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    AERIAL VEHICLE AND METHOD OF FLIGHT
    32.
    发明申请
    AERIAL VEHICLE AND METHOD OF FLIGHT 审中-公开
    空中客车和飞行方法

    公开(公告)号：WO2011117619A3

    公开(公告)日：2011-11-17

    申请号：PCT/GB2011050562

    申请日：2011-03-22

    Applicant: ATHENE WORKS LTD ,  DEAKIN NICHOLAS JAMES

    Inventor： DEAKIN NICHOLAS JAMES

    IPC: B64B1/00

    CPC classification number: B64B1/02 ,  B64B1/08 ,  B64B1/10 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/38 ,  B64B1/64 ,  B64B2201/00 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  H01Q1/36 ,  H01Q9/27

    Abstract: An aerial vehicle is described which comprises: a first compartment (13) for holding a lighter than air gas; a second compartment (6, 4) for holding atmospheric air and having an inlet and an outlet; a solar panel (41) for converting sunlight into electricity; a compressor (242) for pumping atmospheric air through the inlet into the second compartment; control means (1,3) for controlling the pitch and yaw of the vehicle; and a controller (209) for controlling the buoyancy of the vehicle via the compressor and the outlet such that the vehicle is either lighter than the surrounding air and rising or heavier than the surrounding air and falling, and for controlling the control means such that the rising and falling motion includes a horizontal component. In another embodiment the solar panel is replaced by an engine and a fuel tank for storing fuel for the engine is also provided. The aerial vehicle can remain airborne for extended periods by using buoyancy propulsion. In the embodiments including a solar panel, a system including a light transmission station may be provided to supply energy to the solar panel from the light transmission station rather than relying on the incident sunlight alone. A method of flight using buoyancy propulsion is also described.

    Abstract translation: 描述了一种飞行器，其包括：用于保持比气体气体轻的第一隔室（13）; 用于保持大气空气并具有入口和出口的第二隔间（6,4）; 用于将太阳光转换成电的太阳能电池板（41） 压缩机（242），用于将大气通过所述入口排入所述第二隔室; 控制装置（1,3），用于控制车辆的俯仰和偏航; 以及用于经由压缩机和出口控制车辆的浮力的控制器（209），使得车辆比周围空气要轻，并且比周围空气上升或者重，并且为了控制控制装置， 上升和下降运动包括水平分量。 在另一个实施例中，太阳能电池板被发动机代替，并且还提供了用于储存用于发动机的燃料的燃料箱。 航空器可以通过使用浮力推进长时间保持空中。 在包括太阳能电池板的实施例中，可以提供包括光传输站的系统，以从光传输站向太阳能电池板提供能量，而不是仅依赖于入射的太阳光。 还描述了使用浮力推进的飞行方法。

    Combined submersible vessel and unmanned aerial vehicle
    38.
    发明授权
    Combined submersible vessel and unmanned aerial vehicle 有权
    组合潜艇和无人机

    公开(公告)号：US09296270B2

    公开(公告)日：2016-03-29

    申请号：US13765144

    申请日：2013-02-12

    Applicant: Aurora Flight Sciences Corporation

    Inventor： Robert Parks ,  Adam Woodworth ,  Tom Vaneck ,  Justin McClellan

    IPC: B60F5/02 ,  B64C39/02 ,  F42B15/20

    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。

    AERIAL VEHICLE AND METHOD OF FLIGHT
    39.
    发明申请
    AERIAL VEHICLE AND METHOD OF FLIGHT 有权
    空中客车和飞行方法

    公开(公告)号：US20140339356A1

    公开(公告)日：2014-11-20

    申请号：US14324306

    申请日：2014-07-07

    Applicant: Athene Works Limited

    Inventor： Nicholas James DEAKIN

    IPC: B64B1/02 ,  B64B1/64

    CPC classification number: B64B1/02 ,  B64B1/08 ,  B64B1/10 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/38 ,  B64B1/64 ,  B64B2201/00 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  H01Q1/36 ,  H01Q9/27

    Abstract: An aerial vehicle comprises an elongate envelope within which are at least one first compartment for holding a lighter than air gas and at least one second compartment for holding atmospheric air and said at least one second compartment having an inlet and an outlet and at least one pair of wings extending laterally from the envelope; said wings being planar units with a leading and trailing edge, the width of the wings from their leading edges to their trailing edges being substantially less than the length of the envelope with airfoil portions fitted between the leading and trailing edges of the wing: the top and bottom of the wings are mirror images of one another; in which forward motion of the vehicle is obtainable without trust through alternate diving and climbing motion.

    Abstract translation: 一种空中飞行器包括一个细长的外壳，其中至少有一个用于保持比空气气体轻的第一隔间和至少一个用于保持大气空气的第二隔室，并且所述至少一个第二隔室具有入口和出口以及至少一对 的翼从信封横向延伸; 所述翼是具有前缘和后缘的平面单元，翼从其前缘到其后缘的宽度基本上小于具有机翼部分装配在翼的前缘和后缘之间的封套的长度：顶部 翅膀的底部是彼此的镜像; 其中车辆的向前运动通过交替的潜水和爬坡运动而不被信任地获得。

    Unmanned air vehicles and method of landing same
    40.
    发明授权
    Unmanned air vehicles and method of landing same 有权
    无人驾驶飞行器和降落方法相同

    公开(公告)号：US08123162B2

    公开(公告)日：2012-02-28

    申请号：US11098529

    申请日：2005-04-05

    Applicant: Omri Sirkis

    Inventor： Omri Sirkis

    IPC: B64C25/56 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/167 ,  B64C2201/187

    Abstract: There is provided an Unmanned Air Vehicle (UAV) including an engine and an airframe, including means for performing a deep stall maneuver at least one inflatable sleeve connected or connectable to the airframe, and means for inflating the sleeve during flight, wherein the inflated sleeve extends along the lower side of the airframe so as to protect same during deep stall landing. A method for operating an Unmanned Air Vehicle (UAV), including an engine and an airframe is also provided.

    Abstract translation: 提供了包括发动机和机身的无人机（UAV），包括用于对连接或可连接到机身的至少一个充气套筒进行深度失速操纵的装置，以及用于在飞行期间使套筒充气的装置，其中，所述膨胀套筒 沿着机身的下侧延伸，以便在深度失速着陆期间保护它们。 还提供了一种用于操作无人机（UAV）的方法，包括发动机和机身。

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