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    Method for replacing a signal controlling an actuator in a remote-controlled flying device with another signal
    52.
    发明申请
    Method for replacing a signal controlling an actuator in a remote-controlled flying device with another signal 审中-公开

    公开(公告)号：US20170371332A1

    公开(公告)日：2017-12-28

    申请号：US15698303

    申请日：2017-09-07

    Applicant: SkyCat Oy

    Inventor： Henri Hiisilä ,  Janne Laurinen

    IPC: G05D1/00 ,  B64C19/00 ,  B64C39/02 ,  G08C17/02 ,  A63H30/04 ,  A63H33/20 ,  B64D17/80

    CPC classification number: G05D1/0022 ,  A63H30/04 ,  A63H33/20 ,  B64C19/00 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/185 ,  B64D17/80 ,  G05D1/0055 ,  G08C17/02

    Abstract: The present invention relates to a method for replacing a signal controlling an actuator in a remote-controlled flying device with another signal. A flight controller supplies control signals to a safety device, and the signal to be replaced may be a signal to be transmitted by the safety device to a speed controller of at least one motor, or to a servo unit controlling the same, or the signal to be replaced may be a signal to be transmitted from the safety device to a servo unit controlling legs, a camera rack, a camera, a stabilizing system or an electric motor of the flying device. A replacement signal is a signal stored in a memory of the safety device. The replacement signal may be capable of controlling the speed controller directly or via the servo unit, in such a way that power transmission to said motor/motors is stopped or reduced, and this motor is/these motors are switched off or its/their rotation is decelerated, or the replacement signal may be capable of controlling said servo unit in such a way that said actuator is moved to a second position. The replacement signal may be a signal to be transmitted from a receiver past a flight controller, capable of controlling the speed controller or servo unit of the motor in such a way that power transmission to the motor is stopped or reduced, or to control said actuator in such a way that this actuator is moved to another position.

    UNINHABITED AIRBORNE VEHICLE AND METHOD OF CONTROLLING THE SAME
    54.
    发明申请
    UNINHABITED AIRBORNE VEHICLE AND METHOD OF CONTROLLING THE SAME 有权

    公开(公告)号：US20170152051A1

    公开(公告)日：2017-06-01

    申请号：US15065963

    申请日：2016-03-10

    Applicant: OPTiM Corporation

    Inventor： Shunji SUGAYA

    IPC: B64D25/00 ,  B64C39/02

    CPC classification number: B64D25/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/146 ,  B64C2201/185

    Abstract: The present invention is to prevent an uninhabited airborne vehicle from crashing due to fall impact and from being damaged and to protect an object and a living being at the fall point. The uninhabited airborne vehicle 100 includes a rotary wing 10 and a buffer 111 that reduces impact on the airframe when crashed. The battery charge remaining measurement module 122 and the distance measurement module 123 measure the battery charge remaining and the distance to an object, respectively, and compare the measurement with the respective thresholds. If the measurement is less than the respective thresholds, the buffer module 111 is driven by the drive module 121.

    AMPHIBIOUS VTOL SUPER DRONE CAMERA IN A MOBILE CASE (PHONE CASE) WITH MULTIPLE AERIAL AND AQUATIC FLIGHT MODES FOR CAPTURING PANORAMIC VIRTUAL REALITY VIEWS, SELFIE AND INTERACTIVE VIDEO
    56.
    发明申请
    AMPHIBIOUS VTOL SUPER DRONE CAMERA IN A MOBILE CASE (PHONE CASE) WITH MULTIPLE AERIAL AND AQUATIC FLIGHT MODES FOR CAPTURING PANORAMIC VIRTUAL REALITY VIEWS, SELFIE AND INTERACTIVE VIDEO 审中-公开
    大型垂直垂直超级摄像机，具有多种用于捕捉全景虚拟现实视野，美感和互动视频的多种航空和水上飞行模式的手机（电话箱）

    公开(公告)号：US20160286128A1

    公开(公告)日：2016-09-29

    申请号：US15172673

    申请日：2016-06-03

    Applicant: Dylan TX Zhou

    Inventor： Dylan TX Zhou

    IPC: H04N5/232 ,  H04N7/00 ,  B64C39/02 ,  H04N5/38

    CPC classification number: H04N5/23248 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/185 ,  B64D2211/00 ,  G06Q2220/00 ,  H04L65/1069 ,  H04L65/602 ,  H04L65/80 ,  H04N5/23238 ,  H04N5/38 ,  H04N7/00

    Abstract: A mobile case system comprising a real time broadcast stream recording; an unmanned aerial vehicle; a camera stabilization device; a camera movement device; one or more onboard cameras providing real-time first-person video and real-time first-person views and and 360-degree panoramic video recording used for virtual reality views and interactive video; a video transmitter and receiver device configured to perform high definition low latency real time video downlink; a one and two way telemetry device; a live broadcast device; a headset enabling real-time first-person video; a public database for viewing flight activity; software for licensing videos with a watermarked preview; software for autonomously extracting and compiling the usable video footage into a video montage synced to music; and onboard or separate software for stitching videos to form virtual reality views or interactive video, alternative embodiments the case may be adapted as power bank memory device, and use for aerial delivery.

    Abstract translation: 一种包括实时广播流记录的移动案例系统; 无人机; 相机稳定装置; 相机运动装置; 提供实时第一人称视频和实时第一人称视图的一个或多个车载摄像机和用于虚拟现实视图和交互式视频的360度全景视频记录; 配置为执行高清晰度低延迟实时视频下行链路的视频发射机和接收机设备; 一路双向遥测装置; 一个直播广播设备; 支持实时第一人称视频的耳机; 用于查看飞行活动的公共数据库; 使用水印预览授权视频的软件; 用于自动提取和编译可视频录像到同步到音乐的视频蒙太奇的软件; 以及用于拼接视频以形成虚拟现实视图或交互式视频的机载或单独的软件，该情况可以适用于电力银行存储器设备的替代实施例，并且用于空中传送。

    Remote controlled aerial reconnaissance vehicle
    58.
    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

    Applicant: Richard D. Adams

    Inventor： Richard D. Adams

    IPC: B64D9/00

    CPC classification number: B64D9/00 ,  B64C39/024 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/185 ,  B64C2201/203

    Abstract: 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.

    Abstract translation: 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。

    UNMANNED AERIAL VEHICLE SYSTEM
    59.
    发明申请
    UNMANNED AERIAL VEHICLE SYSTEM 审中-公开
    无人驾驶航空系统

    公开(公告)号：US20120043411A1

    公开(公告)日：2012-02-23

    申请号：US13149576

    申请日：2011-05-31

    Applicant: Peter Joseph Beck ,  Nikhil Raghu

    Inventor： Peter Joseph Beck ,  Nikhil Raghu

    IPC: F42B15/08 ,  F42B10/14 ,  H04N7/18 ,  B64D17/80

    CPC classification number: B64C39/024 ,  B64C2201/046 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/185 ,  B64C2201/201 ,  F41F3/042 ,  F41F3/045 ,  F42B15/08 ,  F42B15/10 ,  H04N7/183

    Abstract: A UAV includes: a rocket body, having a rocket motor and a payload section; a parachute coupled with the payload section; an image capture device; a magnetometer to provide a compass reference for images taken from the image capture device; and a transmitter to communicate image and compass data to a remote receiver. Compass bearings are overlaid on image data from the image capture device. A handheld launch unit includes an ignition system, having an activation mechanism and an igniter to activate the rocket motor. A safety pin prevents electrical current from flowing to the igniter until the pin is removed. An accelerometer and/or magnetometer determines an angular orientation of the UAV. Software verifies that the angle is within a user-defined safety limit before activating the igniter.

    Abstract translation: 无人机包括：具有火箭发动机和有效载荷部分的火箭主体; 与有效载荷部分相连的降落伞; 图像捕获装置; 磁力计，用于为从图像捕获装置拍摄的图像提供罗盘参考; 以及用于将图像和罗盘数据传送到远程接收器的发射器。 指南针轴承覆盖在图像捕获装置的图像数据上。 手持式发射单元包括具有启动机构和点火器来激活火箭发动机的点火系统。 一个安全销防止电流流到点火器，直到引脚被移除。 加速度计和/或磁力计确定无人机的角度取向。 激活点火器之前，软件将验证角度在用户定义的安全极限内。

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