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    Sustained over-the-horizon vertical takeoff and landing sensing system
    176.
    发明授权
    Sustained over-the-horizon vertical takeoff and landing sensing system 有权
    持续的超视距垂直起飞和着陆感测系统

    公开(公告)号：US08948928B2

    公开(公告)日：2015-02-03

    申请号：US13866489

    申请日：2013-04-19

    Applicant: Sikorsky Aircraft Corporation

    Inventor： Mark R. Alber ,  Timothy Fred Lauder ,  Jonathan Hartman ,  Bryan Clark Holasek

    IPC: B64C39/00 ,  B64C27/00 ,  B64C19/00 ,  B64C29/00 ,  B64C39/02 ,  B64D47/00

    CPC classification number: B64C19/00 ,  B64C29/00 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/123 ,  B64C2201/148 ,  B64D47/00

    Abstract: An electrically powered of the vertical takeoff and landing aircraft configured for use with a tether station having a continuous power source is provided including at least one rotor system. The vertical takeoff and landing aircraft additionally has an autonomous flight control system coupled to the continuous power source. The autonomous flight control system is configured to operate an electrical motor coupled to the at least one rotor system such that the vertical takeoff and landing aircraft continuously hovers above the tether station in a relative position. The vertical takeoff and landing aircraft also includes a detection system for detecting objects at a distance from the vertical takeoff and landing aircraft.

    Abstract translation: 提供了一种配置成与具有连续动力源的系绳站一起使用的垂直起飞和着陆飞机的电力供应器，其包括至少一个转子系统。 垂直起飞和着陆飞机还具有耦合到连续电源的自主飞行控制系统。 自主飞行控制系统被配置为操作耦合到至少一个转子系统的电动机，使得垂直起飞和着陆飞机在相对位置连续地悬挂在系绳站上方。 垂直起降飞机还包括一个检测系统，用于检测与垂直起飞和着陆飞机相距一定距离处的物体。

    UNMANNED AERIAL VEHICLE (UAV) WITH INTER-CONNECTING WING SECTIONS
    177.
    发明申请
    UNMANNED AERIAL VEHICLE (UAV) WITH INTER-CONNECTING WING SECTIONS 审中-公开
    无人机（UAV）具有相互连接的部分

    公开(公告)号：US20150014482A1

    公开(公告)日：2015-01-15

    申请号：US14330586

    申请日：2014-07-14

    Applicant: Design Intelligence Incorporated, LLC

    Inventor： Jacob R. Weierman ,  James L. Grimsley

    IPC: B64C3/54 ,  H01L31/042 ,  B64D43/00

    CPC classification number: H02S10/40 ,  B64C3/56 ,  B64C2201/021 ,  B64C2201/042 ,  B64D2211/00 ,  Y02T50/55

    Abstract: An unmanned aerial vehicle (UAV) is described. The UAV may include a fuselage assembly and a plurality of inter-connecting wing sections. The inter-connecting wing section may include a connecting assembly on opposing lateral ends. The connecting assembly may be complementary on opposing ends. The fuselage assembly may include a complementary set of the connecting assembly on opposing lateral ends. The complementary set of the connecting assembly may be configured to connect to at least two of the inter-connecting wing sections. At least a portion of the inter-connecting wing sections may include a solar array having solar panels.

    Abstract translation: 描述了无人机（UAV）。 UAV可以包括机身组件和多个相互连接的翼部分。 相互连接翼部分可以包括在相对的侧向端部上的连接组件。 连接组件可以在相对端部互补。 机身组件可以包括在相对的侧端上的连接组件的互补组。 连接组件的互补组可以被构造成连接到至少两个相互连接的翼部分。 相互连接的翼部的至少一部分可以包括具有太阳能电池板的太阳能阵列。

    DEEP STALL AIRCRAFT LANDING
    179.
    发明申请
    DEEP STALL AIRCRAFT LANDING 有权
    深空飞机着陆

    公开(公告)号：US20140343752A1

    公开(公告)日：2014-11-20

    申请号：US13261814

    申请日：2012-08-16

    Applicant: Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    Inventor： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    IPC: G08G5/02 ,  B64D31/00

    CPC classification number: G08G5/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/18 ,  B64D31/00 ,  G05D1/0011 ,  G05D1/0676

    Abstract: An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

    Abstract translation: 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。

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