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    Methods and Apparatus for Aerial Recovery of Flying Apparatus
    11.
    发明申请
    Methods and Apparatus for Aerial Recovery of Flying Apparatus 有权
    飞行器具空中恢复方法与装置

    公开(公告)号：US20120211588A1

    公开(公告)日：2012-08-23

    申请号：US13465220

    申请日：2012-05-07

    Applicant: Kevin Reed Lutke ,  Aaron J. Kutzmann

    Inventor： Kevin Reed Lutke ,  Aaron J. Kutzmann

    IPC: B64D5/00

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/206

    Abstract: Methods and systems are provided which may allow a first vehicle to recover a second air vehicle while both are moving. The first vehicle and the second air vehicle may be traveling at different velocities. An attachment member of the second air vehicle may attach to a recovery member of the first vehicle while the first vehicle and the second air vehicle are traveling at different velocities. The recovery member attached to the second air vehicle may move relative to and along an exterior surface of the first vehicle in a direction substantially parallel to a direction of travel of the first vehicle.

    Abstract translation: 提供了方法和系统，其可以允许第一车辆在移动时都恢复第二空中车辆。 第一车辆和第二空中车辆可以以不同的速度行驶。 当第一车辆和第二空中车辆以不同的速度行驶时，第二空中车辆的附接构件可以附接到第一车辆的回收构件。 附接到第二空气车辆的回收构件可以在与第一车辆的行进方向基本平行的方向上相对于第一车辆的外表面移动并沿其移动。

    MODULAR ARTICULATED-WING AIRCRAFT
    12.
    发明申请
    MODULAR ARTICULATED-WING AIRCRAFT 有权
    MODULAR ARTICULATED-WING飞机

    公开(公告)号：US20110144834A1

    公开(公告)日：2011-06-16

    申请号：US12805434

    申请日：2010-07-30

    Applicant: Geoffrey S. Sommer

    Inventor： Geoffrey S. Sommer

    IPC: B64C37/02 ,  G05D1/00

    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。

    UNMANNED AIRCRAFT SYSTEM AND OPERATION METHOD THEREOF
    13.
    发明申请
    UNMANNED AIRCRAFT SYSTEM AND OPERATION METHOD THEREOF 有权
    不限制的飞机系统及其操作方法

    公开(公告)号：US20110049288A1

    公开(公告)日：2011-03-03

    申请号：US12935432

    申请日：2009-08-13

    Applicant: Satoshi Suzuki

    Inventor： Satoshi Suzuki

    IPC: B64C37/02 ,  B64D5/00

    CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/082 ,  B64C2201/206 ,  G05D1/104

    Abstract: An unmanned aircraft system includes a manned aircraft and an unmanned aircraft. The manned aircraft includes a manned aircraft main wing, a manned aircraft fuselage, a manned aircraft landing system, and a manned aircraft joining mechanism provided at a bottom portion of the manned aircraft fuselage. The unmanned aircraft includes an unmanned aircraft main wing, an unmanned aircraft fuselage, an unmanned aircraft landing system, and an unmanned aircraft joining mechanism provided at a roof portion of the unmanned aircraft fuselage. The manned aircraft joining mechanism and the unmanned aircraft joining mechanism are detachably joined. The unmanned aircraft system can take off or land in a state that the unmanned aircraft and the manned aircraft are joined.

    Abstract translation: 无人机系统包括载人飞机和无人飞机。 载人飞机包括载人飞机主翼，载人飞机机身，载人飞机着陆系统，以及设置在载人飞机机身底部的载人飞机连接机构。 无人机包括无人驾驶飞机主翼，无人飞机机身，无人飞机着陆系统以及设在无人驾驶飞机机身顶部的无人飞机连接机构。 载人飞机接合机构和无人飞行器接合机构可拆卸地接合。 无人驾驶飞机系统可以以无人驾驶飞机和载人飞机加入的状态起飞或着陆。

    MODULAR ARTICULATED-WING AIRCRAFT
    14.
    发明申请
    MODULAR ARTICULATED-WING AIRCRAFT 有权
    MODULAR ARTICULATED-WING飞机

    公开(公告)号：US20100193625A1

    公开(公告)日：2010-08-05

    申请号：US11475085

    申请日：2006-06-27

    Applicant: Geoffrey S. Sommer

    Inventor： Geoffrey S. Sommer

    IPC: B64C37/02 ,  B64D27/02 ,  G05D1/00

    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。

    Combined Vertical Takeoff and Landing UAV
    15.
    发明公开
    Combined Vertical Takeoff and Landing UAV 审中-公开

    公开(公告)号：US20230159164A1

    公开(公告)日：2023-05-25

    申请号：US18058262

    申请日：2022-11-22

    Applicant: Autoflight (Kunshan) Co., Ltd.

    Inventor： Yu Tian

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/02 ,  B64C2201/082 ,  B64C2201/088 ,  B64C2201/206

    Abstract: A combined vertical takeoff and landing UAV having a large vertical takeoff and landing UAV, a connecting device, and a small vertical takeoff and landing UAV. The connecting device having a clamping component and an adsorption component. The clamping component includes a clamping part, and a clamping groove is arranged on the clamping part. The clamping component having a snap-fitting part, and a snap-fitting groove is arranged on the snap-fitting part. The clamping groove and the snap-fitting groove are correspondingly set. A first holding space is arranged on the clamping part, and a second holding space is arranged on the snap-fitting part. The adsorption component comprises a first magnetic element located in the first holding space, and the adsorption component also comprises a second magnetic element, which is located in the second holding space.

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