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    UNMANNED AERIAL VEHICLE
    176.
    发明申请
    UNMANNED AERIAL VEHICLE 审中-公开
    无人驾驶的航空机

    公开(公告)号：US20170036748A1

    公开(公告)日：2017-02-09

    申请号：US14858179

    申请日：2015-09-18

    Applicant: Lance Butler Plater

    Inventor： Lance Butler Plater

    IPC: B64C1/00 ,  B64C13/50 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/028 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2211/00 ,  B64D2221/00

    Abstract: An unmanned aerial vehicle (UAV) which in some embodiments may comprise a fuselage which includes a cavity formed by an interior cavity wall and a fuselage exterior wall, with the cavity disposed within the fuselage. A first electronic module may be electrically coupled to a first magnetic connector and a second electronic module may be electrically coupled to a second magnetic connector. Electronic communication between the first and second modules may be provided by contact between the first magnetic connector and the second magnetic connector. In further embodiments, when removably positioned adjacent to each other in the cavity, the first magnetic connector may contact the second magnetic connector to establish electronic communication between the first and second modules.

    Abstract translation: 一种无人飞行器（UAV），其在一些实施例中可包括机身，该机身包括由内腔壁和机身外壁形成的空腔，空腔设置在机身内。 第一电子模块可以电耦合到第一磁性连接器，并且第二电子模块可以电耦合到第二磁性连接器。 可以通过第一磁性连接器和第二磁性连接器之间的接触来提供第一和第二模块之间的电子通信。 在另外的实施例中，当可移除地定位在空腔中彼此相邻时，第一磁性连接器可以接触第二磁性连接器以在第一和第二模块之间建立电子通信。

    WINGED MULTI-ROTOR FLYING CRAFT WITH PAYLOAD ACCOMODATING SHIFTING STRUCTURE AND AUTOMATIC PAYLOAD DELIVERY
    177.
    发明申请
    WINGED MULTI-ROTOR FLYING CRAFT WITH PAYLOAD ACCOMODATING SHIFTING STRUCTURE AND AUTOMATIC PAYLOAD DELIVERY 审中-公开
    带多功能多功能转向架的移动式移动式起重机构和自动挂载式交付

    公开(公告)号：US20150284079A1

    公开(公告)日：2015-10-08

    申请号：US14583388

    申请日：2014-12-26

    Applicant: Hari Matsuda

    Inventor： Hari Matsuda

    IPC: B64C29/02 ,  G05D1/00 ,  B64C39/02

    CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141

    Abstract: A vertical takeoff/landing capable, multi-engine aircraft with an airfoil without elevator or rudder surfaces. Strut apertures are provided that accommodate vertical and horizontal translation of the airfoil in reference to engine supporting struts which are disposed through the apertures, opposite ends of the struts extending to opposite sides of the airfoil, wherein the struts are adjustably attached to the airfoil. A first and second plurality of engines are attached to ends of the struts, an attachment position of the plurality of engines to the struts is horizontally adjustable. A computerized engine controller, controls thrusts of the engines, to enable the aircraft to vertically lift off/land and re-orient itself to horizontally fly, and perform thrust-initiated elevator and rudder emulating flight. An external payload-to-delivery mating mechanism is attached to the bottom of the payload, which mates to a pole leading to the payload receptacle. Transceivers facilitate precise transfer of the payload.

    Abstract translation: 具有垂直起飞/着陆能力的多发飞机，具有无电梯或方向舵表面的翼型。 提供支撑孔，其适于引擎支撑支柱的翼型件的垂直和水平平移，所述发动机支撑支杆设置穿过所述孔，所述支柱的相对端延伸到所述翼型件的相对侧，其中所述支柱可调节地附接到所述翼型件。 第一和第二多个发动机附接到支柱的端部，多个发动机到支柱的附接位置是水平可调节的。 一台计算机化的发动机控制器控制发动机的推力，使飞机能够垂直地提升/降落，重新定位自身水平飞行，并执行推力启动的电梯和舵模拟飞行。 外部有效载荷与输送匹配机构连接到有效载荷的底部，其与连接到有效载荷的杆相配合。 收发器有助于精确传输有效载荷。

    Unmanned aircraft with failsafe system
    178.
    发明授权
    Unmanned aircraft with failsafe system 有权
    无人机与故障安全系统

    公开(公告)号：US09120579B2

    公开(公告)日：2015-09-01

    申请号：US14221126

    申请日：2014-03-20

    Applicant: Gatewing NV

    Inventor： Bjorn De Smet ,  Maarten De Moor ,  Peter Cosyn

    IPC: B64D31/06 ,  G05D1/06 ,  B64C39/00 ,  G05D1/00 ,  B64C11/00

    CPC classification number: B64D31/06 ,  B64C11/002 ,  B64C39/00 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/18 ,  G05D1/0055 ,  G05D1/0676

    Abstract: An unmanned aircraft configured to fall or crash in a controlled and safe manner. The unmanned aircraft includes a drive system to thrust the unmanned aircraft during a flight, and a reverse thrust system to reverse thrust the unmanned aircraft during a landing. The unmanned aircraft further includes a controller operationally coupled to the reverse thrust system, and a detector to detect and notify to the controller that the unmanned aircraft is in an uncontrolled situation during the flight. The controller is adapted to activate the reverse thrust system in order to reverse thrust the unmanned aircraft in-flight upon notification from the detector that the unmanned aircraft is in an uncontrolled situation.

    Abstract translation: 无人驾驶飞机配置为以受控和安全的方式坠落或碰撞。 无人驾驶飞机包括在飞行期间推动无人驾驶飞机的驱动系统，以及在着陆期间反向推动无人驾驶飞机的反向推力系统。 无人驾驶飞机还包括可操作地耦合到反向推力系统的控制器，以及检测器，用于检测并通知控制器，无人驾驶飞行器在飞行期间处于不受控制的情况。 控制器适于启动反向推力系统，以便在来自检测器的通知中无人驾驶飞机处于不受控制的情况下，使无人机在飞行中反向推进。

    Unmanned aerial vehicle and methods for controlling same
    179.
    发明授权
    Unmanned aerial vehicle and methods for controlling same 有权
    无人机及其控制方法

    公开(公告)号：US09075415B2

    公开(公告)日：2015-07-07

    申请号：US14204634

    申请日：2014-03-11

    Applicant: Airphrame, Inc.

    Inventor： Bret Kugelmass

    IPC: G05D1/10 ,  G06T11/60 ,  H04N7/18

    CPC classification number: H04Q9/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  G05D1/0088 ,  G05D1/0094 ,  G05D1/042 ,  G05D1/101 ,  G05D1/104 ,  G06T1/0014 ,  G06T11/206 ,  G06T11/60 ,  G08G5/0013 ,  G08G5/0039 ,  G08G5/0069 ,  H04N7/181 ,  H04Q2209/40 ,  H04W28/065

    Abstract: One variation of a method for imaging an area of interest includes: within a user interface, receiving a selection for a set of interest points on a digital map of a physical area and receiving a selection for a resolution of a geospatial map; identifying a ground area corresponding to the set of interest points for imaging during a mission; generating a flight path over the ground area for execution by an unmanned aerial vehicle during the mission; setting an altitude for the unmanned aerial vehicle along the flight path based on the selection for the resolution of the geospatial map and an optical system arranged within the unmanned aerial vehicle; setting a geospatial accuracy requirement for the mission based on the selection for the mission type; and assembling a set of images captured by the unmanned aerial vehicle during the mission into the geospatial map.

    Abstract translation: 用于对感兴趣区域成像的方法的一个变型包括：在用户界面内，接收对物理区域的数字地图上的一组感兴趣点的选择，并且接收对于地理空间地图的分辨率的选择; 在任务期间识别与所述一组感兴趣点成像成对应的地面区域; 在飞行任务期间通过无人驾驶飞行器在地面上产生飞行路线，以执行; 基于对地理空间地图的分辨率的选择和布置在无人机内的光学系统，设置沿着飞行路径的无人机的高度; 根据任务类型的选择，为任务确定地理空间精度要求; 并将任务期间由无人驾驶飞行器捕获的一组图像组装到地理空间图中。

    Modular miniature unmanned aircraft with vectored thrust control
    180.
    发明授权
    Modular miniature unmanned aircraft with vectored thrust control 有权
    具有矢量推力控制的模块化微型无人机

    公开(公告)号：US08991750B2

    公开(公告)日：2015-03-31

    申请号：US14274938

    申请日：2014-05-12

    Applicant: Aurora Flight Sciences Corporation

    Inventor： Adam Woodworth ,  Brandon Suarez

    IPC: B64C15/00 ,  B64C39/02 ,  B64C29/00

    CPC classification number: B64C15/00 ,  B64C29/0033 ,  B64C39/02 ,  B64C39/028 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/18 ,  B64C2201/187 ,  B64C2201/201 ,  B64C2211/00

    Abstract: An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust vectoring module and a second thrust vectoring module, and an electronics module. The electronics module provides commands to the two thrust vectoring modules. The two thrust vectoring modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as thrust vectoring modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.

    Abstract translation: 描述了一种无人驾驶飞机。 飞机包括机身，连接到机身后部的一对翅片，连接到机身底部的一对二面支架，第一推力矢量模块和第二推力矢量模块以及电子模块。 电子模块向两个推力矢量模块提供命令。 两个推力矢量模块被配置为通过直接控制飞行器的俯仰，滚动和偏航中的每一个的推力矢量来向飞行器提供侧向和纵向控制。 使用直接铰接的电动机作为推力矢量模块使飞机能够在宽范围的空速下执行紧半径的转弯。

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