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    UNMANNED AERIAL VEHICLE
    132.
    发明申请
    UNMANNED AERIAL VEHICLE 有权
    无人驾驶的航空机

    公开(公告)号：US20140217229A1

    公开(公告)日：2014-08-07

    申请号：US14347375

    申请日：2012-09-14

    Applicant: Keen Ian Chan

    Inventor： Keen Ian Chan

    IPC: B64C29/02 ,  A63H27/00 ,  B64C13/24 ,  B64F5/00 ,  B64C39/02 ,  B64C27/08

    CPC classification number: B64C29/02 ,  A63H27/12 ,  B64C13/24 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/165 ,  G05D1/0669 ,  Y10T29/49826

    Abstract: An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method for assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises a wing structure comprising elongated equal first and second wings; a support structure comprising first and second sections coupled to a middle position of the wing structure and extending in opposite directions perpendicular to the wing structure; and four propellers, each mounted to a respective one of the first and second wings, and first and second sections, for powering the UAV during both vertical and horizontal flight modes.

    Abstract translation: 能够进行垂直和水平飞行模式的无人飞行器（UAV），组装无人机的方法和用于组装无人机的一套零件。 无人机包括翼结构，其包括细长的相等的第一和第二翼; 支撑结构，包括联接到所述机翼结构的中间位置并且在与所述机翼结构垂直的相反方向上延伸的第一和第二部分; 以及四个螺旋桨，每个螺旋桨安装到第一和第二翼中的相应一个以及第一和第二部分，用于在垂直和水平飞行模式期间为无人机提供动力。

    Aircraft
    136.
    发明授权
    Aircraft 有权
    飞机

    公开(公告)号：US08434710B2

    公开(公告)日：2013-05-07

    申请号：US12740005

    申请日：2008-11-20

    Applicant: Inderpal Singh Hothi ,  Jon Robert Stoackley ,  Steven John Stoackley

    Inventor： Inderpal Singh Hothi ,  Jon Robert Stoackley ,  Steven John Stoackley

    IPC: B64C27/22

    CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088

    Abstract: An unmanned aerial vehicle (UAV) in the form of a “tail sitter” flying wing adapted for vertical take off and landing and transitions between flight as a helicopter and wing-borne flight. The vehicle is electrically powered from onboard batteries and equipped with rotors on miniature helicopter rotor heads at the tips of the wing for both lift, during take off and landing, and forward thrust. In planform the wing comprises, to each side of its longitudinal axis, an inner section with swept back leading and trailing edges, and an outer section with a leading edge more perpendicular to the longitudinal axis, being only mildly swept back or substantially unswept, and a swept forward trailing edge.

    Abstract translation: 一种无人机（UAV），以“尾巴”飞翼的形式适用于垂直起飞和着陆，并且作为直升机和机翼飞行之间的飞行之间的过渡。 车辆由车载电池供电，并在机翼顶部的微型直升机转子头上配备转子，用于升降机，起飞和着陆期间以及向前推力。 在平面图中，翼片在其纵向轴线的每一侧包括具有扫掠的前缘和后缘的内部部分，并且具有更垂直于纵向轴线的前缘的外部部分仅被轻度地扫掠或基本上不被刮除，以及 前沿后缘。

    ANNULAR AIRBORNE VEHICLE
    138.
    发明申请
    ANNULAR AIRBORNE VEHICLE 有权

    公开(公告)号：US20120256043A1

    公开(公告)日：2012-10-11

    申请号：US13466343

    申请日：2012-05-08

    Applicant: Harry George Dennis Gosling

    Inventor： Harry George Dennis Gosling

    IPC: B64C9/14 ,  B64C39/06

    CPC classification number: B64C39/062 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/162

    Abstract: An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is open at both ends. A propulsion system is provided comprising one or more pairs of propulsion devices, each pair comprising a first propulsion device mounted to the wing-body and positioned on a first side of a plane including the wing-body axis, and a second propulsion device mounted to the wing-body and positioned on a second side of the plane including the wing-body axis.

    Abstract translation: 一种机载车辆，其具有限定翼体轴线的翼体，并且当沿翼体轴线观察时呈现大致环形，所述环形空间的内部限定在两端敞开的管道。 提供了包括一对或多对推进装置的推进系统，每对推进装置包括安装到翼体上并定位在包括翼体轴线的平面的第一侧上的第一推进装置，以及安装到 翼体并且定位在包括翼体轴线的平面的第二侧上。

    Vibration isolation devices and associated systems and methods
    139.
    发明授权
    Vibration isolation devices and associated systems and methods 有权

    公开(公告)号：US08226039B2

    公开(公告)日：2012-07-24

    申请号：US13347624

    申请日：2012-01-10

    Applicant: Andreas H. von Flotow ,  Tyler Patrick Horton

    Inventor： Andreas H. von Flotow ,  Tyler Patrick Horton

    IPC: B64C1/00

    CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/127 ,  B64C2201/165

    Abstract: Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include a fuselage having a first fuselage section and a second fuselage section adjacent to and at least approximately longitudinally aligned with the first fuselage section. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.

    Methods and apparatus for transforming unmanned aerial vehicle
    140.
    发明授权
    Methods and apparatus for transforming unmanned aerial vehicle 有权
    无人驾驶飞行器转换方法及装置

    公开(公告)号：US08157203B2

    公开(公告)日：2012-04-17

    申请号：US12262747

    申请日：2008-10-31

    Applicant: Lloyd E. Kinsey ,  Patrick Kranking

    Inventor： Lloyd E. Kinsey ,  Patrick Kranking

    IPC: B64C27/22

    CPC classification number: B64C39/024 ,  B64C29/02 ,  B64C2201/028 ,  B64C2201/084 ,  B64C2201/088

    Abstract: Methods and apparatus for a transforming aerial vehicle according to various aspects of the present invention may operate in conjunction with a launch system configured to rotate the aerial vehicle about its longitudinal axis. A lifting surface pivotally connected to the aerial vehicle may be positioned such that the rotation of the aerial vehicle causes the lifting surface to generate a lifting force on the aerial vehicle. This lift causes the aerial vehicle to rise gyroscopically before the lifting surface is rotated to a second position such that the aerial vehicle transforms from a gyroscopic mode to a fixed-wing aerial vehicle. The lifting surface may then be rotated again to allow the aerial vehicle to land as an auto gyro.

    Abstract translation: 根据本发明的各个方面的用于变换航空器的方法和装置可以与被配置为围绕其纵向轴线旋转飞行器的发射系统一起操作。 枢转地连接到飞行器的提升表面可以被定位成使得飞行器的旋转导致提升表面在飞行器上产生提升力。 该升降机使得飞行器在提升表面旋转到第二位置之前陀螺地升高，使得飞行器从陀螺仪模式转换为固定翼型飞行器。 然后可以再次旋转提升表面，以允许飞行器作为自动陀螺仪着陆。

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