附图标记说明:Description of reference numbers:
10-无人机,11-无人机主体,121-电机,122-充电体,1221-第一电极,1222-第一磁铁,123-牵引线缆,13-保护装置,131-上护板,132-下护板,1321-通孔,133-固定件,134-气流孔,14-支架结构,141-立柱,142-横柱,20-无人机回收站,21-壳体,211-开口,212-第二电极,214-第二磁铁,215-卡槽,22-固定结构,221-安装板,222-支撑柱,23-卡合结构,231-卡接件。10-UAV, 11-UAV body, 121-motor, 122-charging body, 1221-first electrode, 1222-first magnet, 123-traction cable, 13-protection device, 131-upper guard plate , 132-lower guard plate, 1321-through hole, 133-fixing piece, 134-airflow hole, 14-support structure, 141-upright column, 142-cross column, 20-drone recycling station, 21-shell, 211 - Opening, 212 - second electrode, 214 - second magnet, 215 - card slot, 22 - fixing structure, 221 - mounting plate, 222 - support column, 23 - snap structure, 231 - snap connector.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,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。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the specific embodiments described herein are only used to explain the present invention, and are not intended to limit the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
需要说明,本发明实施例中所有方向性指示(诸如上、下、左、右、前、后……)仅用于解释在某一特定姿态(如附图所示)下各部件之间的相对位置关系、运动情况等,如果该特定姿态发生改变时,则该方向性指示也相应地随之改变。It should be noted that all directional indications (such as up, down, left, right, front, back, etc.) in the embodiments of the present invention are only used to explain the relationship between various components under a certain posture (as shown in the accompanying drawings). The relative positional relationship, the movement situation, etc., if the specific posture changes, the directional indication also changes accordingly.
在本发明中,除非另有明确的规定和限定,术语“连接”、“固定”等应做广义理解,例如,“连接”可以是固定连接,也可以是可拆卸连接,或成一体;可以是机械连接,也可以是电连接;可以是直接相连,也可以通过中间媒介间接相连,可以是两个元件内部的连通或两个元件的相互作用关系,除非另有明确的限定。对于本领域的普通技术人员而言,可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, unless otherwise expressly specified and limited, the terms "connection" and "fixed" should be understood in a broad sense. For example, "connection" may be a fixed connection, a detachable connection, or an integrated; It can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be an internal communication between two elements or an interaction relationship between the two elements, unless otherwise explicitly defined. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific situations.
另外,在本发明中如涉及“第一”、“第二”等的描述仅用于描述目的,而不能理解为指示或暗示其相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个该特征。In addition, descriptions such as "first", "second", etc. in the present invention are only for descriptive purposes, and should not be construed as indicating or implying their relative importance or implicitly indicating the number of indicated technical features. Thus, a feature delimited with "first", "second" may expressly or implicitly include at least one of that feature.
请参考图1至图6,本发明提供了一种无人机回收系统,包括无人机10、无人机回收站20和回收控制器,在本实施方式中,所述无人机回收站20安装于移动的回收母体上(如车辆、轮船、火车、飞机等运输设备),或者所述无人机回收站20具有稳定移动的功能;Please refer to FIG. 1 to FIG. 6 , the present invention provides a UAV recycling system, including a
其中,所述无人机10包括无人机主体11、以及与无人机主体11电性连接的可升降充电装置,所述可升降充电装置包括驱动装置、充电体122以及电性连接无人机主体11、充电体122的牵引线缆123,所述驱动装置驱动所述充电体122上升或下降,所述充电体122的外侧壁设置有两个极性相反且与所述牵引线缆123电性连接的第一电极1221,即所述第一电极1221通过所述牵引线缆123与所述充电体122连接,所述充电体122的底部设置有第一磁铁1222;The
所述无人机回收站20包括壳体21,所述壳体21的上端设置有开口211,所述壳体21靠近底部的内侧壁间隔设置有两个极性相反且可与所述第一电极1221电性导通的第二电极212,所述第二电极212与外部的供电电源电性连接,所述壳体21的底部设置有定位装置、以及可与所述第一磁铁1222吸附的第二磁铁214;The
所述回收控制器分别与所述无人机10、无人机回收站20通信连接,用于控制所述无人机10的飞行状态、所述驱动装置的运行状态以及所述定位装置的工作状态。The recovery controller is respectively connected to the
当所述无人机10需要充电时,所述回收控制器发送回收指令给所述无人机10,并修订定位装置的向上偏移定位信息(必须超过所述壳体21开口211,保证所述无人机10不会与所述壳体21撞击),将修订后的定位信息发送给所述无人机10,所述无人机10飞行至修订后的定位信息位置处,此时所述无人机10处于所述壳体21的开口211范围内,然后所述回收控制器启动所述驱动装置旋转以将所述充电体122下放,所述充电体122沿着所述壳体21的内侧壁滑落,当其接近所述壳体21的底部,所述第一磁铁1222和所述第二磁铁214吸附固定,所述充电体122与所述无人机回收站20紧贴在一起,同时所述第一电极1221和所述第二电极212相连通,使得外部的供电电源可以对所述无人机10进行充电。此时,所述无人机10可在所述壳体21开口211的上方持续飞行,如需再次执行任务,所述回收控制器启动所述驱动装置旋转将所述充电体122上升收回,所述无人机10即可向目的地飞行。When the
由于仅仅是靠所述第一磁铁1222和第二磁铁214的磁吸作用吸紧所述充电体122,所述无人机10收回所述充电体122无需额外动力,能够快速进行再次执行飞行任务,解决了所述无人机10充电、及时放飞以再次执行飞行任务的问题。Since the charging
当需要回收所述无人机10时,所述无人机10逐渐下降容置于所述无人机回收站20的底部内,并且所述驱动装置旋转将所述牵引线缆123缠绕,从而完成对所述无人机10的回收。所述无人机10充电、回收的过程中无需人工进行对接、拾取,整个过程自动、安全,方便操作。When the
由于所述无人机10和所述无人机回收站20之间受时速差及定位精度的影响,同时受所述无人机10的距离探测精度及空气阻力等影响,所述无人机无10法精确飞行至所述无人机回收站20的正上方,因此,本发明的壳体21开口211远大于所述无人机10整体,能够确保所述无人机10能够保持在所述壳体21的开口211范围内,同时通过第一磁铁1222和第二磁铁214的磁吸固定,提高对所述无人机10充电、回收的准确度和精度。Because the speed difference between the
在本实施方式中,所述无人机主体11内设置有可充电电池,所述充电体122与该可充电电池电性连接,以对所述无人机主体11进行充电,保证所述无人机10的续航能力;所述回收控制器可通过有线或者无线的方式与所述无人机回收站20通信连接,同时通过无线的方式与所述无人机10通信连接,以对所述无人机10进行远程控制;所述连接线123可采用软性电缆线,保证上升或者下降时的弹性度和自由弯曲度;所述充电体122可为塑料外壳。In this embodiment, the
优选地,所述无人机本体11设置有充电端口,所述充电端口的正负极分别通过所述牵引线缆123与对应的所述第一电极1221电性连接,所述供电电源的正负极分别与对应的所述第二电极212电性连接,其中所述第一电极1221、第二电极214也对应分为正、负极,使得本发明的无人机回收站20能够给所述无人机10进行充电和回收,无需人工操作,方便使用。Preferably, the
进一步地,所述无人机主体11的外围设置有保护装置13,所述保护装置13用于保护所述无人机主体11,防止所述无人机10与所述无人机回收站20碰撞损坏,所述保护装置13包括设置于所述无人机主体11上端的上护板131、设置于所述无人机主体11下端的下护板132、以及连接所述上护板131、下护板132的固定件133,所述下护板132开设有对应所述充电体122的通孔1321,所述充电体122经过所述通孔1321进行上升或者下降。Further, a
在本实施方式中,所述上护板131、下护板132均设置有气流孔134,使得气流得以经所述气流孔134排出,不影响所述无人机10机翼所生成的气流出入和无人机镜头的观察,保证所述无人机10功能的正常使用;所述上护板131、下护板132及固定件133可以采用树脂材质,具有良好的机械性能,能够提供良好的保护作用,防止所述无人机10撞击损坏;所述上护板131、下护板132以及固定件133可以采用一体成型结构,提高所述无人机10整体的稳定性。In this embodiment, both the
请继续参考图1,所述可升降充电装置还包括支架结构14,所述支架结构14包括两个分别设置于所述下护板132的立柱141、以及连接两个立柱141的横柱142,所述驱动装置包括设置于所述横柱142一端的电机121,所述牵引线缆123缠绕于所述横柱142上,可以展开或者收拢,从而实现所述充电体122的下降和上升。Please continue to refer to FIG. 1 , the liftable charging device further includes a
其中,所述横柱142的一端与所述电机121的传动轴连接,另一端与其中一个所述立柱141转动连接,例如可通过轴承连接等。所述充电体122收起时所述牵引线缆123缠绕于所述横柱142上,当所述充电体122需要下放时,所述电机121驱动带动所述横柱142旋转,使得缠绕于所述横柱142的牵引线缆123跟着旋转下放,从而所述充电体122能够凭借自身的重力作用下降至所述壳体21内;当需要收起所述充电体122时,所述电机121反方向旋转收起所述牵引线缆123和所述充电体122。Wherein, one end of the
作为一种实施例,所述充电体122为倒圆锥体结构,两个所述第一电极1221分别间隔环设于倒圆锥体结构的斜面,即所述第一电极1221呈倒台阶式设置,防止两所述第一电极1221误触,且所述第一电极1221的电极面朝下,所述第一磁铁1222设置于倒圆锥体结构的顶点位置,即所述第一磁铁1222设置于所述充电体122的底部。As an embodiment, the charging
对应地,所述壳体21为漏斗结构,其直径由下往上逐渐增大,使得所述壳体21的开口211能够容置所述无人机10,而且所述充电体122能够沿着所述漏斗结构的斜面逐渐下落,整个过程稳定平缓,同时所述壳体21由上往下逐渐收紧,能够稳定夹持所述无人机10,所述第二电极212分别间隔环设于漏斗结构的斜面,即所述第二电极212呈台阶式设置,与所述第一电极1221对应设置,且所述第二电极212的电极面朝上与所述第一电极1221的电极面配合。Correspondingly, the
采用倒圆锥结构与漏斗结构的配合,增加了所述无人机10和所述无人机回收站20的配合范围,避免因微小误差而导致所述无人机10不能完成充电、回收的操作,而且所述无人机回收站20的直径逐渐收紧,使得所述充电体122的对接精确度和稳定性能够进一步提高。The combination of the inverted cone structure and the funnel structure increases the range of cooperation between the
进一步地,所述无人机回收站20还包括固定结构22和卡合结构23,所述固定结构22包括安装板221和若干个设置于安装板221上的支撑柱222,所述支撑柱222支撑所述壳体21,提高所述无人机回收站20的稳定性,避免因风力等导致所述壳体21出现倾斜的情况,所述卡合结构23包括若干个水平穿设于所述支撑柱222上的卡接件231,所述壳体21的侧壁开设有对应所述卡接件231的卡槽215,所述卡接件231可穿过所述卡槽215以限制所述充电体122的活动范围。Further, the unmanned aerial
在本实施方式中,所述安装板221用于将所述无人机回收站20固定在移动的回收母体上,如车辆、轮船、火车、飞机等运输设备;或者在所述安装板221下安装有移动结构。In this embodiment, the mounting
当所述充电体122由所述第二磁铁214磁吸固定后,所述卡接件231伸出穿过所述卡槽215以抵住所述充电体122的上端面,从而固定所述充电体122,防止所述充电体122晃动脱离,所述无人机10可降落至所述壳体21内,完成对所述无人机10的回收。After the charging
当需要再次起飞时,所述卡接件231缩进以解锁所述充电体122,所述无人机10可进行起飞并脱离所述第二磁铁1222的吸附作用,并将所述充电体122收回,从而完成所述无人机10的再次起飞。When it needs to take off again, the
在本实施方式中,所述卡接件231可由动力结构驱动,从而实现自动伸出或者缩进,无需人工操作。In this embodiment, the
本发明的无人机回收系统,能够自动完成对所述无人机10的充电,也能够自动完成对所述无人机10的回收,方便操作。The UAV recycling system of the present invention can automatically complete the charging of the
如图7所示,本发明还提供了一种无人机10回收方法,应用于如上述所述的无人机回收系统,包括以下步骤:As shown in FIG. 7 , the present invention also provides a method for recycling the
步骤A:如图8的状态所示,当所述无人机10需要充电时,所述无人机控制器向所述无人机10发送回收指令,并修订定位装置的向上偏移定位信息(必须超过所述壳体21开口211,保证所述无人机10不会与所述壳体21撞击),将修订后的定位信息发送给所述无人机10,使所述无人机10朝所述定位装置方向飞行,所述无人机10飞行至修订后的定位信息位置处,此时所述无人机10处于所述壳体21的开口211范围内,所述卡接件231未伸入所述卡槽215内;Step A: As shown in the state of FIG. 8 , when the
步骤B:所述无人机10飞行至所述无人机回收站20的开口211范围内,此时所述无人机10仍处于飞行状态,所述回收控制器驱使所述驱动装置运行并带动所述充电体122下降(如图9所示),所述牵引线缆123向下展开,使得所述充电体122能够随着重力方向并沿着所述无人机回收站20的内侧壁滑动(如图10所示),所述壳体21为漏斗结构,使得所述充电体122的滑落能够稳定平缓;Step B: The
步骤C:如图11所示,所述充电体122滑动至所述无人机回收站20的底部,所述第一磁铁1222和所述第二磁铁214吸附固定所述充电体122和所述无人机回收站20,所述第一电极1221与所述第二电极212相贴合电性导通,从而外部的供电电源能够对所述无人机10进行充电,而且所述无人机10可一边飞行一边充电,当需要再次执行飞行任务,所述驱动装置运行将所述充电体122上升收回,即可向飞行目的地飞行,该过程快速便捷,无需人工操作。Step C: As shown in FIG. 11 , the charging
进一步地,如图12和13所示,本发明的无人机10回收方法还包括步骤D:所述卡接件231穿过所述卡槽215抵住所述充电体122的上端面,以限制所述充电体122的活动范围,所述无人机10向下飞行降落至所述无人机回收站20中,从而完成所述无人机10的回收。Further, as shown in FIGS. 12 and 13 , the method for recovering the
本发明的无人机回收系统及其回收方法,通过设置无人机10和无人机回收站20,无人机主体11电性连接有可升降充电装置,并由驱动装置驱动充电体122上升或下降,同时无人机回收站20包括上端开口的壳体21,充电体122设置有第一电极1221和第一磁铁1222,壳体21设置有第二电极212、定位装置和第二磁铁214,当无人机10朝着定位装置方向飞行至壳体21开口211的范围内,驱动装置运行并带动充电体122下降至壳体21的底部内,此时第一磁铁1222和第二磁铁214磁吸固定,第一电极1221和第二电极212贴合连通以对无人机10进行充电,如果无人机10需要再次执行任务时,驱动装置运行带动充电体122上升收回即可,如果无人机10需要回收时,无人机10下降至壳体21内即可,使得本发明的无人机10能够自动与无人机回收站20精准对接以进行充电,同时能够及时解除充电状态以快速进行再次飞行任务,也能回收至无人机回收站20内。In the UAV recycling system and its recycling method of the present invention, by setting the
本发明的上述实施例仅仅是为清楚地说明本发明所作的举例,而并非是对本发明的实施方式的限定。对于所属领域的普通技术人员来说,在上述说明的基础上还可以做出其它不同形式的变化或变动。这里无法对所有的实施方式予以穷举。凡是属于本发明的技术方案所引伸出的显而易见的变化或变动仍处于本发明的保护范围之列。The above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention. For those of ordinary skill in the art, changes or modifications in other different forms can also be made on the basis of the above description. Not all implementations can be exhaustive here. Any obvious changes or changes derived from the technical solutions of the present invention are still within the protection scope of the present invention.
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CN112277682A (en) * | 2020-09-14 | 2021-01-29 | 广东顺德电力设计院有限公司 | Belt-off type unmanned aerial vehicle charging system |
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