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    Line Intersect Vehicle Launch and Recovery
    162.
    发明申请
    Line Intersect Vehicle Launch and Recovery 审中-公开
    线相交车辆启动和恢复

    公开(公告)号：US20160221689A1

    公开(公告)日：2016-08-04

    申请号：US14952949

    申请日：2015-11-26

    Applicant: Christopher Ralph Tridico

    Inventor： Christopher Ralph Tridico

    IPC: B64F1/04 ,  B64D3/00 ,  B64D47/02 ,  B64F1/08

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/182 ,  B64C2201/206 ,  B64D5/00

    Abstract: The present invention is a system which facilitates the launch and recovery of an aircraft or other vehicle by another vehicle or site. This system includes cables, wires or other “lines” that are connected to both the subject vehicle and the launch and recovery platform and facilities to extend, retract and position these lines. When the relative motion of the subject vehicle and launch and recovery platform causes the lines to intersect, the lines are connected to each other by means of a hook, carabiner or similar attachment device resulting in the effective capture of the subject vehicle. One or both of the lines may then be retracted resulting in the recovery of the subject vehicle. Launch is accomplished by extending one or both of the lines and subsequently releasing the attachment device.

    Abstract translation: 本发明是一种便于由其他车辆或场所发射和回收飞机或其他车辆的系统。 该系统包括连接到主车辆和发射和恢复平台的电缆，电线或其他“线路”以及用于延伸，缩回和定位这些线路的设备。 当主体车辆和发射和恢复平台的相对运动导致线路相交时，线路通过钩，卡扣或相似的附接装置彼此连接，从而有效地捕获本车辆。 然后可以将一条或两条线缩回，导致本车辆的恢复。 发射通过延伸一条或两条线并随后释放附着装置来实现。

    AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE
    163.
    发明申请
    AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE 有权
    用于空运车辆的空运集装箱

    公开(公告)号：US20150266578A1

    公开(公告)日：2015-09-24

    申请号：US14018493

    申请日：2013-09-05

    Applicant: Raytheon Company

    Inventor： Erick W. Elkins ,  Matthew Glenn Murphy ,  Scott D. Thomas

    IPC: B64D1/12 ,  B64C39/02

    CPC classification number: B64D1/12 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/201 ,  B64C2201/206

    Abstract: A container is used to launch a small aircraft, such as an unmanned aerial vehicle (UAV), from a host aircraft. The container protects the UAV from stresses during the initial ejection from a launcher that is part of the host aircraft. The initial stresses may be due to turbulence in the vicinity of the host aircraft, high airspeed, and/or tumbling that may result from the ejection from the host aircraft moving at a high airspeed. The container may deploy a drag device, such as a drogue chute, to slow the container down and reorient the container, prior to deployment of the UAV from the container. During the time between ejection from the host aircraft and deployment from the container, the UAV may be powered up and acquire data, such as global positioning system (GPS) data, to allow the UAV a “hot start” enabling immediate mission commencement.

    Abstract translation: 一个集装箱用于从一架主机上发射一架小型飞机，如无人飞行器（UAV）。 该容器保护无人机在最初从作为主机的一部分的发射器弹出之前受到压力。 初始应力可能是由于主机飞机附近的湍流，高空速和/或可能由主飞机从高空速下移动而导致的翻滚造成的。 在从容器部署UAV之前，容器可以部署拖动装置，例如锥形滑槽，以使容器向下减速并重新定向容器。 在从主机飞行器和从集装箱部署之间的时间内，UAV可以被加电并且获取诸如全球定位系统（GPS）数据的数据，以允许UAV“启动”，从而能够立即启动任务。

    System for carrying and dropping loads for a transport airplane
    164.
    发明授权
    System for carrying and dropping loads for a transport airplane 有权
    用于运输飞机载运的系统

    公开(公告)号：US08979029B2

    公开(公告)日：2015-03-17

    申请号：US13515760

    申请日：2010-12-13

    Applicant: Benoît Jaurand ,  Frédéric Michaud

    Inventor： Benoît Jaurand ,  Frédéric Michaud

    IPC: B64C1/22 ,  B64D1/10 ,  B64D1/12

    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 the 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， 负载。

    Convertible compounded rotorcraft
    165.
    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
    166.
    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
    167.
    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
    168.
    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。

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