TRANSPORTABLE GROUND STATION FOR AN UNMANNED AERIAL VEHICLE
    23.
    发明公开
    TRANSPORTABLE GROUND STATION FOR AN UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶飞机的可移动地面站

    公开(公告)号:EP3201088A1

    公开(公告)日:2017-08-09

    申请号:EP15847916.2

    申请日:2015-09-24

    Inventor: STREETT, Andrew

    Abstract: A transportable ground station for a UAV includes a container in which the UAV may be transported and housed. The container includes a wireless or contact-based recharging station that recharges the UAV's batteries or other power sources after the UAV returns from a mission. The recharging station may be directly or indirectly connected to one or more solar panels that generate energy to power the recharging station. The ground station may be deployed virtually anywhere, from any vehicle (e.g., plane, train, boat, truck, etc.), and may operate over an extended period of time without human intervention.

    Abstract translation: 用于无人飞行器的可移动地面站包括其中可以运输和容纳无人飞行器的容器。 该集装箱包括无线或基于接触的充电站,在无人机返回任务后,该无线充电站可为无人机的电池或其他电源充电。 再充电站可以直接或间接地连接到一个或多个太阳能电池板,这些太阳能电池板产生能量以给再充电站供电。 地面站几乎可以从任何车辆(例如飞机,火车,船,卡车等)的任何地方部署,并且可以在延长的时间段内运行而无需人工干预。

    SYSTEMS AND METHODS FOR AERODYNAMIC DEPLOYMENT OF WING STRUCTURES

    公开(公告)号:US20200079492A1

    公开(公告)日:2020-03-12

    申请号:US16128432

    申请日:2018-09-11

    Abstract: A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.

    Power cell casing
    26.
    发明授权

    公开(公告)号:US10158104B1

    公开(公告)日:2018-12-18

    申请号:US15657059

    申请日:2017-07-21

    Abstract: A casing for a battery assembly may include a first casing portion having a first base portion and a pair of first leg portions extending generally perpendicularly to the first base portion. At least one of the first leg portions may have a flared end. The casing may further include a second casing portion with a second base portion and a pair of second leg portions extending generally perpendicularly to the second base portion. At least one of the second leg portions may have a flat end. The casing portions are attached at a joint including the flat end attached to the flared end. In some embodiments, a battery assembly may include at least one power cell and a casing including a first casing portion and a second casing portion attached together at a joint. The joint may be under tension. The casing applies pressure to the power cell.

    SYSTEMS AND METHODS FOR AERODYNAMIC DEPLOYMENT OF WING STRUCTURES

    公开(公告)号:US20240116624A1

    公开(公告)日:2024-04-11

    申请号:US18484394

    申请日:2023-10-10

    CPC classification number: B64C3/56 B64C9/00 B64C39/024 B64C2009/005 B64U10/25

    Abstract: A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.

    ROBOTIC FOREARMS
    30.
    发明申请
    ROBOTIC FOREARMS 审中-公开

    公开(公告)号:US20200009746A1

    公开(公告)日:2020-01-09

    申请号:US16027157

    申请日:2018-07-03

    Inventor: Joseph YOUNG

    Abstract: Joints for facilitating relative motion between a first part of a machine, such as a robot, and a second part of the machine may include linear actuators connecting the first part to the second part and a shaft member connecting the first part to the second part. Each of the linear actuators may be oriented at an oblique angle relative to the shaft member. The first and second parts of the machine may be parts of a robotic arm, such as other robotic joints or an end-effector, such as a robotic hand. The joints may facilitate simulation of the movement and dexterity of human body parts, such as a human wrist and forearm.

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