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    COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE
    3.
    发明申请
    COMBINED SUBMERSIBLE VESSEL AND UNMANNED AERIAL VEHICLE 有权
    组合的不合格船只和无人驾驶的航空器

    公开(公告)号：US20150375586A1

    公开(公告)日：2015-12-31

    申请号：US14851453

    申请日：2015-09-11

    Applicant: Aurora Flight Sciences Corporation

    Inventor： ROBERT PARKS ,  ADAM WOODWORTH ,  TOM VANECK ,  JUSTIN MCCLELLAN

    IPC: B60F5/02 ,  B64C39/02 ,  B63G8/08

    CPC classification number: B64C37/00 ,  B60F5/02 ,  B63G8/001 ,  B63G8/08 ,  B63G2008/005 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  F42B15/20

    Abstract: A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment.

    Abstract translation: 组合潜艇和无人驾驶飞行器优选地包括主体结构，至少一个翼结构，至少一个垂直稳定器结构和至少一个水平稳定器结构。 推进系统联接到车身结构并且被构造成在空中飞行和水下操作中推进飞行潜艇。 优选地，推进系统包括电动机，耦合到电动机并被配置为接收由电动机产生的电力并提供可变输出功率的变速箱;耦合到齿轮箱并被配置为传递由变速箱提供的可变输出功率的驱动轴， 以及联接到所述驱动轴并被配置为接受从所述驱动轴传递到其的动力的螺旋桨。 螺旋桨进一步构造成在空中环境和水下环境中旋转和推进飞行潜艇。

    TETHERED AERIAL SYSTEMS FOR DATA GATHERING
    6.
    发明申请
    TETHERED AERIAL SYSTEMS FOR DATA GATHERING 审中-公开
    数据采集​​的专用系统

    公开(公告)号：US20160144958A1

    公开(公告)日：2016-05-26

    申请号：US14280992

    申请日：2014-05-19

    Applicant: AURORA FLIGHT SCIENCES CORPORATION

    Inventor： ADAM WOODWORTH ,  JAMES PEVERILL

    IPC: B64C39/02 ,  B64F3/02 ,  B64C27/00 ,  B64C27/20 ,  B64C9/00 ,  B64C25/58

    CPC classification number: B64C39/022 ,  B64C9/00 ,  B64C25/58 ,  B64C27/006 ,  B64C27/20 ,  B64C37/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/143 ,  B64C2201/148 ,  B64D17/80 ,  B64F3/02 ,  G05D1/0866 ,  G05D1/104 ,  H02G11/00

    Abstract: A tethered unmanned aerial vehicle (“UAV”) may be outfitted with a sensor payload for data gathering. The tethered UAV may be tethered to a ground station for constricting the flight space of the UAV while also providing the option for power delivery and/or bidirectional communications. The tethered UAV's flight path may be extended by introducing one or more secondary UAVs that cooperate to extend the horizontal flight path of a primary UAV. The ground station, which may be coupled with the tethered aerial vehicle, may comprise a listening switch configured to determine a condition of the tether such that the supply of power to the tether may be terminated when tether damage or a tether severance is detected.

    Abstract translation: 系绳无人机（“UAV”）可以装备有用于数据采集的传感器有效载荷。 系缚的UAV可以被绑在地面站上，用于收缩无人机的飞行空间，同时还提供功率传送和/或双向通信的选项。 可以通过引入一个或多个辅助UAV以扩展主UAV的水平飞行路径来扩展系留的UAV的飞行路径。 可以与系留式航空器耦合的地面站可以包括侦听开关，其被配置为确定系绳的状况，使得当检测到系绳损伤或系绳断开时，可以终止对系绳的供电。

    MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED THRUST CONTROL
    8.
    发明申请
    MODULAR MINIATURE UNMANNED AIRCRAFT WITH VECTORED THRUST CONTROL 有权
    具有显着控制的模块化MINIATURE UNMANNED飞机

    公开(公告)号：US20140284429A1

    公开(公告)日：2014-09-25

    申请号：US14274938

    申请日：2014-05-12

    Applicant: Aurora Flight Sciences Corporation

    Inventor： ADAM WOODWORTH ,  Brandon Suarez

    IPC: B64C15/00 ,  B64C39/02

    CPC classification number: B64C15/00 ,  B64C29/0033 ,  B64C39/02 ,  B64C39/028 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/18 ,  B64C2201/187 ,  B64C2201/201 ,  B64C2211/00

    Abstract: An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust vectoring module and a second thrust vectoring module, and an electronics module. The electronics module provides commands to the two thrust vectoring modules. The two thrust vectoring modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as thrust vectoring modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

    Abstract translation: 描述了一种无人驾驶飞机。 飞机包括机身，连接到机身后部的一对翅片，连接到机身底部的一对二面支架，第一推力矢量模块和第二推力矢量模块以及电子模块。 电子模块向两个推力矢量模块提供命令。 两个推力矢量模块被配置为通过直接控制飞行器的俯仰，滚动和偏航中的每一个的推力矢量来向飞行器提供侧向和纵向控制。 使用直接铰接的电动机作为推力矢量模块使飞机能够在宽范围的空速下执行紧半径的转弯。

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