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71 条记录 (耗时 0.022 秒)

    Unmanned airborne reconnaissance system
    22.
    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

    申请人： Beverly Cox ,  Hampton Dews ,  Nicholas Nyroth

    发明人： Beverly Cox ,  Hampton Dews ,  Nicholas Nyroth

    IPC分类号： B64C13/20 ,  B64C13/00

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

    摘要： 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.

    Self-enclosed air vehicle
    24.
    发明授权
    Self-enclosed air vehicle 有权

    公开(公告)号：US10011354B2

    公开(公告)日：2018-07-03

    申请号：US14973466

    申请日：2015-12-17

    申请人： GoPro, Inc.

    发明人： Ryan Michael Goldstein

    IPC分类号： B64C39/02

    CPC分类号： B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/203

    摘要： Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.

    UNMANNED AERIAL VEHICLE
    27.
    发明申请
    UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶的航空机

    公开(公告)号：US20170029101A1

    公开(公告)日：2017-02-02

    申请号：US15192438

    申请日：2016-06-24

    申请人： Riderless Technologies Inc.

    发明人： STEFAN WEISSENBERG

    IPC分类号： B64C27/20 ,  G05D1/00 ,  B64D9/00 ,  B64D47/08 ,  B64C27/08 ,  B64C39/02

    CPC分类号： B64C39/024 ,  B64C27/006 ,  B64C2201/027 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/203

    摘要： There is provided an unmanned aerial vehicle (UAV) with a flexible propeller guard. The flexible propeller guard may allow the UAV to be resiliently repelled from objects in the UAV's flight path, thereby protecting one or more of the UAV's propellers. The UAV may have foldable arms, movable between a deployed configuration and a stored configuration, and the flexible propeller guard may be used to restrain the folded arms in the stored configuration. The flexible propeller guard may be arranged so as to not interfere with the foldability of the arms.

    摘要翻译： 提供了一种带有柔性螺旋桨护罩的无人驾驶飞行器（UAV）。 灵活的螺旋桨防护装置可以允许UAV从无人机飞行路径内的物体弹性地排斥，从而保护一个或多个无人机的螺旋桨。 UAV可以具有在展开构型和存储构型之间可移动的可折叠臂，并且柔性螺旋桨防护件可用于限制存储构型中的折叠臂。 柔性螺旋桨护罩可以布置成不干扰臂的可折叠性。

    Remote controlled aerial reconnaissance vehicle
    28.
    发明授权
    Remote controlled aerial reconnaissance vehicle 有权
    遥控空中侦察车

    公开(公告)号：US09033281B1

    公开(公告)日：2015-05-19

    申请号：US13410225

    申请日：2012-03-01

    申请人： Richard D. Adams

    发明人： Richard D. Adams

    IPC分类号： B64D9/00

    CPC分类号： B64D9/00 ,  B64C39/024 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/185 ,  B64C2201/203

    摘要： A radio controlled UAV is disclosed. The UAV includes a parachute, with a cylindrical power and control module suspended vertically below the parachute. In one embodiment, a propulsion source is mounted on top of the power and control module with control lines connected to the module below the propulsion source, and in another embodiment the power and control module is suspended from a point above a propulsion source. The UAV is controlled by radio controls from a hand held controller, with actuators retracting and letting out control lines attached to the parachute in order to control direction of the parachute. The UAV may be launched from a tube using a pressurized tank with a nozzle expelling gas from the tank, the tank and nozzle towing a canister from which the UAV is deployed.

    摘要翻译： 公开了一种无线电控制的无人机。 无人机包括一个降落伞，一个圆柱形的电源和控制模块垂直悬挂在降落伞下方。 在一个实施例中，推进源安装在功率和控制模块的顶部，其控制线连接到推进源下方的模块，并且在另一个实施例中，功率和控制模块从推进源上方的点悬挂。 无人机由手持控制器的无线电控制控制，执行器缩回并释放连接到降落伞的控制线，以控制降落伞的方向。 无人机可以使用加压罐从管中发射，喷嘴排出来自罐，罐和喷嘴的气体，其牵引无人机从其部署的罐。

    MORPHING AIRCRAFT
    30.
    发明申请
    MORPHING AIRCRAFT 有权
    MORPHING飞机

    公开(公告)号：US20110155840A1

    公开(公告)日：2011-06-30

    申请号：US13061019

    申请日：2009-08-25

    申请人： Richard Charles Lind, JR. ,  Daniel Thurmond Grant ,  David Eaton

    发明人： Richard Charles Lind, JR. ,  Daniel Thurmond Grant ,  David Eaton

    IPC分类号： B64C39/02 ,  B64C13/24 ,  B64C3/56 ,  B64C5/12 ,  B64C5/06 ,  B64C11/00 ,  G09F3/00 ,  B64C27/04 ,  B64C27/50

    CPC分类号： B64C39/024 ,  B60F3/00 ,  B64C37/00 ,  B64C2001/0045 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/203

    摘要： A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

    摘要翻译： 实现多模式位置和伪装用于有效载荷的变形飞机变形飞机包括基本上圆柱形的机身，其包括被配置为具有第一端和第二端的包装容器的形状。一组翼结合到机身。该组 的翼部包括第一位置，其中所述一组翼从机身向外延伸，并且第二位置，其中该组翼向内朝向机身A缩回。尾部联接到圆柱形机身的第二端。尾部包括第一位置 其中尾部从机身向外延伸，而第二位置则是尾部朝向机身向内缩进。螺旋桨安装在机身的第一端。发动机机械地联接到螺旋桨。发动机被封闭在机身内并且动力 螺旋桨