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    METHODS AND APPARATUSES FOR LAUNCHING AIRBORNE DEVICES ALONG FLEXIBLE ELONGATED MEMBERS
    72.
    发明申请
    METHODS AND APPARATUSES FOR LAUNCHING AIRBORNE DEVICES ALONG FLEXIBLE ELONGATED MEMBERS 审中-公开
    用于启动柔性伸长构件的空气动力装置的方法和装置

    公开(公告)号：WO2005016753A2

    公开(公告)日：2005-02-24

    申请号：PCT/US2004/009988

    申请日：2004-04-01

    Applicant: THE INSITU GROUP, INC. ,  ROESELER, Cory ,  MCGEER, Brian, T. ,  VON FLOTOW, Andreas, H.

    Inventor： ROESELER, Cory ,  MCGEER, Brian, T. ,  VON FLOTOW, Andreas, H.

    IPC: B64F

    CPC classification number: B64C39/024 ,  B64C2201/084

    Abstract: Methods and apparatuses for cable launching airborne devices (e.g., unmanned aircraft) are disclosed. In one embodiment, an apparatus includes an elongated structure, e.g., a tower, boom or derrick. At least one flexible elongated member (e.g., a cable or rope) can be attached toward one end to the structure and toward another end to the ground or another structure to form an elongated launch path. A cradle, which can carry the airborne device, can also be movably attached to the flexible elongated member and can be accelerated along the launch path. As the cradle decelerates, the aircraft can be released into flight.

    Abstract translation: 公开了用于电缆发射机载装置（例如，无人飞行器）的方法和装置。 在一个实施例中，装置包括细长结构，例如塔架，起重臂或井架。 至少一个柔性细长构件（例如，电缆或绳索）可以朝向结构的一端并且朝向地面或另一结构的另一端附接以形成细长的发射路径。 可以携带机载装置的托架也可以可移动地附接到柔性细长构件并且可以沿着发射路径被加速。 当支架减速时，飞机可以释放飞行。

    An air intake system for an air vehicle
    78.
    发明公开
    An air intake system for an air vehicle 审中-公开
    Lufteinlasssystemfürein Luftfahrzeug

    公开(公告)号：EP2460729A1

    公开(公告)日：2012-06-06

    申请号：EP11275081.5

    申请日：2011-05-12

    Applicant: MBDA UK Limited

    Inventor： The designation of the inventor has not yet been filed

    IPC: B64D33/02 ,  F02C7/042 ,  F42B10/32 ,  F42B15/10

    CPC classification number: B64D33/02 ,  B64C2201/084 ,  B64D2241/00 ,  F02C7/042 ,  F05D2250/411 ,  F05D2250/51 ,  F42B10/32 ,  F42B15/10 ,  Y10T137/0536

    Abstract: A missile comprises a propulsion system, a passageway (1) for delivering air to the propulsion system and a ducting element (9) associated with the passageway (1). The ducting element (9) has a ducting surface for ducting air into the passageway (1), and the ducting element (9) is rotatable, about an axis (13) that is aligned, or more preferably co-axial, with the axis (19) of the passageway (1), from a stowed position in which the ducting surface is received in the passageway (1), to a deployed position in which the ducting surface protrudes from the passageway (1) to duct air into the passageway.

    Abstract translation: 导弹包括推进系统，用于将空气传送到推进系统的通道（1）和与通道（1）相关联的管道元件（9）。 管道元件（9）具有用于将空气引导到通道（1）中的管道表面，并且管道元件（9）可绕轴线（13）旋转，该轴线（13）与轴线 （1）的管道表面被收纳在通道（1）中的收起位置处的通道（19）到管道表面从通道（1）突出到管道空气进入通道的通道位置 。

    Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft
    79.
    发明公开
    Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft 审中-公开
    方法和用于自动启动装置，检索和操纵飞机盘旋

    公开(公告)号：EP2371715A2

    公开(公告)日：2011-10-05

    申请号：EP11159710.0

    申请日：2011-03-25

    Applicant: Aerovel Corporation

    Inventor： McGeer, Brian Theodore ,  Heavey, Robert Joseph ,  McMillan, Damon Lucas ,  Stafford, John William

    IPC: B64F1/02 ,  B64F1/04

    CPC classification number: B64F1/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/182 ,  B64D37/00 ,  B64F5/00

    Abstract: An aircraft capable of thrust-borne flight can be automatically retrieved, serviced, and launched using equipment suitable for use on a small vessel, or at a base with similarly limited space or irregular motion. For retrieval, the aircraft drops a tether, and pulls the tether at low relative speed into contact with a horizontal guide. The tether is pulled across the guide until the guide is captured by a hook or other end effector. The tether length is then adjusted as necessary, and the aircraft swings on the guide to hang in an inverted position. Translation of the tether along the guide then brings the aircraft to a docking carriage, in which the aircraft parks for servicing. For launch the carriage is swung upright, the end effector is released from the guide, and the aircraft thrusts into free flight. A full ground-handling cycle can thus be accomplished automatically with simple and economical apparatus. It can be used with low risk of damage, and requires only moderate accuracy in manual or automatic flight control.

    Abstract translation: 能够推力传飞行的飞机可以被自动检索，维修和使用适合于使用设备上的一个小容器推出，或者在具有类似的限制空间或不规则的运动的位置。 进行检索，飞机下降的系绳，并且拉动在低相对速度系绳与水平引导接触。 直到所述引导件通过钩或其它端部执行器中捕获的系绳横越导拉动。 然后系绳长度被调整为必要的，并且在引导飞机摆动到在倒置位置挂出。 沿导系绳的翻译，那么带来的飞机对接的马车，其中飞机公园进行维修。 对于发射架摆动直立，末端执行器从引导释放，飞机推力到自由飞行。 全地处理周期因此可以提供简单而经济的装置自动完成。 它可以与损坏的风险低一起使用，并且只需要在手动或自动飞行控制中等精度。

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