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    Apparatus, Systems and Methods for Unmanned Aerial Vehicles
    71.
    发明申请
    Apparatus, Systems and Methods for Unmanned Aerial Vehicles 审中-公开
    无人机的装置，系统和方法

    公开(公告)号：US20160304217A1

    公开(公告)日：2016-10-20

    申请号：US15001232

    申请日：2016-01-19

    Applicant: Foundation Productions, LLC

    Inventor： James Mark Fisher ,  Bryan Jonathan Davis ,  Ronald Eugene Fisher

    IPC: B64F1/22 ,  G05D1/00 ,  B60L11/18 ,  B64C39/02

    CPC classification number: B64F1/222 ,  B60L53/00 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/18 ,  B64C2201/203 ,  G05D1/0011

    Abstract: The disclosed inventions include personal Unmanned Aerial Vehicles (UAV's) and UAV universal docking ports “docking ports” to be incorporated into and/or attached to headwear, including helmets, hard hats and hats and face masks, as well as footwear including boots and shoes, clothing and outerwear, devices, gear and equipment, land, air, water and space vehicles, buildings, wireless towers and other mobile or stationary objects and surfaces referred to collectively as “docking stations”. A docking station may have one or more docking ports for docking, networking and charging or refueling compact personal UAVs, and for providing data communications between said UAVs and other electronic devices that remain with the person while the UAV is in flight or driving or landed on terrain. Said docking ports may also incorporate wireless power transmission for remote wireless charging of one or more UAV's. Supplemental power for recharging said UAVs when docked may be supplied by integrated battery(s) in said docking port or me be provided directly from the docking station or other connected power source.

    Abstract translation: 所公开的发明包括个人无人驾驶飞行器（UAV）和UAV通用对接端口“对接端口”将被并入和/或连接到头饰，包括头盔，帽子和帽子和面罩，以及包括靴子和鞋子的鞋 服装和外衣，设备，齿轮和设备，陆地，空中，水和空间车辆，建筑物，无线电塔和其他被称为“对接站”的移动或固定物体和表面。 对接站可以具有一个或多个对接端口用于对接，联网和充电或加油紧凑的个人无人机，并且用于在UAV在飞行或驾驶或着陆时在所述UAV和与该人员之间留下的其他电子设备之间提供数据通信 地形。 所述对接端口还可以包括用于一个或多个无人机的远程无线充电的无线电力传输。 在停靠时对所述UAV进行再充电的补充功率可以由集成电池提供在所述对接端口中，或者直接从对接站或其他连接的电源提供。

    Morphing aircraft
    74.
    发明授权
    Morphing aircraft 有权
    变形飞机

    公开(公告)号：US08888035B2

    公开(公告)日：2014-11-18

    申请号：US13061019

    申请日：2009-08-25

    Applicant: Richard Charles Lind, Jr. ,  Daniel Thurmond Grant ,  David Eaton

    Inventor： Richard Charles Lind, Jr. ,  Daniel Thurmond Grant ,  David Eaton

    IPC: B64C39/02 ,  B64C37/00 ,  B60F3/00 ,  B64C1/00

    CPC classification number: B64C39/024 ,  B60F3/00 ,  B64C37/00 ,  B64C2001/0045 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/203

    Abstract: A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

    Abstract translation: 实现多模式位置和伪装用于有效载荷的变形飞机变形飞机包括基本上圆柱形的机身，其包括被配置为具有第一端和第二端的包装容器的形状。一组翼结合到机身。该组 的翼部包括第一位置，其中所述一组翼从机身向外延伸，并且第二位置，其中该组翼向内朝向机身A缩回。尾部联接到圆柱形机身的第二端。尾部包括第一位置 其中尾部从机身向外延伸，而第二位置则是尾部朝向机身向内缩进。螺旋桨安装在机身的第一端。发动机机械地联接到螺旋桨。发动机被封闭在机身内并且动力 螺旋桨

    UAV KIT
    75.
    发明申请
    UAV KIT 有权
    无人机套件

    公开(公告)号：US20140217242A1

    公开(公告)日：2014-08-07

    申请号：US14003406

    申请日：2012-03-26

    Applicant: Petter Muren ,  Trygve Frederik Marton ,  Geir Morten Mellem ,  Dag Henning Paulsen

    Inventor： Petter Muren ,  Trygve Frederik Marton ,  Geir Morten Mellem ,  Dag Henning Paulsen

    IPC: B64C39/02 ,  B64D47/08

    CPC classification number: B64C39/024 ,  A63H27/12 ,  B64C39/028 ,  B64C2201/024 ,  B64C2201/127 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2203/00 ,  B64D47/08

    Abstract: The embodiments herein disclose a personal UAV kit for storing, preparing and remote control of micro UAVs (40). The UAV kit includes a base unit (10), a control unit (30) and at least one UAV. The UAVs can typically be a winged aircraft with foldable wings or a helicopter with a two-bladed or foldable rotor. The base unit comprises UAV compartments for housing at least one UAV, bay (14) for storing the control unit, batteries and electronic components for charging, communication, control and processing and storing of data. In addition, the system includes an eye near display device for viewing system information and sensor data, typically live video, transmitted from the UAV.

    Abstract translation: 本文的实施方案公开了用于存储，准备和远程控制微型无人机（40）的个人UAV套件。 UAV套件包括基本单元（10），控制单元（30）和至少一个UAV。 无人机通常可以是具有可折叠翼的有翼飞机或具有双叶片或可折叠转子的直升机。 基座单元包括用于容纳至少一个UAV的UAV隔间，用于存储控制单元的舱（14），用于对数据进行充电，通信，控制和处理和存储的电池和电子组件。 此外，该系统包括用于观看系统信息的眼睛附近，以及从UAV发送的通常是实时视频的传感器数据。

    Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV)
    80.
    发明申请
    Autonomous, back-packable computer-controlled breakaway unmanned aerial vehicle (UAV) 失效
    自主的，可回填计算机控制的无人机（UAV）

    公开(公告)号：US20060091258A1

    公开(公告)日：2006-05-04

    申请号：US10976153

    申请日：2004-10-29

    Applicant: Tien Chiu ,  Jay Willmott

    Inventor： Tien Chiu ,  Jay Willmott

    IPC: B64C27/22

    CPC classification number: B64C1/00 ,  A45C5/00 ,  A45C13/02 ,  B64C1/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/165 ,  B64C2201/187 ,  B64C2201/201 ,  B64C2201/203

    Abstract: A modular unmanned aerial vehicle (UAV) having a fuselage, a nose cone, a left wing piece, a right wing piece, and a tail section. The tail section and nose cone each join to the fuselage through mating bulkhead structures that provide quick connection capability while being readily separated so as to enable the UAV to break apart at these connection points and thereby absorb or dissipate impact upon landing. The UAV is capable of rapid assembly in the field for two-man launch and data retrieval, as well as quick disassembly into these five component parts for transport and storage in a highly compact transport case that can be carried as a backpack.

    Abstract translation: 具有机身，鼻锥，左翼片，右翼片和尾部的模块化无人驾驶飞行器（UAV）。 尾部和鼻锥每个通过配合的隔板结构连接到机身，提供快速的连接能力，同时易于分离，以便使UAV在这些连接点处分裂，从而吸收或消散着陆时的冲击。 无人机能够在现场快速组装两人发射和数据检索，以及快速拆卸到这五个部件中，用于运输和存储，可以作为背包携带的高度紧凑的运输箱。

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