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    Airborne Launch of Inflatable Devices
    61.
    发明申请
    Airborne Launch of Inflatable Devices 审中-公开

    公开(公告)号：US20170355462A1

    公开(公告)日：2017-12-14

    申请号：US15621100

    申请日：2017-06-13

    Applicant: Raymond Hoheisel

    Inventor： Raymond Hoheisel

    IPC: B64D1/12 ,  B64B1/62 ,  B64B1/40 ,  B64D1/02

    CPC classification number: B64D1/12 ,  B64B1/40 ,  B64B1/64 ,  B64C2201/082 ,  B64C2201/101 ,  B64D17/02 ,  B64D17/38

    Abstract: Aspects described herein relate to an apparatus, system, and method for the airborne launch of inflatable, lighter-than-air devices from aircraft. In some instances, a container comprising a drag parachute and a main parachute assembly may be deployed from an aircraft. Drag forces on the container may cause the drag parachute to be expelled from the container. Drag forces on the drag parachute may cause the main parachute assembly to be expelled from the container. The main parachute assembly may include a canopy with an opening and a release channel connecting the opening with the container. The container may further include a balloon inflation mechanism, which may be used to inflate one or more balloon envelopes. The one or more balloon envelopes, after being inflated, may be configured to be released from the container, traverse the release channel, and exit the main parachute assembly through the opening.

    Buoyant aerial vehicle
    62.
    发明授权
    Buoyant aerial vehicle 有权

    公开(公告)号：US09802691B2

    公开(公告)日：2017-10-31

    申请号：US15322008

    申请日：2016-06-15

    Applicant: Kohei Nakamura

    Inventor： Kohei Nakamura

    IPC: B64B1/30 ,  B64B1/58 ,  B64C39/02 ,  B64C25/06

    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: A buoyant aerial vehicle includes 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, and a horizontal propulsion propeller which provides horizontal propulsive force The buoyant vehicle body is configured with flotation chambers and connecting portions. The flotation chambers are arranged at positions point-symmetric with respect to a center of the buoyant vehicle body. Central portions of the flotation chambers are bulged in a side view and the connecting portions connect the flotation chambers. The connecting portions are formed in a flat shape thinner than the central portions of the flotation chambers such that wind passages along which the air flows are formed on the connecting portions, and the wind passages are oriented in at least two directions in the plan view.

    AIRSHIP WITH A CONTROLLED VARIABLE PROFILE
    67.
    发明申请
    AIRSHIP WITH A CONTROLLED VARIABLE PROFILE 有权
    具有可控变量轮廓的航空

    公开(公告)号：US20140054421A1

    公开(公告)日：2014-02-27

    申请号：US14004784

    申请日：2012-03-07

    Applicant: Alain Bernard

    Inventor： Alain Bernard

    IPC: B64B1/58

    CPC classification number: B64B1/58 ,  B64B1/04 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101

    Abstract: The invention relates to an airship comprising a flexible envelope having at least one adjustment region provided with two longitudinal adjustment elements mounted in opposition and mobile in relation to each other between a maximum distancing position and a minimum distancing position, the two longitudinal adjustment elements being connected to each other by a group comprising a plurality of cables crossing the inner space of the envelope, each of the cables cooperating with a plurality or tightening points provided along each longitudinal element. The cables are connected to at least one tightening module that can exert a tightening or loosening action on the cables and thereby bring the longitudinal adjustment elements closer together or move them further away.

    Abstract translation: 本发明涉及一种飞艇，其包括具有至少一个调节区域的至少一个调节区域，该调节区域设置有两个纵向调整元件，两个纵向调节元件相对于彼此安装，并且在最大间距位置和最小间距位置之间相对移动，两个纵向调节元件连接 通过包括穿过信封的内部空间的多个电缆的组彼此相互联系，每个电缆与沿着每个纵向元件设置的多个或紧固点配合。 电缆连接到至少一个可在电缆上施加紧固或松动的紧固模块，从而使纵向调节元件更靠近在一起或将它们移开。

    LIGHTER-THAN-AIR SYSTEMS, METHODS, AND KITS FOR OBTAINING AERIAL IMAGES
    68.
    发明申请
    LIGHTER-THAN-AIR SYSTEMS, METHODS, AND KITS FOR OBTAINING AERIAL IMAGES 有权
    用于获取空中影像的照明系统，方法和工具

    公开(公告)号：US20130299628A1

    公开(公告)日：2013-11-14

    申请号：US13942964

    申请日：2013-07-16

    Applicant: John Ciampa

    Inventor： John Ciampa ,  Bertrand Dano

    IPC: B64B1/02

    CPC classification number: B64B1/62 ,  B64B1/02 ,  B64B1/08 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/146 ,  B64D47/08 ,  G05D1/0094

    Abstract: Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/or descent of a lighter-than-air system are described. In addition, various structural arrangements of lighter-than-air systems for accomplishing planned ascent, drift, and/or descent and obtaining aerial images are described.

    Abstract translation: 描述了用于获取空中图像的比空气系统更轻的方法和套件。 例如，描述了用于确定轻于空气系统的计划上升，漂移和/或下降的各种方法。 此外，描述了用于实现计划上升，漂移和/或下降并获得空中图像的轻于空气系统的各种结构布置。

    APPARATUS AND SYSTEM FOR PROVIDING SURVEILLANCE OF AN AREA OR A SPACE
    69.
    发明申请
    APPARATUS AND SYSTEM FOR PROVIDING SURVEILLANCE OF AN AREA OR A SPACE 审中-公开
    用于提供区域或空间监视的装置和系统

    公开(公告)号：US20100270425A1

    公开(公告)日：2010-10-28

    申请号：US12449872

    申请日：2009-08-31

    Applicant: Yonatan Zur

    Inventor： Yonatan Zur

    IPC: B64B1/50 ,  B64B1/40 ,  B64B1/42 ,  F42B4/08

    CPC classification number: B64B1/40 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/201 ,  G08B13/19632

    Abstract: The present invention is an apparatus and system for providing surveillance of an area or a space. According to some embodiments of the present invention there may be provided a housing containing a deployable and inflatable surveillance balloon, which balloon may elevate and/or support a surveillance payload including one or more sensor assemblies. Data collected by the sensors may be transmitted to a user interface which may display the data to a user.

    Abstract translation: 本发明是一种用于提供区域或空间的监视的装置和系统。 根据本发明的一些实施例，可以提供一种容纳可部署和可充气的监视气球的壳体，所述气囊可以提升和/或支撑包括一个或多个传感器组件的监视有效载荷。 由传感器收集的数据可以被发送到可以向用户显示数据的用户界面。

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