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    Rapid deployment air and water vehicle
    92.
    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。

    Unmanned aircraft system and operation method thereof
    93.
    发明授权
    Unmanned aircraft system and operation method thereof 有权
    无人机系统及其操作方法

    公开(公告)号：US08740134B2

    公开(公告)日：2014-06-03

    申请号：US12935432

    申请日：2009-08-13

    Applicant: Satoshi Suzuki

    Inventor： Satoshi Suzuki

    IPC: B64C37/02

    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。

    Methods and Apparatus for Aerial Recovery of Flying Apparatus
    94.
    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
    95.
    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。

    System and methods for airborne launch and recovery of aircraft
    96.
    发明授权
    System and methods for airborne launch and recovery of aircraft 有权
    机载发射和恢复飞机的系统和方法

    公开(公告)号：US07900866B2

    公开(公告)日：2011-03-08

    申请号：US11874804

    申请日：2007-10-18

    Applicant: Aaron J. Kutzmann ,  Kevin R. Lutke

    Inventor： Aaron J. Kutzmann ,  Kevin R. Lutke

    IPC: B64D5/00

    CPC classification number: B64D3/00 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/182 ,  B64D5/00

    Abstract: A system and methods for airborne launch and recovery of aircraft. In one embodiment the system comprises a flexible tether configured to be towed behind an airborne mother ship. A drag device is secured to a distal end of the flexible tether to generate drag and maintain tension in the flexible tether. A reel associated with the mother ship anchors a proximal portion of the flexible tether and selectively lets out and takes up the flexible tether to adjust a length of the flexible tether. A capture mechanism associated with the aircraft engages the flexible tether to enable the aircraft to translate along the flexible tether. In embodiments of the present methods, a flexible tether is deployed from an airborne mother ship. An aircraft translates forward and rearward along the flexible tether. Prior to launch, the weight of the aircraft is transferred from the flexible tether to the wings. During recovery, the weight of the aircraft is transferred from the wings to the flexible tether.

    Abstract translation: 飞机机载发射和恢复的系统和方法。 在一个实施例中，系统包括被配置为被拖到空中母舰后面的柔性系绳。 牵引装置固定到柔性系绳的远端以产生阻力并保持柔性系绳中的张力。 与母船相关联的卷轴锚定柔性系绳的近端部分，并且选择性地放出并吸收柔性系绳以调节柔性系绳的长度。 与飞行器相关联的捕获机构接合柔性系绳，以使飞机沿着柔性系绳平移。 在本方法的实施例中，从空中母舰部署柔性系绳。 飞机沿着柔性系绳向前和向后平移。 在发射之前，飞机的重量从柔性系绳转移到机翼。 在恢复期间，飞机的重量从翼转移到柔性系绳。

    UNMANNED AIRCRAFT SYSTEM AND OPERATION METHOD THEREOF
    97.
    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
    99.
    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。

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