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    FULLY-PROTECTED UNMANNED AERIAL VEHICLE
    271.
    发明公开
    FULLY-PROTECTED UNMANNED AERIAL VEHICLE 审中-公开
    充分保护的无人驾驶航空器

    公开(公告)号：EP3241758A1

    公开(公告)日：2017-11-08

    申请号：EP15875205.5

    申请日：2015-12-29

    Applicant: Beijing Zero Zero Infinity Technology Co. Ltd.

    Inventor： ZHANG, Tong ,  WANG, Mengqiu ,  WANG, Zhaozhe ,  ZHANG, Xuyang ,  ZHANG, Guanqun ,  GONG, Shuang ,  ZHANG, Yalin ,  WANG, Jinglong ,  LIU, Lixin

    IPC: B64D45/00 ,  B64C27/08

    CPC classification number: B64C27/006 ,  B64C1/30 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/201

    Abstract: A fully-protected unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and a rotor (2) connected to the unmanned aerial vehicle body (1), and further comprises a protection housing (3) connected to the unmanned aerial vehicle body (1). The protection housing (3) is a hollowed-out closed housing and has a hollow cavity (31), and the rotor (2) is installed in the hollow cavity (31). Because the rotor is installed in the hollow cavity of the protection housing, the rotor cannot make contact with a human body, so that the unmanned aerial vehicle can be released or reclaimed by an operator with the hand, and the operation portability and safety of the rotor are improved. The hollowed-out structure provides a forming space of lift for the rotor and normal flight of the unmanned aerial vehicle is ensured. The rotor is installed in the protection housing that is connected to the unmanned aerial vehicle body, so that the overall height of the unmanned aerial vehicle is reduced, and the portability of the unmanned aerial vehicle is further improved.

    Abstract translation: 一种全保护式无人飞行器，包括无人机体（1）和与无人机体（1）连接的转子（2），还包括与无人机体（1）连接的保护壳体（3） 1）。 保护壳体（3）为镂空封闭壳体，并具有空腔（31），转子（2）安装在空腔（31）中。 由于转子安装在保护壳体的空腔内，因此转子不会与人体接触，使得无人飞行器可以由操作者用手释放或回收，并且操作的便携性和安全性 转子得到改进。 镂空结构为转子提供了升力形成空间，保证了无人飞行器的正常飞行。 转子安装在与无人机相连的保护壳内，使无人机的整体高度降低，无人机的便携性进一步提高。

    FOLDABLE UNMANNED AERIAL VEHICLE
    272.
    发明公开
    FOLDABLE UNMANNED AERIAL VEHICLE 审中-公开
    可折叠的无人机空中车辆

    公开(公告)号：EP3241741A1

    公开(公告)日：2017-11-08

    申请号：EP15875204.8

    申请日：2015-12-29

    Applicant: Beijing Zero Zero Infinity Technology Co. Ltd.

    Inventor： ZHANG, Tong ,  WANG, Mengqiu ,  WANG, Zhaozhe ,  ZHANG, Xuyang ,  ZHANG, Guanqun ,  GONG, Shuang ,  ZHANG, Yalin ,  WANG, Jinglong ,  LIU, Lixin

    IPC: B64C3/56 ,  B64C27/08

    CPC classification number: B64C27/006 ,  B64C1/30 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/201

    Abstract: A foldable unmanned aerial vehicle for improving the portability of unmanned aerial vehicles comprises an unmanned aerial vehicle body (1) and a rotor portion connected to the unmanned aerial vehicle body (1). The rotor portion comprises a first rotor module (2) and a second rotor module (3) each having at least one rotor. The first rotor module and the second rotor module can be folded or unfolded by rotation around their own hinge shafts (4). According to the unmanned aerial vehicle, the rotor is designed in a modular manner: first, two rotor modules that can be folded or unfolded relatively are formed, and the folding and unfolding are implemented by the rotation of the rotor modules, so that the state of the unmanned aerial vehicle is changed, the folding and flying demands for the unmanned aerial vehicle are satisfied, and the portability of the unmanned aerial vehicle is improved; a flight path and a control module that the unmanned aerial vehicle needs can be arranged in the unmanned aerial vehicle body and do not need to be separately arranged in the rotor modules, so that the control reliability is improved.

    Abstract translation: 一种用于提高无人机便携性的可折叠无人飞行器，包括无人机（1）和与无人机体（1）连接的转子部分。 转子部分包括各自具有至少一个转子的第一转子模块（2）和第二转子模块（3）。 第一转子模块和第二转子模块可以通过围绕它们自己的铰链轴（4）旋转而折叠或展开。 根据无人机，转子以模块化方式设计：首先，形成两个可以相对折叠或展开的转子模块，通过转子模块的转动来实现折叠和展开，从而使得状态 改变了无人机的折叠飞行需求，提高了无人机的便携性; 无人机需要的飞行路径和控制模块可以设置在无人机体内，不需要单独设置在转子模块中，提高了控制的可靠性。

    SYSTEM AND METHOD FOR LAUNCHING AND LANDING UAVs
    277.
    发明公开
    SYSTEM AND METHOD FOR LAUNCHING AND LANDING UAVs 审中-公开
    系统和方法用于启动和土地无人弹箭

    公开(公告)号：EP2766260A1

    公开(公告)日：2014-08-20

    申请号：EP11874051.3

    申请日：2011-10-12

    Applicant: Saab AB

    Inventor： DANIELSSON, Torkel

    IPC: B64F1/02 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/084 ,  B64C2201/182 ,  B64C2201/201

    Abstract: The present invention relates to a system and method for automatic launch and landing UAVs (Unmanned Aerial Vehicles). The system comprises a ground station adapted for automatic UAV launching and landing. The ground station comprises: means for communication with UAVs present within a range from the ground station; an arrangement adapted for launching UAVs and for capturing in-flight UAVs, said arrangement having at least one controllable arm; a computing unit arranged to compute a meeting point between the at least one controllable arm and one in-flight UAV based on data communicated between the UAV and the ground station by means of said means for communication; and a control unit arranged to control the at least one arm to capture an in-flight UAV at the meeting point or to launch one UAV. The system is characterized in that the control unit is arranged to control the at least one arm to move a UAV between the meeting point and at least one storage position.

    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE
    280.
    发明公开
    SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE 有权
    VerstärktesRohr zum katapultieren von Drohnen

    公开(公告)号：EP2475578A2

    公开(公告)日：2012-07-18

    申请号：EP10833731.2

    申请日：2010-09-09

    Applicant: AeroVironment, Inc.

    Inventor： MIRALLES, Carlos Thomas ,  SU, Guan H. ,  ANDRYUKOV, Oleksandr ,  MCNEIL, John

    IPC: B64F1/04 ,  F41F3/04 ,  B64C13/20

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/201 ,  B64F1/06 ,  F41A21/02 ,  F41F1/00 ,  F41F3/042 ,  F42B39/14

    Abstract: An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).

    Abstract translation: 一种无人驾驶飞行器（UAV）发射管（100），其包括围绕右平行六面体孔（305）设置的至少一个预浸料衬底内层（370），至少一个围绕右侧设置的预浸料衬底（380）外层 平行六面体孔和设置在至少一层预浸料衬底（340）的内层与至少一层预浸料衬底（380）之间的一个或多个结构面板（341-344）。 一种无人驾驶飞行器（UAV）发射管（100），其包括被构造成与在内壁限定的发射器体内接合无人机的拴系的膛体（700,740），所述拴系的炮（700,740）的尺寸设置成在内部提供压力密封 并且其中所述系绳式突破（700,740）是中空的，具有朝向高压容积定向的开口端和连接在所述破坏物（700）的中空部（910）内的系绳（740），并且附接到 所述内壁保持高压容积或附接到所述内底壁（1013）。 包括通信节点（1500-1505）和发射器（1520）的系统，其包括处于预发射状态的无人驾驶飞行器（UAV），其被配置为接收并响应来自通信节点（1500-1505）的命令输入。

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