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    SYSTEM AND METHOD FOR ENHANCING DISTRIBUTION LOGISTICS AND INCREASING SURVEILLANCE RANGES WITH UNMANNED AERIAL VEHICLES AND A DOCK NETWORK
    71.
    发明申请
    SYSTEM AND METHOD FOR ENHANCING DISTRIBUTION LOGISTICS AND INCREASING SURVEILLANCE RANGES WITH UNMANNED AERIAL VEHICLES AND A DOCK NETWORK 审中-公开
    用于增强分配物流的系统和方法，并增加与无人机动车和锁网的监控范围

    公开(公告)号：US20160185466A1

    公开(公告)日：2016-06-30

    申请号：US14818329

    申请日：2015-08-05

    Applicant: Frank Dreano, JR.

    Inventor： Frank Dreano, JR.

    IPC: B64F1/32 ,  G06Q30/06 ,  G06Q10/08 ,  B64C39/02

    CPC classification number: G06Q10/083 ,  A47G29/141 ,  B64C2201/06 ,  B64C2201/128 ,  B64C2201/20 ,  B64C2201/201 ,  G06Q30/0635 ,  H04W84/005

    Abstract: A system and method for enhancing distribution logistics and surveillance ranges with unmanned aerial vehicles (UAV) and at least one dock in a dock network. The UAV remains in communication with the dock for enhancing distribution logistics of at least one package and increasing the range of surveillance for the unmanned aerial vehicle. From the dock, the UAV delivers the package to a destination point, obtains the package from a pick up point, recharges the unmanned aerial vehicle throughout the network of docks, and increases the range of distribution and surveillance. A logistics software controls the delivery and surveillance. A wireless communication device enables communication between the UAV and the dock. Light indicators indicate status of the package and the operational status of the UAV. A camera captures an image of the package in the dock. A motion detector detects the UAV for regulating access for loading/unloading and docking.

    Abstract translation: 一种用于通过无人机（UAV）加强配送物流和监控范围的系统和方法，以及至少在码头网络中的一个码头。 无人机与码头保持通信，以加强至少一个包裹的配送物流，并增加对无人驾驶飞行器的监视范围。 从码头，无人机将包裹运送到目的地，从接送点获取包裹，在无人驾驶飞机的整个网络网络中充电，并增加了分配和监视的范围。 物流软件控制交货和监控。 无线通信设备实现无人机与码头之间的通信。 光指示灯指示包的状态和无人机的操作状态。 摄像机捕获码头中包装的图像。 运动检测器检测无人机用于调节进出货和对接的通道。

    SHORT TAKEOFF AND LANDING AIRCRAFT
    73.
    发明申请
    SHORT TAKEOFF AND LANDING AIRCRAFT 有权
    短途起飞和着陆飞机

    公开(公告)号：US20150183522A1

    公开(公告)日：2015-07-02

    申请号：US14231003

    申请日：2014-03-31

    Applicant: The Boeing Company

    Inventor： Rich P. Ouellette

    IPC: B64D41/00 ,  B64D27/24

    CPC classification number: B64D41/00 ,  B64C2201/06 ,  B64C2201/08 ,  B64D27/24 ,  B64D2027/026 ,  B64F1/04 ,  B64F3/02 ,  Y10S903/902

    Abstract: Short takeoff and landing aircraft are disclosed. An example fixed wing aircraft includes a primary powertrain to provide power to a propulsion unit, a secondary powertrain to provide power to the propulsion unit, and a detachable power coupling to transfer power to the secondary powertrain from a source external to the fixed wing aircraft during takeoff.

    Abstract translation: 公开了起飞和着陆飞机。 示例性固定翼飞机包括用于向推进单元提供动力的主动力系，用于向推进单元提供动力的次级动力系，以及可拆卸动力联接，以从固定翼飞机外部的源将动力传递到次级动力系 脱掉。

    UNMANNED AERIAL VEHICLE BATTERY AND UNMANNED AERIAL VEHICLE
    75.
    发明公开
    UNMANNED AERIAL VEHICLE BATTERY AND UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：EP3244468A4

    公开(公告)日：2017-12-13

    申请号：EP16863190

    申请日：2016-10-25

    Applicant: AUTEL ROBOTICS CO LTD

    Inventor： QIU LONGXUE ,  WU XINGWEN

    IPC: H01M2/10 ,  B64C39/02

    CPC classification number: H01M2/1083 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/06 ,  H01M2220/20

    Abstract: The present invention discloses an unmanned aerial vehicle and a battery thereof. The battery includes a battery body and a shell disposed on one end of the battery body. The shell has a clamp button disposed on the side opposite the unmanned aerial vehicle. One end of the clamp button is fixed on the shell and the other is used for detachably connecting with the unmanned aerial vehicle. The clamp button makes the battery detachably connect with the main body of the unmanned aerial vehicle be possible and it is very convenient for changing the battery.

    Power management method and system for an unmanned air vehicle
    78.
    发明公开
    Power management method and system for an unmanned air vehicle 审中-公开
    Leistungsverwaltungsverfahren und Systemfürein unbemanntes Luftfahrzeug

    公开(公告)号：EP2853494A1

    公开(公告)日：2015-04-01

    申请号：EP13382370.8

    申请日：2013-09-26

    Applicant: The Boeing Company

    Inventor： Lemus Martin, Jose Luis ,  Pereira Mayán, Sergio ,  Ferreyra, Eduardo Gabriel

    IPC: B64D41/00 ,  H02J1/14 ,  H02J3/12

    CPC classification number: B64C39/024 ,  B64C2201/06 ,  B64C2201/141 ,  B64D31/14 ,  B64D41/00 ,  B64D2041/005 ,  B64D2211/00 ,  B64D2221/00 ,  G05B13/0275 ,  G05D1/0005 ,  Y02T90/36

    Abstract: Power management method and system for an unmanned air vehicle, wherein the unmanned air vehicle comprises a plurality of power demanding subsystems and a plurality of power sources. The invention establishes mission oriented fixed parameters. A fuzzy logic power management unit, comprised in the system, automatically calculates and assigns priorities for delivering power to the subsystems. It also automatically calculates and assigns amounts of power delivered to each subsystem and automatically decides which of the power sources to deliver power to which subsystem. The fuzzy logic power management system calculates and assigns the priorities and loads in function of a plurality of internal variables, external variables and the mission oriented fixed parameters.

    Abstract translation: 一种用于无人驾驶飞行器的电力管理方法和系统，其中所述无人驾驶飞行器包括多个功率要求较高的子系统和多个电源。 本发明建立了面向任务的固定参数。 包括在系统中的模糊逻辑电源管理单元自动计算和分配用于向子系统传送电力的优先级。 它还自动计算和分配交付给每个子系统的功率量，并自动决定哪个电源向哪个子系统提供电力。 模糊逻辑电源管理系统根据多个内部变量，外部变量和面向任务的固定参数来计算和分配优先级和负载。

    Autonomous solar aircraft
    79.
    发明公开
    Autonomous solar aircraft 有权
    自主太阳能电池

    公开(公告)号：EP2660151A1

    公开(公告)日：2013-11-06

    申请号：EP13166020.1

    申请日：2013-04-30

    Applicant: Sunlight Photonics Inc.

    Inventor： Frolov, Sergey V. ,  Cyrus, Michael ,  Bruce, Allan J.

    IPC: B64C31/036

    CPC classification number: B64C39/024 ,  B64C2201/02 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/165 ,  B64D27/24 ,  B64D2211/00 ,  H01L31/048 ,  H02S20/00 ,  Y02E10/50 ,  Y02T50/64

    Abstract: An unmanned solar-powered aircraft (300) comprises a lightweight solar wing (310) comprising an airfoil profile, a top surface, a bottom surface, a leading edge, a trailing edge, wing tips, and at least one photovoltaic cell, wherein the surfaces and edges follow an arched bow shape across a span of the wing. The unmanned solar-powered aircraft includes a fuselage (330) and a propeller (340), wherein the fuselage is placed below the solar wing and contains an electric motor, battery, and electronics.

    Abstract translation: 无人太阳能飞机（300）包括轻型太阳能翼（310），其包括翼型轮廓，顶表面，底表面，前缘，后缘，翼尖和至少一个光伏电池，其中， 表面和边缘沿着机翼跨度的弓形弓形。 无人太阳能飞机包括机身（330）和螺旋桨（340），其中机身放置在太阳能飞轮下方并且包含电动机，电池和电子设备。

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