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    AIRCRAFT DEPLOYMENT AND RETRIEVAL OF UNMANNED AERIAL VEHICLES
    194.
    发明申请
    AIRCRAFT DEPLOYMENT AND RETRIEVAL OF UNMANNED AERIAL VEHICLES 审中-公开
    飞机部署和检索无人机动车

    公开(公告)号：US20150329205A1

    公开(公告)日：2015-11-19

    申请号：US14792165

    申请日：2015-07-06

    Applicant: The Boeing Company

    Inventor： Mark Hanna ,  David R. Poling

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/082 ,  B64C2201/126 ,  B64C2201/182 ,  B64C2201/206

    Abstract: An aircraft system incorporates a first aircraft having a grappling device including a first gripper with a first actuator and a second gripper with a second actuator. The first gripper and the second gripper are movable between an open and a closed position to engage a hooking device and pivot together to change a capture angle. A first controller receives a command and operates the actuators in response to open and close the first and second grippers of the grappling device. The controller also receives a second command and operates the first and second actuators to pivot the grippers and provide grappling at a range of capture angles. A second aircraft, which may be a UAV, incorporates the hooking device. The hooking device includes a ring rotatable from the surface and a third actuator to rotate the ring between a stowed and an extended position.

    Abstract translation: 飞行器系统包括具有抓斗装置的第一飞行器，该抓斗装置包括具有第一致动器的第一夹持器和具有第二致动器的第二夹持器。 第一夹持器和第二夹持器可在打开位置和关闭位置之间移动以接合钩挂装置并枢转在一起以改变捕获角度。 响应于打开和关闭抓斗装置的第一和第二夹持器，第一控制器接收命令并操作致动器。 控制器还接收第二命令并且操作第一和第二致动器以枢转夹持器并且在捕获角度范围内提供抓斗。 可能是UAV的第二架飞机结合了挂钩装置。 挂钩装置包括从表面可旋转的环和第三致动器，以在收起和伸出位置之间旋转环。

    UAV deployment and control system
    195.
    发明申请
    UAV deployment and control system 审中-公开
    无人机部署和控制系统

    公开(公告)号：US20150321758A1

    公开(公告)日：2015-11-12

    申请号：US14121422

    申请日：2014-09-02

    Applicant: Peter Christopher Sarna, II

    Inventor： Peter Christopher Sarna, II

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/08 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/201 ,  G05D1/0011

    Abstract: A system of software and hardware components is disclosed comprising a system designed to deploy, manage, and control unmanned aerial vehicles (UAVs). The integrated UAVs can be deployed from vehicles, buildings, and other types of fixed locations. The present disclosure enables users to deploy UAVs to perform pre-defined flight maneuvers and fly to pre-designated locations. The present disclosure also and affords the ability for users to maintain the UAVs flight control locally or transfer control of a deployed UAV to remotely located system operators.

    Abstract translation: 公开了一种软件和硬件组件的系统，其包括被设计为部署，管理和控制无人机（UAV）的系统。 集成无人机可以从车辆，建筑物和其他类型的固定位置部署。 本公开使得用户能够部署无人机来执行预定义的飞行操纵并飞到预先指定的位置。 本公开还提供了用户能够本地维护UAV飞行控制的能力或者将部署的UAV的控制转移到位于远程的系统操作者的能力。

    Rapid deployment air and water vehicle
    196.
    发明授权
    Rapid deployment air and water vehicle 有权
    快速部署空中和水车

    公开(公告)号：US09010678B1

    公开(公告)日：2015-04-21

    申请号：US13786299

    申请日：2013-03-05

    Applicant: The Boeing Company

    Inventor： Nathan Hiller

    IPC: B60F5/02

    CPC classification number: B60F5/02 ,  B64C37/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/205 ,  B64C2201/206

    Abstract: A vehicle which is adaptable for both flight and water travel includes: a body; a wing, a stabilizer, or a first propelling member; and at least one attachment member. The body is configured to fly through air and to move through water. The at least one attachment member attaches the wing, the stabilizer, or the first propelling member to the body while the body is in flight. The at least one attachment member detaches at least a portion of the wing, at least a portion of the stabilizer, or at least a portion of the first propelling member from the body when the body is in the water.

    Abstract translation: 适用于飞行和水上旅行的车辆包括：身体; 翼，稳定器或第一推进构件; 和至少一个附接构件。 身体被配置为飞过空气并移动通过水。 当身体飞行时，至少一个附接构件将翼，稳定器或第一推进构件附接到身体。 当身体在水中时，至少一个附接构件将至少一部分翼，至少一部分稳定器，或至少一部分第一推进构件与身体分开。

    Vehicle with aerial and ground mobility
    197.
    发明授权
    Vehicle with aerial and ground mobility 有权
    具有空中和地面移动性的车辆

    公开(公告)号：US08991740B2

    公开(公告)日：2015-03-31

    申请号：US13846074

    申请日：2013-03-18

    Applicant: Draganfly Innovations Inc.

    Inventor： Orville Olm ,  Greg Wood ,  Zenon Dragan

    IPC: B64C37/00 ,  B60F5/02 ,  B60B1/00

    CPC classification number: B64C37/00 ,  B60B1/00 ,  B60F5/02 ,  B60Y2200/80 ,  B64C39/005 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162

    Abstract: A combination rotor and wheel assembly for an unmanned vehicle with ground and aerial mobility has a rotor arm adapted to be attached at an inner end thereof to a vehicle body. A rotor is rotatably connected to an outer end of the rotor arm about a rotor axis, and a rotor drive mounted on the rotor arm rotates the rotor such that the rotor exerts an upward lift force on the rotor arm. An open spoked wheel is rotatably connected about the rotor axis independent of the rotor The diameter of the wheel is greater than that of the rotor, and a bottom edge of the wheel is below the rotor. A wheel drive rotates the wheel. Vehicles can have various numbers and orientations of the rotor and wheel assembly to provide aerial and ground mobility.

    Abstract translation: 用于具有地面和空中移动性的无人驾驶车辆的组合转子和车轮组件具有适于在其内端附接到车体的转子臂。 转子围绕转子轴线可旋转地连接到转子臂的外端，并且安装在转子臂上的转子驱动器使转子旋转，使得转子在转子臂上施加向上的升力。 开放式的轮轮围绕转子轴线可旋转地连接，与转子无关。轮的直径大于转子的直径，并且车轮的底部边缘在转子下方。 轮驱动器旋转车轮。 车辆可以具有转子和车轮组件的各种数量和方向，以提供空中和地面的移动性。

    Helicopter with multi-rotors and wireless capability
    198.
    发明授权
    Helicopter with multi-rotors and wireless capability 有权
    具有多转子和无线能力的直升机

    公开(公告)号：US08774982B2

    公开(公告)日：2014-07-08

    申请号：US13200986

    申请日：2011-10-06

    Applicant: John Robert Oakley ,  David Scott Heath

    Inventor： John Robert Oakley ,  David Scott Heath

    IPC: G05D1/00 ,  B64C27/08 ,  G05D1/08 ,  B64C39/02 ,  H04N7/18 ,  B64C25/32

    CPC classification number: B64C39/024 ,  B64C25/52 ,  B64C27/08 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2211/00 ,  G05D1/0038 ,  G05D1/0088 ,  G05D1/0202 ,  G05D1/0858 ,  H04N7/185

    Abstract: The present invention relates to a helicopter having a modular airframe, with multiple layers which can be connected easily, the layers which house the electronics (autopilot and navigation systems), batteries, and payload (including camera system) of the helicopter. The helicopter has four, six, and eight rotors, which can be easily changed via removing one module of the airframe. In one embodiment, the airframe has a vertical stacked appearance, and in another embodiment, a domed shape (where several of the layers are stacked internally). In one embodiment, there is a combination landing gear and camera mount. The helicopter allows for simple flight and usage by remote control, and non-remote control, users.

    Abstract translation: 本发明涉及一种具有模块化机身的直升机，其具有容易连接的多层，容纳直升机的电子设备（自动驾驶仪和导航系统），电池和有效载荷（包括照相机系统）的层。 直升机有四个，六个和八个转子，可以通过卸下机身的一个模块轻松更换。 在一个实施例中，机身具有垂直的堆叠外观，并且在另一个实施例中，圆顶形状（其中几个层内部堆叠）。 在一个实施例中，存在组合起落架和相机安装座。 直升机允许通过遥控器和非遥控器，用户进行简单的飞行和使用。

    Modular Pods for Use with an Unmanned Aerial Vehicle
    200.
    发明申请
    Modular Pods for Use with an Unmanned Aerial Vehicle 审中-公开
    用于无人机的模块化荚

    公开(公告)号：US20120153087A1

    公开(公告)日：2012-06-21

    申请号：US12186693

    申请日：2008-08-06

    Applicant: Daniel Ross Collette ,  Joseph Scott Helsing, JR.

    Inventor： Daniel Ross Collette ,  Joseph Scott Helsing, JR.

    IPC: B64C39/00 ,  B64D47/08 ,  B64D37/02 ,  B64C7/00

    CPC classification number: B64C39/024 ,  B64C27/20 ,  B64C2201/027 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/162 ,  B64C2211/00

    Abstract: A pod for an unmanned aerial vehicle is provided that may be removed and re-attached to the vehicle. The pod comprises an outer shell, within which a variety of payloads may be carried. A first surface on the vehicle frame comprises a plurality of connects or electrical traces. The plurality of attachments are used to removably attach the pods to the first surface. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.

    Abstract translation: 提供用于无人驾驶飞行器的舱架，其可以被移除并重新附接到车辆。 荚包括外壳，在其中可以携带各种有效载荷。 车架上的第一表面包括多个连接或电迹线。 多个附件用于将荚可移除地附接到第一表面。 因此，可以简单地通过将不同的荚移除并附接到固定的车辆核心，使用相同的无人驾驶飞行器来传送各种有效载荷。 这些荚可以成形为形成车辆外部的一部分，并且当荚附接到框架时，它们增强了车辆的空气动力学。

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