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    SYSTEM FOR AUTOMATIC TAKEOFF AND LANDING BY INTERCEPTION OF SMALL UAVS
    31.
    发明申请
    SYSTEM FOR AUTOMATIC TAKEOFF AND LANDING BY INTERCEPTION OF SMALL UAVS 审中-公开
    通过拦截小型无人机进行自动起飞和着陆的系统

    公开(公告)号：US20150266575A1

    公开(公告)日：2015-09-24

    申请号：US14222158

    申请日：2014-03-21

    Applicant: Brandon Borko

    Inventor： Brandon Borko

    IPC: B64C39/02 ,  B64F1/12 ,  G05D1/10 ,  B64F1/02

    CPC classification number: B64C39/024 ,  B64C2201/024 ,  B64C2201/088 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/182 ,  B64C2201/20 ,  B64C2201/205 ,  B64F1/02 ,  B64F1/06 ,  B64F1/12 ,  B64F1/222 ,  G05D1/101

    Abstract: A system for facilitating automated landing and takeoff of an autonomous or pilot controlled hovering air vehicle with a cooperative underbody at a stationary or mobile landing place and an automated storage system used in conjunction with the landing and takeoff mechanism that stores and services a plurality of UAVs is described. The system is primarily characterized in that the landing mechanism is settable with 6 axes in roll, pitch, yaw, and x, y and z and becomes aligned with and intercepts the air vehicle in flight and decelerates the vehicle with respect to vehicle's inertial limits. The air vehicle and capture mechanism are provided with a transmitter and receiver to coordinate vehicle priority and distance and angles between landing mechanism and air vehicle. The landing and takeoff system has means of tracking the position and orientation of the UAV in real time. The landing mechanism will be substantially aligned to the base of the air vehicle. With small UAVs, their lifting capacity is limited. Reducing sensing and computation requirements by having the landing plate perform the precision adjustments for the landing operation allows for increased flight time and/or payload capacity.

    Abstract translation: 一种用于促进自主着陆和起飞的自动着陆和起飞的系统，其具有在固定或移动着陆地点的协作车身，以及与着陆和起飞机构结合使用的自动存储系统，其存储和服务多个UAV 被描述。 该系统的主要特征在于，着陆机构可设置为具有卷轴，俯仰，偏航以及x，y和z的6个轴线，并与飞行中的空中车辆对准并截取，并相对于车辆的惯性极限使车辆减速。 飞行器和捕获机构设置有发射器和接收器，以协调车辆优先级，着陆机构和机动车辆之间的距离和角度。 着陆和起飞系统具有实时跟踪无人机的位置和方向的方法。 着陆机构将基本上与机动车辆的底座对准。 对于小型无人机，起重能力有限。 通过使着陆板执行着陆操作的精确调整来减少感测和计算要求，可以增加飞行时间和/或有效载荷。

    HOVERING UNMANNED AERIAL VEHICLE
    32.
    发明申请
    HOVERING UNMANNED AERIAL VEHICLE 有权
    不顾一切的空中客车

    公开(公告)号：US20150259066A1

    公开(公告)日：2015-09-17

    申请号：US14436310

    申请日：2013-10-17

    Applicant: AERYON LABS INC.

    Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/20

    Abstract: In an aspect, an apparatus includes a hovering unmanned aerial vehicle (HUAV). The HUAV includes an arm assembly configured to support a propeller in such a way that propeller drag of the propeller is decoupled from yaw torque requirements associated with the hovering unmanned aerial vehicle. In another aspect, an apparatus includes an HUAV that has an arm assembly that is field-foldable relative to the HUAV between a flight-ready state and a folded state. In another aspect, an apparatus includes an HUAV having an arm assembly that is keyed in such a way as to facilitate field-assembly relative to the HUAV.

    Abstract translation: 一方面，一种装置包括悬停无人机（HUAV）。 HUAV包括臂组件，其构造成支撑螺旋桨，使螺旋桨的螺旋桨阻力与悬停的无人驾驶飞行器相关的偏航扭矩要求分离。 在另一方面，一种装置包括具有臂组件的HUAV，所述臂组件相对于在待飞状态和折叠状态之间的HUAV是可折叠的。 在另一方面，一种装置包括具有臂组件的HUAV，该臂组件以便于相对于HUAV的现场组装的方式键入。

    Self-enclosed air vehicle
    37.
    发明授权
    Self-enclosed air vehicle 有权

    公开(公告)号：US11655026B2

    公开(公告)日：2023-05-23

    申请号：US17379942

    申请日：2021-07-19

    Applicant: GoPro, Inc.

    Inventor： Ryan Michael Goldstein

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/203

    Abstract: 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.

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