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    COMBINATION OF UNMANNED AERIAL VEHICLES AND THE METHOD AND SYSTEM TO ENGAGE IN MULTIPLE APPLICATIONS
    34.
    发明申请
    COMBINATION OF UNMANNED AERIAL VEHICLES AND THE METHOD AND SYSTEM TO ENGAGE IN MULTIPLE APPLICATIONS 审中-公开
    无人驾驶航空器的组合以及多种应用中的方法和系统

    公开(公告)号：US20160214717A1

    公开(公告)日：2016-07-28

    申请号：US15025245

    申请日：2013-11-08

    Applicant: SHELTON GAMINI DE SILVA

    Inventor： Shelton Gamini De Silva

    IPC: B64D5/00 ,  G05D1/10 ,  G05D1/00 ,  B64C39/02 ,  B64D47/08

    CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/082 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/143 ,  B64C2201/145 ,  B64C2201/206 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/104 ,  H04L67/12

    Abstract: This invention relates to an Unmanned Aerial Vehicle hereinafter called “Mother UAV” member (11) capable of carrying modules of Sub Unmanned Aerial Vehicle members (12) hereinafter called “Sub UAV” member. More particularly, the method and system that is capable of communicating via satellite and remote control technology wherein ejecting said Sub UAV members (12) from the Mother UAV member (11) wherein Sub UAV members (12) autonomously fly in sequence in a coordinated manner with the Mother UAV member (11), and capable of engaging in multiple missions in high, medium, low altitude, and surface, also communication with under sea submarines (27). Further, comprises of a method and system that the Sub UAV members (12) are able to return back to the Mother UAV member (11) after the mission is completed and be firmly secured to the flatbed (14) of the Mother UAV member (11). The present invention is specifically designed for multifunctional and multipurpose applications where humans and other vehicles are unable to access, for civil, commercial and military purposes.

    Abstract translation: 本发明涉及以下称为“无人机UAV”的无人飞行器，其能够携带以下称为“副无人机”的副无人飞行器部件（12）的模块。 更具体地，能够通过卫星和遥控技术进行通信的方法和系统，其中从UA无人机组成员（11）弹出所述副无人机部件（12），其中副无人机部件（12）以协调的方式自主地飞行 与无人机无人机（11）成员（11），能够从事高，中，低空和地面的多个任务，并与海底潜艇（27）进行通信。 此外，还包括一个方法和系统，子任务机构（12）能够在任务完成之后返回到无人机（UA）成员（11），并牢固地固定在无人机（UAV）成员的平板（14）上 11）。 本发明专为多功能和多用途应用而设计，人类和其他车辆无法进入民用，商业和军事目的。

    AIRCRAFT DEPLOYMENT AND RETRIEVAL OF UNMANNED AERIAL VEHICLES
    38.
    发明申请
    AIRCRAFT DEPLOYMENT AND RETRIEVAL OF UNMANNED AERIAL VEHICLES 有权
    飞机部署和检索无人机动车

    公开(公告)号：US20140117147A1

    公开(公告)日：2014-05-01

    申请号：US13664323

    申请日：2012-10-30

    Applicant: THE BOEING COMPANY

    Inventor： Mark Hanna ,  David R. Poling

    IPC: B64D5/00

    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。

    Micro-unmanned aerial vehicle deployment system
    39.
    发明授权
    Micro-unmanned aerial vehicle deployment system 失效
    微型无人机部署系统

    公开(公告)号：US08708285B1

    公开(公告)日：2014-04-29

    申请号：US13004152

    申请日：2011-01-11

    Applicant: Paul J. Carreiro

    Inventor： Paul J. Carreiro

    IPC: B64C13/20

    CPC classification number: B64C39/028 ,  B64C2201/082 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/206 ,  F42B12/60 ,  F42B15/10

    Abstract: A micro-unmanned aerial vehicle deployment system is provided for a cruise missile having submunition compartments. The system includes a vehicle launch module releasable from the cruise missile submunition compartment. The vehicle launch system has a control circuit and at least one micro-unmanned aerial vehicle contained therein. Structure is provided in the launch module for deploying the micro-unmanned aerial vehicle. A separable tether can be joined between the cruise missile and the vehicle launch module that separates when subjected to tension after deployment of the vehicle launch module.

    Abstract translation: 为具有子弹药舱的巡航导弹提供了一种微型无人驾驶飞行器部署系统。 该系统包括可从巡航导弹子弹药室释放的车辆发射模块。 车辆发射系统具有控制电路和其中容纳的至少一个微型无人驾驶飞行器。 在发射模块中提供了用于部署微型无人驾驶飞行器的结构。 可以在巡航导弹和在车辆发射模块部署之后经受张力时分离的车辆发射模块之间连接可分离系绳。

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