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    Apparatus to lift and fill a balloon
    123.
    发明授权
    Apparatus to lift and fill a balloon 有权

    公开(公告)号：US09849962B2

    公开(公告)日：2017-12-26

    申请号：US15480582

    申请日：2017-04-06

    Applicant: X Development LLC

    Inventor： Daniel Ratner

    IPC: B64B1/62 ,  B64B1/40

    CPC classification number: B64B1/62 ,  B64B1/40 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/122

    Abstract: Aspects of the disclosure relate to filling and lifting high altitude balloons. For instance, one example system for lifting and filling a balloon having a balloon envelope includes an apparatus for use with the balloon envelope. The apparatus includes a load line, a fill tube having a hollow portion nested within the load line and a termination member attached to the fill tube and load line. The load line is configured to lift the balloon envelope during inflation. The fill tube extends through the load line and is configured to allow lift gas to pass through the hollow portion. The termination member is configured to mate with an opening in the balloon envelope so that lift gas can pass through the hollow portion of the fill tube and into the opening in the balloon envelope.

    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM
    126.
    发明申请
    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM 审中-公开

    公开(公告)号：US20170205536A1

    公开(公告)日：2017-07-20

    申请号：US15326764

    申请日：2015-07-17

    Applicant: ALTEC S.P.A.

    Inventor： Ivano MUSSO

    IPC: G01W1/08 ,  H04N5/232 ,  B63B35/00 ,  H04N5/225 ,  B64D1/12 ,  B64D47/08 ,  G01S13/95 ,  H04N7/18

    CPC classification number: G01W1/08 ,  B63B35/00 ,  B64C2201/022 ,  B64C2201/125 ,  B64C2201/127 ,  B64D1/12 ,  B64D47/08 ,  G01C11/02 ,  G01S13/953 ,  G01S13/956 ,  G03B15/006 ,  G03B17/08 ,  G03B17/561 ,  G05D1/0094 ,  H04N5/2252 ,  H04N5/23238 ,  H04N7/18

    Abstract: Platform (100; 200, 200′, 200″) configured to acquire images and/or radio signals and to be carried by lightweight aviation aircrafts, characterised in that it comprises housing means (1, 3; 22, 201, 202, 203, 31) that houses one or more acquisition sensors selected from the group comprising or consisting of cameras (5; 51; 32) configured to acquire still and/or moving images and radio signal receivers (62; 34) configured to acquire radio signals, said housing means (1, 3; 22, 201, 202, 203, 31) being configured to be coupled to a light aviation aircraft (540), said one or more acquisition sensors (5; 51; 32; 62; 34) being connected to processing means (6; 23) configured to receive sensing data from a position and motion sensing unit (10; 230) coupled to said one or more acquisition sensors (5; 51; 32; 62; 34), said processing means (6; 23) being configured to control and/or program, on the basis of the received sensing data, each acquisition sensor (5; 51; 32; 62; 34) so as to enable the same to acquire images and/or radio signals when such acquisition sensor (5; 51; 32; 62; 34) is in a determined position and is subject to oscillations having a velocity that is not larger in absolute value than a maximum oscillation velocity value, whereby a rate of variation of an actual aiming of such acquisition sensor (5; 51; 32; 62; 34) is not larger in absolute value than a respective maximum value of rate of variation of offset with respect to an ideal aiming at a target, so as to ensure focusing of such acquisition sensor (5; 51; 32; 62; 34) on an aimed area.

    Ground terminal and UAV beam pointing in an unmanned aerial vehicle (UAV) for network access
    127.
    发明授权
    Ground terminal and UAV beam pointing in an unmanned aerial vehicle (UAV) for network access 有权

    公开(公告)号：US09660718B2

    公开(公告)日：2017-05-23

    申请号：US15260049

    申请日：2016-09-08

    Applicant: UBIQOMM LLC

    Inventor： Ahmad Jalali ,  Viktor Filiba

    IPC: H04B7/185 ,  H04W64/00 ,  H04W24/10 ,  H04W16/28 ,  B64C39/02 ,  H04W84/00

    CPC classification number: H04B7/18504 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/122 ,  H04W16/28 ,  H04W24/10 ,  H04W64/006 ,  H04W84/005

    Abstract: Systems and methods for detecting an unmanned aerial vehicle (UAV). Network access (for example, to the Internet) may be provided by detecting a UAV and fixing one or more beams from one or more ground terminals to the UAV. In one embodiment, the detection of a UAV includes forming and pointing beams from a ground terminal and ground gateways toward the UAV. The ground terminal may be configured to autonomously steer its antenna beam during initial installation to detect the reference signal from a UAV. In one variant, the ground terminals are steered to more finely track the position of the UAV based on a signal quality metric such as received signal strength and the UAV real-time position location coordinates. In one embodiment, the ground terminal antenna is initially manually pointed toward the UAV, and thereafter allowed to automatically steer to track the position of the UAV. In another embodiment the UAV antenna is steered toward a ground terminal using signal quality received from the ground terminal and real-time position coordinates and orientation of the UAV.

    BUOYANT AERIAL VEHICLE
    128.
    发明申请
    BUOYANT AERIAL VEHICLE 审中-公开

    公开(公告)号：US20170137104A1

    公开(公告)日：2017-05-18

    申请号：US15322008

    申请日：2016-06-15

    Applicant: Kohei NAKAMURA

    Inventor： Kohei NAKAMURA

    IPC: B64B1/30 ,  B64C39/02 ,  B64C25/06 ,  B64C27/08

    CPC classification number: B64B1/30 ,  B64B1/58 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/127

    Abstract: Provided is a buoyant aerial vehicle which can secure high safety by reducing the risk of crashing, and which can facilitate control of movement by suppressing the influence of wind and exhibit high mobility capability. The buoyant aerial vehicle is configured by including: a buoyant vehicle body in which gas having a specific gravity smaller than air is hermetically filled; a vertical propulsion propeller which provides vertical propulsive force to the buoyant vehicle body; and a horizontal propulsion propeller which provides horizontal propulsive force to the buoyant vehicle body, and is configured such that the buoyant vehicle body has horizontal wind passages formed in at least two directions, and has outer peripheral edges each formed into an acute angle in side view.

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