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    Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
    52.
    发明授权
    Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion 有权
    用于发射无人机的方法和装置，包括在发射期间可释放地夹持飞行器并制动随后的抓地力

    公开(公告)号：US07165745B2

    公开(公告)日：2007-01-23

    申请号：US10808725

    申请日：2004-03-24

    Applicant: Brian T. McGeer ,  Andreas H. von Flotow ,  Cory Roeseler

    Inventor： Brian T. McGeer ,  Andreas H. von Flotow ,  Cory Roeseler

    IPC: B64F1/06

    CPC classification number: B64F1/06 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/084 ,  B64C2201/104 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/165

    Abstract: Methods and apparatuses for launching unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be launched from an apparatus that includes a launch carriage that moves along a launch guide. The carriage can accelerate when portions of the carriage and/or the launch guide move relative to each other. A gripper carried by the launch carriage can have at least one grip portion in contact with the aircraft while the launch carriage accelerates along the launch axis. The at least one grip portion can move out of contact with the aircraft as the launch carriage decelerates, releasing the aircraft for takeoff. A brake can arrest the motion of the gripper after launch.

    Abstract translation: 描述了发射无人机和其他飞行装置或射弹的方法和装置。 在一个实施例中，飞行器可以从包括沿发射导向装置移动的发射台的装置发射。 当滑架和/或发射引导件的部分相对于彼此移动时，托架可以加速。 由发射托架携带的夹具可以具有至少一个与飞行器接触的抓握部分，同时发射托架沿着发射轴加速。 当发射架减速时，至少一个把手部分可以与飞行器脱离接触，释放飞机起飞。 制动器可以在发射后阻止夹具的运动。

    Bendable wing for micro air vehicle
    53.
    发明申请
    Bendable wing for micro air vehicle 有权
    微型飞机的弯曲翼

    公开(公告)号：US20060284005A1

    公开(公告)日：2006-12-21

    申请号：US11510013

    申请日：2006-08-25

    Applicant: Peter Ifju ,  Kyu-Ho Lee ,  Roberto Albertani ,  Shawn Mitryk ,  Frank Boria ,  Mujahid Abdulrahim

    Inventor： Peter Ifju ,  Kyu-Ho Lee ,  Roberto Albertani ,  Shawn Mitryk ,  Frank Boria ,  Mujahid Abdulrahim

    IPC: B64C3/56 ,  B64C3/00

    CPC classification number: B64C39/028 ,  A63H27/007 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/201

    Abstract: A micro air vehicle having a bendable wing enabling the micro air vehicle to fly. The bendable wing may be bent downwards so that the wingspan may be reduced for storing the micro air vehicle. The bendable wing may be formed from one or more layers of material, and the wing may have a camber such that a concave surface of the wing faces downward. The wing may substantially resist flexing upwards and may transfer uplift forces to a central body of the micro air vehicle. In addition, the wing may be bent severely downwards by applying a force to tips of the wing. The micro air vehicle is capable of being stored in a small cylindrical tube and may be deployed from the tube by simply releasing the micro air vehicle from the tube.

    Abstract translation: 具有能够使微型飞行器飞行的可弯曲翼的微型飞行器。 可弯曲翼可以向下弯曲，使得翼展可以减小以存储微型飞行器。 可弯曲翼可以由一层或多层材料形成，并且翼可以具有弯曲，使得翼的凹面朝向下方。 机翼可以基本上抵抗向上弯曲并且可以将提升力传递到微型飞行器的中心体。 此外，机翼可能通过对机翼的尖端施加力而严重地向下弯曲。 微型飞行器能够存储在小圆柱形管中，并且可以通过从管中简单地释放微型飞行器而从管展开。

    METHODS AND APPARATUSES FOR LAUNCHING, CAPTURING, AND STORING UNMANNED AIRCRAFT, INCLUDING A CONTAINER HAVING A GUIDE STRUCTURE FOR AIRCRAFT COMPONENTS
    56.
    发明申请
    METHODS AND APPARATUSES FOR LAUNCHING, CAPTURING, AND STORING UNMANNED AIRCRAFT, INCLUDING A CONTAINER HAVING A GUIDE STRUCTURE FOR AIRCRAFT COMPONENTS 有权
    用于发射，捕获和存储未经规定的飞机的方法和装置，包括具有航空器组件指导结构的集装箱

    公开(公告)号：US20060175463A1

    公开(公告)日：2006-08-10

    申请号：US11269395

    申请日：2005-11-08

    Applicant: Brian McGeer

    Inventor： Brian McGeer

    IPC: B64F5/00

    CPC classification number: B64F1/04 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/02 ,  B64F1/06

    Abstract: Methods and apparatuses for launching, capturing, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be assembled from a container with little or no manual engagement by an operator. The container can include a guide structure to control motion of the aircraft components. The aircraft can be launched from an apparatus that includes an extendable boom. The boom can be extended to deploy a recovery line to capture the aircraft in flight. The aircraft can then be returned to its launch platform, disassembled, and stored in the container, again with little or no direct manual contact between the operator and the aircraft.

    Abstract translation: 描述了用于发射，捕获和存储无人机和其他飞行装置或射弹的方法和装置。 在一个实施例中，飞行器可以由操作者很少或没有手动接合的容器组装。 容器可以包括用于控制飞机部件的运动的引导结构。 飞机可以从包括可伸缩吊杆的装置发射。 可以扩展繁荣部署一个恢复线，以便在飞行中捕获飞机。 飞机然后可以返回到其发射平台，拆卸并存储在容器中，再次与操作员和飞机之间的很少或没有直接的手动接触。

    Dual wing-pair air vehicle
    57.
    发明申请
    Dual wing-pair air vehicle 失效
    双翼对机动车

    公开(公告)号：US20050178896A1

    公开(公告)日：2005-08-18

    申请号：US10774653

    申请日：2004-02-04

    Applicant: David Cylinder

    Inventor： David Cylinder

    IPC: B64C33/02 ,  B64C39/02 ,  B64C39/08

    CPC classification number: B64C39/08 ,  B64C33/02 ,  B64C39/024 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146

    Abstract: A vehicle for flying and having a forward portion and a rearward portion opposite the forward. The vehicle includes a first pair of wings arranged at the forward portion of the vehicle, a second pair of wings arranged at the rearward portion of the vehicle, and a support structure. The support structure is connected to the forward pair of wings and connected to the rearward pair of wings, the support structure being arranged to drive the forward pair of wings alternately toward each other and apart and drives the second pair of wings alternately toward each other and apart.

    Abstract translation: 用于飞行并具有向前部分和与向前相对的后部的车辆。 车辆包括布置在车辆前部的第一对翼，布置在车辆后部的第二对翼和支撑结构。 支撑结构连接到前一对翼部并且连接到后一对翼部，支撑结构被布置成相互交替地驱动前一对翼片并分开，并且将第二对翼片彼此交替地驱动， 分开

    Bendable wing for micro air vehicle
    59.
    发明申请
    Bendable wing for micro air vehicle 审中-公开
    微型飞机的弯曲翼

    公开(公告)号：US20040245393A1

    公开(公告)日：2004-12-09

    申请号：US10731777

    申请日：2003-12-09

    Applicant: University of Florida

    Inventor： Peter Ifju ,  Kyu-Ho Lee ,  Roberto Albertani ,  Shawn J. Mitryk ,  Frank J. Boria ,  Mujahid Abdulrahim

    IPC: B64C001/00

    CPC classification number: B64C39/028 ,  A63H27/007 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/201

    Abstract: A micro air vehicle having a bendable wing enabling the micro air vehicle to fly. The bendable wing may be bent downwards so that the wingspan may be reduced for storing the micro air vehicle. The bendable wing may be formed from one or more layers of material, and the wing may have a camber such that a concave surface of the wing faces downward. The wing may substantially resist flexing upwards and may transfer uplift forces to a central body of the micro air vehicle. In addition, the wing may be bent severely downwards by applying a force to tips of the wing. The micro air vehicle is capable of being stored in a small cylindrical tube and may be deployed from the tube by simply releasing the micro air vehicle from the tube.

    Abstract translation: 具有能够使微型飞行器飞行的可弯曲翼的微型飞行器。 可弯曲翼可以向下弯曲，使得翼展可以减小以存储微型飞行器。 可弯曲翼可以由一层或多层材料形成，并且翼可以具有弯曲，使得翼的凹面朝向下方。 机翼可以基本上抵抗向上弯曲并且可以将提升力传递到微型飞行器的中心体。 此外，机翼可能通过对机翼的尖端施加力而严重地向下弯曲。 微型飞行器能够存储在小圆柱形管中，并且可以通过从管中简单地释放微型飞行器而从管展开。

    Virtual sensor mast
    60.
    发明申请
    Virtual sensor mast 有权
    虚拟传感器桅杆

    公开(公告)号：US20040167682A1

    公开(公告)日：2004-08-26

    申请号：US10639267

    申请日：2003-08-12

    Applicant: Lockheed Martin Corporation

    Inventor： Michael S. Beck ,  Wendell H. Chun ,  Jon T. Stinchcomb

    IPC: G06F017/00

    CPC classification number: B64C39/028 ,  B60K7/0007 ,  B60K17/046 ,  B60K17/356 ,  B60T1/062 ,  B62D61/10 ,  B62D61/12 ,  B64B1/50 ,  B64C27/20 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/162 ,  B64C2201/208

    Abstract: A virtual sensor mast for a ground vehicle and a method for operating a ground vehicle using a virtual sensor mast are disclosed. The virtual sensor mast includes an unmanned airborne vehicle capable of lifting itself from the ground vehicle upon deployment therefrom; a sensor suite mounted to the unmanned airborne vehicle; and a tether between the unmanned airborne vehicle and the ground vehicle over which the sensor suite is capable of communicating sensed data upon deployment. The method includes elevating a tethered unmanned airborne vehicle from the ground vehicle to a predetermined height; sensing environmental conditions surrounding the ground vehicle; and terminating the deployment.

    Abstract translation: 公开了一种用于地面车辆的虚拟传感器桅杆和使用虚拟传感器桅杆操作地面车辆的方法。 虚拟传感器桅杆包括能够在其从其展开时从地面车辆提升自身的无人机载机; 安装在无人机载体上的传感器套件; 以及在无人驾驶的机载车辆和地面车辆之间的系绳，传感器套件能够在部署时传送感测数据。 该方法包括：将有系带的无人机载体从地面车辆升高到预定的高度; 感测地面车辆周围的环境条件; 并终止部署。

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