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    Unmanned airborne reconnaissance system
    47.
    发明授权
    Unmanned airborne reconnaissance system 有权

    公开(公告)号：US07014141B2

    公开(公告)日：2006-03-21

    申请号：US10194814

    申请日：2002-07-12

    Applicant: Beverly Cox ,  Hampton Dews ,  Nicholas Nyroth

    Inventor： Beverly Cox ,  Hampton Dews ,  Nicholas Nyroth

    IPC: B64C13/20 ,  B64C13/00

    CPC classification number: F41G3/02 ,  B64C39/024 ,  B64C2201/044 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/185 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06 ,  Y02T50/82

    Abstract: An unmanned airborne reconnaissance system, the unmanned airborne reconnaissance system including a lightweight, portable, powered aircraft and a foldable launch rail, the aircraft, in a broken down condition and the launch rail in a broken down condition fitable inside a box, the box capable of being carried by one man. The launch system includes an elongated launch rail with the carriage assembly, and a propulsion means for accelerating the carriage assembly from one end of the launch rail to the other. The carriage assembly releasably engages the aircraft so as to propel the aircraft from one end of the launch rail to the other. The propulsion may be by a cartridge that explodes and releases a gas through a cylinder, or by elastic cords. The aircraft is guided through the air either by a programmed onboard computer which controls the control surfaces of the aircraft and/or by remote control. The aircraft typically contains a camera for recording and transmitting images received from the ground below.

    PROGRAMMABLE WRIST DEVICE FOR MAKING AERIAL VIDEOS AND PHOTOS
    48.
    发明申请
    PROGRAMMABLE WRIST DEVICE FOR MAKING AERIAL VIDEOS AND PHOTOS 审中-公开
    用于制作视频和照片的可编程手写设备

    公开(公告)号：WO2016170416A1

    公开(公告)日：2016-10-27

    申请号：PCT/IB2016/000509

    申请日：2016-04-22

    Applicant: CERIOLI, Mattia

    Inventor： CERIOLI, Mattia

    IPC: G03B17/02 ,  B64C39/02 ,  G03B15/00 ,  G03B17/06 ,  G03B17/56

    CPC classification number: G03B15/006 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/127 ,  B64C2201/203 ,  G03B17/02 ,  G03B17/561

    Abstract: A wrist programmable device (1) for making aerial videos and photos, comprising a watch strap (2) and a watch case body (4) removably coupled to said watch strap (2), said watch case body (4) having a bottom and a dial, at least videocamera means (T), hover means (13-14) for allowing said watch case body (4) to hover while separating from said watch strap (2), and programmable electronic means adapted to operatively control said at least videocamera means (T) and said hovering means (13-14).

    Abstract translation: 一种用于制造航空视频和照片的手腕可编程设备（1），包括手表带（2）和可拆卸地联接到所述表带（2）的表壳体（4），所述表壳主体（4）具有底部和 至少摄像机装置（T），用于允许所述表壳主体（4）在与所述表带（2）分离的同时悬停的悬挂装置（13-14）;以及可编程电子装置，其适于可操作地控制所述至少 视频摄像机装置（T）和所述盘旋装置（13-14）。

    UAV KIT
    49.
    发明申请
    UAV KIT 审中-公开
    无人机套件

    公开(公告)号：WO2012130790A3

    公开(公告)日：2013-01-03

    申请号：PCT/EP2012055298

    申请日：2012-03-26

    Applicant: PROX DYNAMICS AS ,  MUREN PETTER

    Inventor： MUREN PETTER

    IPC: B64C39/02 ,  A63H27/10

    CPC classification number: B64C39/024 ,  A63H27/12 ,  B64C39/028 ,  B64C2201/024 ,  B64C2201/127 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2203/00 ,  B64D47/08

    Abstract: The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs (40). The UAV kit includes a base unit (10), a control unit (30) and at least one UAV. The UAVs can typically be a winged aircraft with foldable wings or a helicopter with a two-bladed or foldable rotor. The base unit comprises UAV compartments for housing at least one UAV, bay (14) for storing the control unit, batteries and electronic components for charging, communication, control and processing and storing of data. In addition, the system includes an eye near display device for viewing system information and sensor data, typically live video, transmitted from the UAV.

    Abstract translation: 本文的实施方案公开了用于存储，准备和远程控制微型无人机（40）的个人UAV套件。 UAV套件包括基本单元（10），控制单元（30）和至少一个UAV。 无人机通常可以是具有可折叠翼的有翼飞机或具有双叶片或可折叠转子的直升机。 基座单元包括用于容纳至少一个UAV的UAV隔间，用于存储控制单元的舱（14），用于对数据进行充电，通信，控制和处理和存储的电池和电子组件。 此外，该系统包括用于观看系统信息的眼睛附近，以及从UAV发送的通常是实时视频的传感器数据。

    UNMANNED AERIAL SURVEILLANCE DEVICE
    50.
    发明申请
    UNMANNED AERIAL SURVEILLANCE DEVICE 审中-公开
    不定期的空中监视装置

    公开(公告)号：WO2007084186A2

    公开(公告)日：2007-07-26

    申请号：PCT/US2006/032105

    申请日：2006-08-17

    Applicant: CHANG INDUSTRY, INC. ,  DE LA TORRE, Samuel

    Inventor： DE LA TORRE, Samuel

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/102 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/201 ,  B64C2201/203

    Abstract: An aerial surveillance device is provided, comprising an image capturing device capable of being supported by an airframe structure above the ground. The airframe structure includes a body portion defining a longitudinal axis and configured to support the image-capturing device. A tail portion having control surfaces is operably engaged with the body portion along the axis. Transversely-extending wing portions are directly engaged with the body portion. Each wing portion is defined by longitudinally-opposed spars extending from a spaced-apart disposition at the body portion to a common connection distally from the body portion. The spars have a fabric extending therebetween to provide a wing surface. A support member extends along an aerodynamic center, transversely to the body portion, of each wing portion, to tension and rigidify the wing portions so as to provide a positive camber for the wing portions and to form an airfoil.

    Abstract translation: 提供了一种空中监视装置，其包括能够由地面上方的机身结构支撑的图像捕获装置。 机身结构包括限定纵向轴线并构造成支撑图像捕获装置的主体部分。 具有控制表面的尾部部分沿着轴线与主体部分可操作地接合。 横向延伸的翼部直接与主体部分接合。 每个翼部分由纵向相对的翼梁限定，该翼梁从主体部分处的间隔布置延伸到远离主体部分的公共连接。 翼梁具有在其间延伸的织物以提供机翼表面。 支撑构件沿每个翼部横向于主体部分的空气动力学中心延伸，以张紧和刚化翼部，以便为翼部提供正弧形并形成翼型。

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