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    Device for launching unmanned missiles from an aircraft
    61.
    发明授权
    Device for launching unmanned missiles from an aircraft 有权
    从飞机上发射无人导弹的装置

    公开(公告)号：US08387920B2

    公开(公告)日：2013-03-05

    申请号：US13034369

    申请日：2011-02-24

    Applicant: Michael Grabmeier

    Inventor： Michael Grabmeier

    IPC: B64D1/12

    CPC classification number: B64D1/12 ,  B64C2201/206

    Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylon for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

    Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有一个上部容器部分，该部分具有用于导弹悬挂的可拆卸支撑件的塔架。 容器具有较低的容器部分，其被实施为导弹的支撑区域。

    TOWABLE AIR VEHICLE
    62.
    发明申请
    TOWABLE AIR VEHICLE 有权
    可行的空中车辆

    公开(公告)号：US20120091259A1

    公开(公告)日：2012-04-19

    申请号：US13215034

    申请日：2011-08-22

    Applicant: John William Morris ,  Charles A. Jarnot

    Inventor： John William Morris ,  Charles A. Jarnot

    IPC: B64C27/02 ,  B64C27/12 ,  B64C27/54

    CPC classification number: B64C27/02 ,  B64C19/00 ,  B64C2201/108 ,  B64C2201/206 ,  B64D3/00

    Abstract: An unmanned, towable air vehicle is described and includes electronic sensors to increase the detection range relative to the horizon detection limitations of a surface craft, an autogyro assembly to provide lift, and a controller to control operation the autogyro assembly for unmanned flight. A forward motive force powers the autogyro assembly to provide lift. In an example, the autogyro assembly includes a mast extending from the container, a rotatable hub on an end of the mast, and a plurality of blades connected to the hub for rotation to provide lift to the vehicle. In an example, an electrical motor rotates the blades prior to lift off to assist in take off. The electrical motor does not have enough power to sustain flight of the vehicle in an example.

    Abstract translation: 描述了一种无人驾驶的可拖动的飞行器，并且包括电子传感器，以增加相对于水面飞行器的水平面检测限制的检测范围，用于提供电梯的自动组件，以及用于控制无人驾驶自动组合的操作的控制器。 向前的动力为自动组件提供动力。 在一个示例中，自动组件组件包括从容器延伸的桅杆，在桅杆的端部上的可旋转轮毂，以及连接到轮毂以便旋转以提供车辆升力的多个叶片。 在一个示例中，电动马达在升降之前旋转叶片以帮助起飞。 在一个例子中，电动机没有足够的能力来维持车辆的飞行。

    MODULAR ARTICULATED-WING AIRCRAFT
    63.
    发明申请
    MODULAR ARTICULATED-WING AIRCRAFT 有权
    MODULAR ARTICULATED-WING飞机

    公开(公告)号：US20120048990A1

    公开(公告)日：2012-03-01

    申请号：US13154796

    申请日：2011-06-07

    Applicant: Geoffrey S. SOMMER

    Inventor： Geoffrey S. SOMMER

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/143 ,  B64C2201/165 ,  B64C2201/206

    Abstract: Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

    Abstract translation: 提供了用于形成具有高纵横比翼平台的多关节飞行系统（天基）的系统和/或方法，其可操作以在高海拔地区的感兴趣区域上游荡。 在某些示例性实施例中，自主模块化飞行器以翼尖到翼尖的方式连接在一起。 这样的模块化飞行器可以从日晒中获得其功率。 自主传单可以包括单独操作的传感器，或者在形成天空基础之后集体运行。 天空基优选地可以按照主要条件的要求进行聚合，分解和/或再聚集。 因此，可能提供“永远在车”的飞机。

    DEVICE FOR LAUNCHING UNMANNED MISSILES FROM AN AIRCRAFT
    64.
    发明申请
    DEVICE FOR LAUNCHING UNMANNED MISSILES FROM AN AIRCRAFT 有权
    从飞机上发射无人机的装置

    公开(公告)号：US20110209602A1

    公开(公告)日：2011-09-01

    申请号：US13034369

    申请日：2011-02-24

    Applicant: Michael GRABMEIER

    Inventor： Michael GRABMEIER

    IPC: B64D1/04

    CPC classification number: B64D1/12 ,  B64C2201/206

    Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylon for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

    Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有一个上部容器部分，该部分具有用于导弹悬挂的可拆卸支撑件的挂钩。 容器具有较低的容器部分，其被实施为导弹的支撑区域。

    Device for launching unmanned missiles from an aircraft
    65.
    发明授权
    Device for launching unmanned missiles from an aircraft 有权
    从飞机上发射无人导弹的装置

    公开(公告)号：US07926764B2

    公开(公告)日：2011-04-19

    申请号：US11766343

    申请日：2007-06-21

    Applicant: Michael Grabmeier

    Inventor： Michael Grabmeier

    IPC: B64D1/12

    CPC classification number: B64D1/12 ,  B64C2201/206

    Abstract: A device for launching unmanned missiles from an aircraft with a pallet, on which at least one container is provided to receive a missile. The container has an upper container section that has a pylon for the suspended, detachable support of the missile. The container has a lower container section that is embodied as a support area for the missile.

    Abstract translation: 用于从具有托盘的飞机发射无人导弹的装置，其上提供至少一个容器以接收导弹。 容器具有一个上部容器部分，该部分具有用于导弹悬挂的可拆卸支撑件的挂钩。 容器具有较低的容器部分，其被实施为导弹的支撑区域。

    Drone deployment system
    70.
    发明授权
    Drone deployment system 有权

    公开(公告)号：US09896208B2

    公开(公告)日：2018-02-20

    申请号：US14951527

    申请日：2015-11-25

    Applicant: Alan Retig ,  David J Kreher

    Inventor： Alan Retig ,  David J Kreher

    IPC: B64D5/00

    CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/182 ,  B64C2201/206

    Abstract: The present disclosure reveals a drone deployment system for use from an airborne aircraft such that the drone deployment system is capable of moving through the aircraft, picking up a drone with a grappling means attached to an extendable arm, moving to an opening in the aircraft, extending and deploying the drone. The drone deployment system is further capable of retrieving a drone by having the extendable arm extended out the opening in the aircraft, having the drone fly into the grappling means which then engages, holding the drone, and the extendable arm is then retractable so that the opening can be closed and the drone placed in storage.

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