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    HOVERING UNMANNED AERIAL VEHICLE
    241.
    发明申请
    HOVERING UNMANNED AERIAL VEHICLE 有权
    不顾一切的空中客车

    公开(公告)号：US20150259066A1

    公开(公告)日：2015-09-17

    申请号：US14436310

    申请日：2013-10-17

    Applicant: AERYON LABS INC.

    Inventor： Glen Johannesson ,  David Kroetsch ,  Michael Peasgood ,  Stephen Marchetti

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/165 ,  B64C2201/20

    Abstract: In an aspect, an apparatus includes a hovering unmanned aerial vehicle (HUAV). The HUAV includes an arm assembly configured to support a propeller in such a way that propeller drag of the propeller is decoupled from yaw torque requirements associated with the hovering unmanned aerial vehicle. In another aspect, an apparatus includes an HUAV that has an arm assembly that is field-foldable relative to the HUAV between a flight-ready state and a folded state. In another aspect, an apparatus includes an HUAV having an arm assembly that is keyed in such a way as to facilitate field-assembly relative to the HUAV.

    Abstract translation: 一方面，一种装置包括悬停无人机（HUAV）。 HUAV包括臂组件，其构造成支撑螺旋桨，使螺旋桨的螺旋桨阻力与悬停的无人驾驶飞行器相关的偏航扭矩要求分离。 在另一方面，一种装置包括具有臂组件的HUAV，所述臂组件相对于在待飞状态和折叠状态之间的HUAV是可折叠的。 在另一方面，一种装置包括具有臂组件的HUAV，该臂组件以便于相对于HUAV的现场组装的方式键入。

    Landing Pad For Unmanned Aerial Vehicle Delivery
    242.
    发明申请
    Landing Pad For Unmanned Aerial Vehicle Delivery 审中-公开
    无人机搭载的着陆垫

    公开(公告)号：US20150183528A1

    公开(公告)日：2015-07-02

    申请号：US14587828

    申请日：2014-12-31

    Applicant: Ryan Walsh ,  Alex J. Falesch

    Inventor： Ryan Walsh ,  Alex J. Falesch

    IPC: B64F1/32 ,  A01M29/16 ,  B64C39/02 ,  B64F1/36 ,  G05D1/02

    CPC classification number: B64F1/32 ,  A01M29/16 ,  A47G29/14 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/128 ,  B64C2201/145 ,  B64F1/04 ,  G05D1/0202

    Abstract: A landing pad receives and stores packages delivered from an aerial vehicle are awaiting pickup from an aerial vehicle. The landing pad can be placed outside of a window and can contain a transmitter for sending out an identification signal via radio frequency to aid aerial vehicles in finding the landing pad. The landing pad contains a landing platform with a trapdoor that leads to a storage compartment. The trapdoor can be configured to only open when it receives a signal from an authorized aerial vehicle. The storage compartment can be accessed via a storage compartment door which can contain a locking mechanism. The storage compartment can be climate controlled. The landing pad can also have a transmitter that emits sounds to discourage animals from nesting on or near the landing pad. The landing pad can also include a solar power generator as a source of electrical energy.

    Abstract translation: 登陆垫接收和存储从空中飞行器传送的包裹正在​​等待从飞行器拾取。 着陆垫可以放置在窗户之外，并且可以包含用于通过射频发送识别信号的发射器，以帮助航空器找到着陆垫。 着陆垫包含一个着陆平台，带有通向存储隔间的活门。 陷板门可以配置为仅在从授权的飞行器接收到信号时打开。 可以通过可以容纳锁定机构的储藏室门访问储藏室。 储藏室可以进行气候控制。 登陆垫还可以具有发射声音的发射器，以阻止动物在着陆垫上或附近嵌套。 着陆垫还可以包括作为电能源的太阳能发电机。

    FLOATING MOBILE OBJECT AND FLOATING MOBILE SYSTEM USING THE SAME
    246.
    发明申请
    FLOATING MOBILE OBJECT AND FLOATING MOBILE SYSTEM USING THE SAME 有权
    浮动移动对象和浮动移动系统使用它

    公开(公告)号：US20150108282A1

    公开(公告)日：2015-04-23

    申请号：US14385506

    申请日：2013-02-14

    Applicant: The Ritsumeikan Trust

    Inventor： Katsuya Kanaoka

    IPC: B64C15/12 ,  B64C39/02

    CPC classification number: B64C15/12 ,  B63B2035/008 ,  B63H25/04 ,  B63H25/46 ,  B63H2025/465 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/10 ,  B64C2201/146 ,  G05D1/10 ,  G05D1/102

    Abstract: A holonomic floating mobile object is operated under gravity and includes a main body and six or more thrusters for generating thrust by changing the momentum of a fluid. The six or more thrusters are controlled independently of one another such that the thrust is set at a desired value. The six or more thrusters are arranged in a fuselage coordinate system defined on the main body, such that the range in which a total thrust vector obtained by combining vectors of the thrust generated by all of the thrusters can be generated spans a six-dimensional space with three directions of translation and three directions of rotation. Incoming and outgoing flows to and from one of the thrusters are spaced apart from incoming and outgoing flows to and from the other thrusters and even apart from every other fuselage structure aside from that one thruster.

    Abstract translation: 完整的浮动移动物体在重力作用下运行，包括主体和六个或更多个用于通过改变流体动量产生推力的推进器。 六个或更多个推进器彼此独立地控制，使得推力被设定在期望的值。 六个或更多个推进器被布置在限定在主体上的机身坐标系中，使得可以产生通过组合由所有推进器产生的推力的矢量而获得的总推力向量的范围跨越六维空间 具有三个方向的翻译和三个方向的旋转。 来往于其中一个推进器的进出流量与进入和离开其它推进器的进出流量间隔开，甚至除了一个推进器之外的每个其他机身结构。

    Aerial photogrammetry and aerial photogrammetric system
    249.
    发明授权
    Aerial photogrammetry and aerial photogrammetric system 有权
    空中摄影测量和航空摄影测量系统

    公开(公告)号：US08953933B2

    公开(公告)日：2015-02-10

    申请号：US14059784

    申请日：2013-10-22

    Applicant: Kabushiki Kaisha TOPCON

    Inventor： Fumio Ohtomo ,  Hitoshi Otani ,  Kazuki Osaragi ,  Tetsuji Anai

    IPC: G03B39/00 ,  G01C11/00 ,  G01C11/02

    CPC classification number: G01C11/00 ,  A01B79/005 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/127 ,  G01C11/025 ,  G05D1/0094 ,  G05D1/104

    Abstract: Aerial photogrammetry is provided by using two or more flying vehicles, each equipped with a GPS device and an image pickup unit. This method comprises setting up two or more photographing points and setting up a photographing point area, respectively, with each of the photographing points as the center, measuring a position of the flying vehicle by the GPS device, a step where each of the flying vehicle reaches each corresponding photographing point area and maintains the position of the photographing point area, acquiring a time when the flying vehicle finally reaches the photographing point area, setting up a shutter timing time after a predetermined time from the moment when the flying vehicle has finally reached the photographing point area, and taking aerial photographs by the two or more flying vehicles at the shutter timing time.

    Abstract translation: 通过使用两个或更多个飞行器，每个配备有GPS装置和图像拾取单元来提供空中摄影测量。 该方法包括以每个拍摄点为中心分别设置两个或更多个拍摄点和设置拍摄点区域，通过GPS装置测量飞行器的位置，其中每个飞行器 到达每个对应的拍摄点区域并保持拍摄点区域的位置，获取飞行时间最终到达拍摄点区域的时间，在从飞行器最终到达之后的预定时间之后设置快门定时时间 拍摄点区域，并且在快门定时时间由两个或更多个飞行车辆拍摄空中照片。

    Modular Vehicle Lift System
    250.
    发明申请
    Modular Vehicle Lift System 有权
    模块化车辆升降系统

    公开(公告)号：US20140374532A1

    公开(公告)日：2014-12-25

    申请号：US13925305

    申请日：2013-06-24

    Applicant: The Boeing Company

    Inventor： Michael J. Duffy ,  Scott H. Bouwer ,  John J. Mattero

    IPC: B64C37/02

    CPC classification number: B64C37/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/146 ,  G05D1/104

    Abstract: Apparatus, systems, and methods provide for a modular vehicle system utilized for lifting and maneuvering payloads. According to aspects of the disclosure, any number of individual lift vehicles may be connected to create a unified lift vehicle. The individual lift vehicles may be placed adjacent to one another according to a determined lifting array formation and coupled together using connection mechanisms. The connection mechanisms rigidly and communicatively connect the individual lift vehicles to create the unified lift vehicle suitable for lifting and maneuvering a payload.

    Abstract translation: 装置，系统和方法提供了用于提升和操纵有效载荷的模块化车辆系统。 根据本公开的方面，可以连接任意数量的单独的升降车，以产生统一的升降车。 各个电梯车辆可以根据确定的提升阵列形状彼此相邻放置并且使用连接机构联接在一起。 连接机构刚性地和连通地连接各个电梯车辆，以产生适于提升和操纵有效载荷的统一升降车。

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