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    SYSTEM AND METHOD FOR PLACEMENT OF SENSORS THROUGH USE OF UNMANNED AERIAL VEHICLES
    31.
    发明申请
    SYSTEM AND METHOD FOR PLACEMENT OF SENSORS THROUGH USE OF UNMANNED AERIAL VEHICLES 审中-公开
    通过使用无人驾驶飞机放置传感器的系统和方法

    公开(公告)号：US20160232794A1

    公开(公告)日：2016-08-11

    申请号：US14716850

    申请日：2015-05-19

    Applicant: Usman Hafeez ,  David Mauer

    Inventor： Usman Hafeez ,  David Mauer

    IPC: G08G5/00 ,  B64C39/02

    CPC classification number: G08G5/0034 ,  B64C39/024 ,  B64C2201/00 ,  B64C2201/027 ,  B64C2201/12 ,  G01C21/20 ,  G05D1/104 ,  G08G5/0043 ,  G08G5/0069

    Abstract: The invention is directed toward a system and method for placing, activating, and testing sensors. The system comprises one or more server computers, one or more communication hubs, one or more unmanned aerial vehicles, and one or more sensors. The method comprises the steps of receiving geographic sensor placement locations, receiving sensor parameters, determining the geographic location of sensors, respectively sending location query signals to the unmanned aerial vehicles, respectively receiving location reply signals from the unmanned aerial vehicles, and calculating a geographic flight path for the unmanned aerial vehicles. The method also comprises calculating mission objectives and the energy needs of the unmanned aerial vehicles to complete the mission objectives. The method then determines the most efficient combination of unmanned aerial vehicles to complete the mission objectives and assigns the tasks to the unmanned aerial vehicles. The unmanned aerial vehicles place, activate, and test the sensors.

    Abstract translation: 本发明涉及用于放置，激活和测试传感器的系统和方法。 该系统包括一个或多个服务器计算机，一个或多个通信集线器，一个或多个无人驾驶飞行器以及一个或多个传感器。 该方法包括以下步骤：接收地理传感器放置位置，接收传感器参数，确定传感器的地理位置，分别向无人驾驶飞行器发送位置查询信号，分别接收来自无人机的位置应答信号，以及计算地理飞行 无人机的路径。 该方法还包括计算任务目标和无人机的能源需求，以完成任务目标。 然后，该方法确定无人机的最有效的组合来完成任务目标并将任务分配给无人驾驶飞行器。 无人驾驶飞行器放置，激活和测试传感器。

    LENTICULAR AIRSHIP
    36.
    发明申请
    LENTICULAR AIRSHIP 有权
    航空公司

    公开(公告)号：US20120160959A1

    公开(公告)日：2012-06-28

    申请号：US13342373

    申请日：2012-01-03

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/00

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

    Lenticular airship
    37.
    发明申请
    Lenticular airship 有权
    透镜飞艇

    公开(公告)号：US20080179454A1

    公开(公告)日：2008-07-31

    申请号：US11907883

    申请日：2007-10-18

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/06 ,  B64B1/08 ,  B64B1/12 ,  B64B1/24 ,  G05D1/08

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

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