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    Lightweight air vehicle and pneumatic launcher
    33.
    发明授权
    Lightweight air vehicle and pneumatic launcher 有权
    轻型机动车和气动发射器

    公开(公告)号：US07584925B2

    公开(公告)日：2009-09-08

    申请号：US11877201

    申请日：2007-10-23

    Applicant: Stephen W. Miller ,  Matthew Velazquez

    Inventor： Stephen W. Miller ,  Matthew Velazquez

    IPC: B64C3/56 ,  B64F1/04

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06

    Abstract: A portable unmanned air vehicle and launcher system that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.

    Abstract translation: 一种便携式无人机和发射系统，包括具有压力管的可折叠无人机; 用于发射气体的发射气藏; 操作地连接到发射气体储存器并具有位于空中载体的压力管中的自由端的发射管; 位于发射管内的自由活塞; 和自由活塞止挡件，以防止自由活塞离开发射管。 发射气体储存器中的发射气体的第一部分被释放到发射管中，并且将自由活塞从初始位置推动到自由活塞由自由活塞停止的终止位置。

    Motion assisting apparatus
    35.
    发明授权
    Motion assisting apparatus 失效
    运动辅助装置

    公开(公告)号：US07204455B2

    公开(公告)日：2007-04-17

    申请号：US10481944

    申请日：2002-06-28

    Applicant: Peter Logan Sinclair

    Inventor： Peter Logan Sinclair

    IPC: B64C33/02

    CPC classification number: A63H31/08 ,  A63H27/008 ,  B64C33/02 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/203

    Abstract: A drive assembly for use with a mechanical flying or walking device comprises an articulated member (7) having first and second portions (7a, 7b) arranged such that the portions move relative to each other, and a drive mechanism (9) for imparting motion to the articulated member. The drive mechanism (9) comprises: a drive member for imparting a cyclic motion on the articulated member, and a control member for controlling, in a predetermined manner, the relative position of the first and second portions during each cycle of the cyclic motion of the articulated member. In the case of a mechanical flying device, two such drive assemblies may be provided, the articulated member of each assembly forming a wing.

    Abstract translation: 一种与机械飞行或步行装置一起使用的驱动组件包括铰接构件（7），其具有被布置成使得所述部分相对于彼此移动的第一和第二部分（7a，7b）以及驱动机构（9） 向铰接构件施加运动。 驱动机构（9）包括：驱动构件，用于在铰接构件上施加循环运动;以及控制构件，用于以预定方式控制第一和第二部分在循环运动的每个循环期间的相对位置 铰接构件。 在机械飞行装置的情况下，可以设置两个这样的驱动组件，每个组件的铰接构件形成翼。

    Lightweight air vehicle and pneumatic launcher
    36.
    发明申请
    Lightweight air vehicle and pneumatic launcher 有权
    轻型机动车和气动发射器

    公开(公告)号：US20050274845A1

    公开(公告)日：2005-12-15

    申请号：US10509659

    申请日：2004-02-19

    Applicant: Stephen Miller ,  Matthew Velazquez

    Inventor： Stephen Miller ,  Matthew Velazquez

    IPC: B64B20060101 ,  B64B1/00 ,  B64C3/56 ,  B64C39/02 ,  B64F1/04 ,  B64F1/06

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06

    Abstract: A portable unmanned air vehicle and launcher system is provided that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.

    Abstract translation: 提供了一种便携式无人驾驶飞行器和发射系统，其包括具有压力管的可折叠无人驾驶飞行器; 用于发射气体的发射气藏; 操作地连接到发射气体储存器并具有位于空中载体的压力管中的自由端的发射管; 位于发射管内的自由活塞; 和自由活塞止挡件，以防止自由活塞离开发射管。 发射气体储存器中的发射气体的第一部分被释放到发射管中，并且将自由活塞从初始位置推动到自由活塞由自由活塞停止的终止位置。

    SELF-ENCLOSED AIR VEHICLE
    38.
    发明申请
    SELF-ENCLOSED AIR VEHICLE 审中-公开

    公开(公告)号：US20180297704A1

    公开(公告)日：2018-10-18

    申请号：US16014766

    申请日：2018-06-21

    Applicant: GoPro, Inc.

    Inventor： Ryan Michael Goldstein

    IPC: B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/203

    Abstract: Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.

    Launching an unmanned aerial vehicle using a hand-held weapon
    40.
    发明授权
    Launching an unmanned aerial vehicle using a hand-held weapon 有权

    公开(公告)号：US09611054B2

    公开(公告)日：2017-04-04

    申请号：US14187846

    申请日：2014-02-24

    Applicant: AAI Corporation

    Inventor： Alexander D. Manasseh

    IPC: B64F1/04 ,  B64C39/02

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/203

    Abstract: A technique is directed to launching an unmanned aerial vehicle (UAV). The technique involves attaching a UAV launcher to a hand-held weapon, and installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon. The technique further involves activating the hand-held weapon to launch the UAV into flight from the UAV launcher. Since a user already may be carrying the hand-held weapon for firing ammunition, the user simply needs to further carry the UAV launcher and the UAV which, in some situations, can be packaged into an easy-to-carry container such as a backpack, a carrying case, and so on.

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