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    Convertible compounded rotorcraft
    81.
    发明授权
    Convertible compounded rotorcraft 有权
    可转换复合旋翼航空器

    公开(公告)号：US08950698B1

    公开(公告)日：2015-02-10

    申请号：US13661567

    申请日：2012-10-26

    Applicant: The Boeing Company

    Inventor： Glenn T. Rossi

    IPC: B64D5/00 ,  B64C37/02 ,  B64C29/02

    CPC classification number: B64C27/26 ,  B64C27/28 ,  B64C29/0033 ,  B64C29/02 ,  B64C37/02 ,  B64C39/003 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/206 ,  B64D5/00

    Abstract: A compound rotorcraft including a rotary wing aircraft having a fuselage and at least one rotor and a fixed-wing aircraft coupled to the rotary wing aircraft, wherein the rotary wing aircraft can fly on the rotor or the fixed-wing aircraft, and wherein the fixed-wing aircraft is detachable from the rotary wing aircraft to fly independently.

    Abstract translation: 一种复合旋翼航空器，其包括具有机身的旋翼飞机和至少一个转子以及耦合到旋转翼飞行器的固定翼飞行器，其中所述旋翼飞机可以在所述转子或所述固定翼飞行器上飞行，并且其中所述固定 飞机可以从旋翼飞机上拆下来独立飞行。

    Marine vessel-towable aerovehicle system with automated tow line release
    82.
    发明授权
    Marine vessel-towable aerovehicle system with automated tow line release 有权
    具有自动牵引线释放的海洋船只可拖动的航空运输系统

    公开(公告)号：US08646719B2

    公开(公告)日：2014-02-11

    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: B65D3/00 ,  B65D47/00

    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。

    SYSTEM FOR CARRYING AND DROPPING LOADS FOR A TRANSPORT AIRPLANE
    83.
    发明申请
    SYSTEM FOR CARRYING AND DROPPING LOADS FOR A TRANSPORT AIRPLANE 有权
    运输和运输装载系统

    公开(公告)号：US20120251280A1

    公开(公告)日：2012-10-04

    申请号：US13515760

    申请日：2010-12-13

    Applicant: Benoit Jaurand ,  Frédéric Michaud

    Inventor： Benoit Jaurand ,  Frédéric Michaud

    IPC: B60P1/00

    CPC classification number: B64D1/10 ,  B64C2201/082 ,  B64C2201/206 ,  B64D1/12

    Abstract: The present disclosure relates to a system for carrying and dropping ammunition for a transport airplane. The system includes a container which contains at least one load, in particular ammunition, which is capable of being brought into a drop position, in which a portion is located outside the airplane, and from which a load can be dropped, usually by simply releasing said load.

    Abstract translation: 本公开涉及一种用于运输和运送飞机弹药的系统。 该系统包括容器，该容器包含至少一个负载，特别是弹药，其能够进入下降位置，其中一部分位于飞机外部，并且可以通过简单地释放负载， 说负载

    Methods and apparatus for aerial recovery of flying apparatus
    84.
    发明授权
    Methods and apparatus for aerial recovery of flying apparatus 有权
    飞行装置空中回收方法及装置

    公开(公告)号：US08191828B2

    公开(公告)日：2012-06-05

    申请号：US12120065

    申请日：2008-05-13

    Applicant: Kevin Reed Lutke ,  Aaron J. Kutzmann

    Inventor： Kevin Reed Lutke ,  Aaron J. Kutzmann

    IPC: B64F1/04

    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。

    System for airborne launch of an aircraft from a larger carrier aircraft
    87.
    发明授权
    System for airborne launch of an aircraft from a larger carrier aircraft 有权
    用于从较大载波飞机机载发射飞机的系统

    公开(公告)号：US06869042B2

    公开(公告)日：2005-03-22

    申请号：US10472230

    申请日：2002-02-20

    Applicant: Richard G Harrison

    Inventor： Richard G Harrison

    IPC: B64C39/02 ,  B64D3/00 ,  B64D5/00 ,  B64D39/02 ,  B64D39/06 ,  B64C37/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/206 ,  B64D3/00 ,  B64D5/00 ,  B64D39/02 ,  B64D39/06

    Abstract: A system for launching, refuelling and recovering in flight an aircraft (10) such as an unmanned aerial vehicle (UAV) from a larger carrier aircraft (16) comprising a holder (22) on the carrier aircraft (16) to which the UAV (10) is detachably connectable and an extendable and retractable refuelling device (23, 24) on the carrier aircraft (16) detachably connectable to the UAV (10) whereby to launch the UAV it is disconnected from the holder (22), the refuelling device (23, 24) is extended with the UAV connected thereto to cause the UAV to trail behind the carrier aircraft and the UAV is then disconnected from the refuelling device.

    Abstract translation: 一种用于从飞机上起飞，加油和恢复飞行器（10）的系统，所述飞机（10）从诸如无人飞行器（UAV）的大型载客飞机（16）起飞，所述飞机（10）包括在所述载体飞机（16）上的载具飞机（16） 10）可拆卸地连接，并且可拆卸地连接到UAV（10）的载体飞行器（16）上的可伸缩的加油装置（23,24），由此能够将UAV从保持器（22）断开，加油装置 （23,24）在与其连接的UAV的情况下延伸，使得UAV在载客飞行器后行驶，然后UAV从加油装置断开。

    System for airborn launch of an aircraft from a larger carrier aircraft
    88.
    发明申请
    System for airborn launch of an aircraft from a larger carrier aircraft 有权
    飞机从较大的载具飞机发射飞机的系统

    公开(公告)号：US20040089767A1

    公开(公告)日：2004-05-13

    申请号：US10472230

    申请日：2003-09-22

    Inventor： Richard G. Harrison

    IPC: H04B007/185

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/206 ,  B64D3/00 ,  B64D5/00 ,  B64D39/02 ,  B64D39/06

    Abstract: A system for launching, refuelling and recovering in flight an aircraft (10) such as an unmanned aerial vehicle (UAV) from a larger carrier aircraft (16) comprising a holder (22) on the carrier aircraft (16) to which the UAV (10) is detachably connectable and an extendable and retractable refuelling device (23, 24) on the carrier aircraft (16) detachably connectable to the UAV (10) whereby to launch the UAV it is disconnected from the holder (22), the refuelling device (23, 24) is extended with the UAV connected thereto to cause the UAV to trail behind the carrier aircraft and the UAV is then disconnected from the refuelling device.

    Abstract translation: 一种用于从飞机上起飞，加油和恢复飞行器（10）的系统，所述飞机（10）从诸如无人飞行器（UAV）的大型载客飞机（16）起飞，所述飞机（10）包括在所述载体飞机（16）上的载具飞机（16） 10）可拆卸地连接，并且可拆卸地连接到UAV（10）的载体飞行器（16）上的可伸缩的加油装置（23,24），由此能够将UAV从保持器（22）断开，加油装置 （23,24）在与其连接的UAV的情况下延伸，使得UAV在载客飞行器后行驶，然后UAV从加油装置断开。

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