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    INFLATABLE STRUCTURAL SUPPORT FOR PROPULSION AND CONTROL SYSTEMS OF UAVS (UNMANNED AERIAL VEHICLE)
    83.
    发明申请
    INFLATABLE STRUCTURAL SUPPORT FOR PROPULSION AND CONTROL SYSTEMS OF UAVS (UNMANNED AERIAL VEHICLE) 审中-公开
    无人机推进和控制系统的可燃结构支持（无人机）

    公开(公告)号：WO2015000088A1

    公开(公告)日：2015-01-08

    申请号：PCT/CH2014/000089

    申请日：2014-06-27

    Applicant: TAUSEL, Marco

    Inventor： TAUSEL, Marco

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64B2201/00 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/105 ,  B64C2201/108 ,  B64C2201/162 ,  B64C2201/203 ,  B64C2201/22

    Abstract: To improve overall performance and reduce the weight of an unmanned aerial vehicle (UAV) an inflatable structure was invented to directly support systems for propulsion and control system of the UAV. Independent claims have been implemented to obtain a relatively small radar footprint, methods to obtain a reduced visibility, methods to realize a hybrid power supply, methods for transporting the different components of the inflatable UAV.

    Abstract translation: 为了提高无人机（UAV）的整体性能和减轻重量，发明了一种充气结构，直接支持无人机的推进和控制系统。 已实施独立权利要求，以获得相对较小的雷达足迹，获得可见度降低的方法，实现混合动力供应的方法，运送可充气无人机的不同部件的方法。

    A MULTI-ROTOR AIRCRAFT
    84.
    发明申请
    A MULTI-ROTOR AIRCRAFT 审中-公开
    多转机飞机

    公开(公告)号：WO2014207732A1

    公开(公告)日：2014-12-31

    申请号：PCT/IB2014/062731

    申请日：2014-06-30

    Applicant: BELLEZZA QUATER, Paolo

    Inventor： BELLEZZA QUATER, Paolo

    IPC: B64C27/20 ,  B64B1/34 ,  B64C3/30 ,  B64C39/02 ,  B64B1/30

    CPC classification number: B64C39/024 ,  B64B1/34 ,  B64C3/30 ,  B64C27/20 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/105 ,  B64C2201/165

    Abstract: Described herein is a multi-rotor aircraft (10; 200) including: - a load-bearing structure (10A; 200A); and - a plurality of propulsion assemblies (M1, M2, M3, M4, M5, M6; M1', M2', M3', M4') each including a rotor (R1, R2, R3, R4, R5, R6; R1', R2', R3', R4'), which can be driven in rotation about a respective axis of rotation (X1, X2, X3, X4, X5, X6; X1', X2', X3', X4'), these propulsion assemblies being coupled to and supported by the load-bearing structure (10A; 200A), wherein the load-bearing structure (10A; 200A) is inflatable (C11, C12, C13, C14, C15, C16; C200).

    Abstract translation: 这里描述的是多转子飞机（10; 200），包括： - 承重结构（10A; 200A）; 每个包括转子（R1，R2，R3，R4，R5，R6; R1）的多个推进组件（M1，M2，M3，M4，M5，M6; M1'，M2'，M3'，M4' （X1，X2，X3，X4，X5，X6; X1'，X2'，X3'，X4'）相对旋转驱动， 这些推进组件联接到承载结构（10A; 200A）并由其承载，其中承载结构（10A; 200A）是可膨胀的（C11，C12，C13，C14，C15，C16; C200）。

    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM
    85.
    发明申请
    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM 审中-公开
    提供快速高空作战平台的系统

    公开(公告)号：WO2012099699A1

    公开(公告)日：2012-07-26

    申请号：PCT/US2011/068207

    申请日：2011-12-30

    Applicant: INFORMATION SYSTEMS LABORATORIES, INC.

    Inventor： VAN STAAGEN, Peter, K. ,  MCDANIEL, William, Douglas ,  BOSCHMA, James, H., Jr.

    IPC: B64F3/00

    CPC classification number: B64B1/50 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/14

    Abstract: A system and method for deploying a payload with an aerostat uses a mobile transporter for moving the system to a deployment site. Structurally, the system includes a base unit with a rotation head mounted thereon. An envelope container for holding a deflated aerostat is mounted on the rotation head and a rotation of the container on the rotation head positions the aerostat for optimal compliance with the existing wind condition. Also included in the system is an inflator that is mounted on the base unit to inflate the aerostat with a Helium gas. And, the system includes a tether control unit for maintaining a connection with the aerostat during its deployment, in-flight use, and recovery. Preferably, a deployment computer is used for a coordinated control of the rotation head, inflator and tether.

    Abstract translation: 用空气净化器部署有效载荷的系统和方法使用移动运输装置将系统移动到部署现场。 在结构上，该系统包括其上安装有旋转头的基座单元。 用于保持放气空气净化器的信封容器安装在旋转头上，并且旋转头上的容器的旋转定位了空气调节器，以最佳地符合现有的风况。 还包括在系统中的是充气机，其安装在基座单元上，以用氦气对空气净化器进行充气。 而且，该系统包括一个系绳控制单元，用于在其部署，飞行中使用和恢复期间维持与浮空器的连接。 优选地，部署计算机用于旋转头，充气机和系绳的协调控制。

    AERIAL VEHICLE AND METHOD OF FLIGHT
    86.
    发明申请
    AERIAL VEHICLE AND METHOD OF FLIGHT 审中-公开
    空中客车和飞行方法

    公开(公告)号：WO2011117619A2

    公开(公告)日：2011-09-29

    申请号：PCT/GB2011/050562

    申请日：2011-03-22

    Applicant: ATHENE WORKS LIMITED ,  DEAKIN, Nicholas James

    Inventor： DEAKIN, Nicholas James

    IPC: B64B1/62

    CPC classification number: B64B1/02 ,  B64B1/08 ,  B64B1/10 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/38 ,  B64B1/64 ,  B64B2201/00 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  H01Q1/36 ,  H01Q9/27

    Abstract: An aerial vehicle is described which comprises: a first compartment for holding a lighter than air gas; a second compartment for holding atmospheric air and having an inlet and an outlet; a solar panel for converting sunlight into electricity; a compressor for pumping atmospheric air through the inlet into the second compartment; control means for controlling the pitch and yaw of the vehicle; and a controller for controlling the buoyancy of the vehicle via the compressor and the outlet such that the vehicle is either lighter than the surrounding air and rising or heavier than the surrounding air and falling, and for controlling the control means such that the rising and falling motion includes a horizontal component. In another embodiment the solar panel is replaced by an engine and a fuel tank for storing fuel for the engine is also provided. The aerial vehicle can remain airborne for extended periods by using buoyancy propulsion. In the embodiments including a solar panel, a system including a light transmission station may be provided to supply energy to the solar panel from the light transmission station rather than relying on the incident sunlight alone. A method of flight using buoyancy propulsion is also described.

    Abstract translation: 描述了一种飞行器，其包括：用于保持比空气气体轻的第一隔室; 用于容纳大气并具有入口和出口的第二隔室; 用于将阳光转化为电的太阳能电池板; 用于将大气通过所述入口泵送到所述第二隔室中的压缩机; 用于控制车辆的俯仰和偏航的控制装置; 以及用于经由压缩机和出口控制车辆的浮力的控制器，使得车辆比周围空气要轻，并且比周围空气上升或者重，并且下降，并且用于控制控制装置使得上升和下降 运动包括水平分量。 在另一个实施例中，太阳能电池板被发动机代替，并且还提供了用于储存用于发动机的燃料的燃料箱。 航空器可以通过使用浮力推进长时间保持空中。 在包括太阳能电池板的实施例中，可以提供包括光传输站的系统，以从光传输站向太阳能电池板提供能量，而不是仅依赖于入射的太阳光。 还描述了使用浮力推进的飞行方法。

    HOVER ATTACHMENT FOR MOBILE DEVICE
    88.
    发明申请
    HOVER ATTACHMENT FOR MOBILE DEVICE 审中-公开

    公开(公告)号：US20180327070A1

    公开(公告)日：2018-11-15

    申请号：US15774246

    申请日：2016-03-24

    Applicant: Hossein RAHNAMA

    Inventor： Hossein RAHNAMA

    IPC: B64B1/40 ,  G05D1/00 ,  B64C39/02 ,  G06F3/147 ,  H04B1/3888

    CPC classification number: B64B1/40 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  G05D1/0094 ,  G06F3/147 ,  H04B1/3888 ,  H04M1/72527

    Abstract: According to embodiments described in the specification, a hover attachment includes a housing operable to receive a mobile device having a processor, a memory, and a display, at least one sensor operable to detect a position parameter of the mobile device relative to an object under tracking, and a regulator operable to maintain, responsive to the detecting, the mobile device in a hover relation to the object under tracking, wherein the display of the mobile device is a situational display. An exemplary method includes providing a situational display interface on a display of a mobile device mounted in a hover attachment, detecting a movement of an object under tracking in hover relation to the mobile device, and when the detected movement is associated with a position change function, controlling the hover attachment to maintain the hover relation between the mobile device and the object under tracking.

    FLYING ROBOT PROVIDED WITH PROJECTOR
    89.
    发明申请
    FLYING ROBOT PROVIDED WITH PROJECTOR 审中-公开

    公开(公告)号：US20180229828A1

    公开(公告)日：2018-08-16

    申请号：US15753162

    申请日：2015-08-19

    Applicant: (X-CONTROL SYSTEM CO., LTD.)

    Inventor： Fan YANG

    IPC: B64B1/06 ,  G09F19/18 ,  G09F21/06 ,  B64C39/02 ,  G03B29/00

    CPC classification number: B64B1/06 ,  B64B1/26 ,  B64B1/34 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/127 ,  G03B21/10 ,  G03B29/00 ,  G03B37/04 ,  G09F19/18 ,  G09F21/06

    Abstract: The present invention provides a flying robot (10) with projector, including a movable end (100) and a fixed end (200). A distributed working mode is used on the movable end (100) and the fixed end (200). The movable end (100) includes a top (110), a main body (120) and a bottom (130). The top (110) includes a lift system (112) and one or more proximity sensors (114); the main body (120) is a sealed hollow spherical body or spheroid body made of a film material capable of being used as a rear projection screen, and is filled with a gas of which the density is less than that of the air. The bottom (130) includes one or more rear projectors (131), a wireless communication module (132), a microcontroller (133), a battery (134), a direction and steering controlling device (135), a camera device (136), a sound capturing and reproduction device (137), a height sensor (138) and other sensors, etc. The fixed end (200) includes a wireless communication module (220), a control apparatus (240), a charging port (260), and other data interfaces, etc. The flying robot (10) with projector according to the present invention facilitates human-machine interaction and is suitable for being used in both indoor and outdoor environments.

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