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    Apparatus to lift and fill a balloon
    74.
    发明授权
    Apparatus to lift and fill a balloon 有权
    用于提升和填充气球的装置

    公开(公告)号：US09266599B1

    公开(公告)日：2016-02-23

    申请号：US14546412

    申请日：2014-11-18

    Applicant: Google Inc.

    Inventor： Daniel Ratner

    IPC: B64B1/62

    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.

    Abstract translation: 本公开的方面涉及填充和提升高空气球。 例如，用于提升和填充具有气球外壳的球囊的一个示例性系统包括用于气球外壳的装置。 该装置包括负载线，填充管，其具有嵌套在负载线内的中空部分，以及连接到填充管和负载线的端接构件。 负载线被配置为在充气期间抬起气囊外壳。 填充管延伸穿过负载管线并且构造成允许提升气体通过中空部分。 终端构件被配置为与球囊封套中的开口配合，使得提升气体可以穿过填充管的中空部分并进入气囊封套中的开口。

    Methods and systems for determining fleet trajectories to satisfy a sequence of coverage requirements
    76.
    发明授权
    Methods and systems for determining fleet trajectories to satisfy a sequence of coverage requirements 有权
    确定车队轨迹以满足覆盖要求序列的方法和系统

    公开(公告)号：US09014957B2

    公开(公告)日：2015-04-21

    申请号：US13730867

    申请日：2012-12-29

    Applicant: Google Inc.

    Inventor： Keith Allen Bonawitz ,  Adrien Treuille

    IPC: G06Q10/00 ,  G08G5/00 ,  G08G1/00

    CPC classification number: G08G5/0034 ,  B64B1/58 ,  B64B1/60 ,  B64C2201/022 ,  B64C2201/122 ,  G05D1/104 ,  G06Q10/047 ,  G08G1/20 ,  G08G1/202 ,  G08G5/0043 ,  G08G5/0069 ,  G08G5/0091 ,  H04B7/18504

    Abstract: Methods and systems for determining trajectories for vehicles of a fleet of vehicles are provided. In one example, a method comprises receiving an initial location of one or more vehicles, and receiving a sequence of coverage requirements for a region and an associated period of time. The region may be divided into a plurality of landmarks and the period of time may be divided into a plurality of phases. The method also comprises determining for each of one or more phases and at least one respective landmark, a set of starting landmarks from which a vehicle could reach the respective landmark during the phase. The method further comprises determining which respective landmark that the vehicle should travel to during the one or more phases based on the sequence of coverage requirements and the set of starting landmarks for the one or more phases and the at least one respective landmark.

    Abstract translation: 提供了用于确定车队车辆轨迹的方法和系统。 在一个示例中，一种方法包括接收一个或多个车辆的初始位置，以及接收一个区域和相关时间段的覆盖要求序列。 该区域可以被划分为多个地标，并且该时间段可以被分成多个阶段。 该方法还包括确定一个或多个相位中的每一个以及至少一个相应的标记，一组起始地标，在该阶段期间车辆可从该起始地标到达相应的地标。 所述方法还包括基于所述一个或多个相位和所述至少一个相应地标的覆盖要求序列和所述一组起始地标来确定所述车辆在所述一个或多个阶段期间应该行进到哪个相应的标记。

    Methods and Systems for Determining Fleet Trajectories to Satisfy a Sequence of Coverage Requirements
    77.
    发明申请
    Methods and Systems for Determining Fleet Trajectories to Satisfy a Sequence of Coverage Requirements 有权
    确定舰队轨迹以满足覆盖要求序列的方法和系统

    公开(公告)号：US20140188377A1

    公开(公告)日：2014-07-03

    申请号：US13730867

    申请日：2012-12-29

    Applicant: Google Inc.

    Inventor： Keith Allen Bonawitz ,  Adrien Treuille

    IPC: G08G5/00

    CPC classification number: G08G5/0034 ,  B64B1/58 ,  B64B1/60 ,  B64C2201/022 ,  B64C2201/122 ,  G05D1/104 ,  G06Q10/047 ,  G08G1/20 ,  G08G1/202 ,  G08G5/0043 ,  G08G5/0069 ,  G08G5/0091 ,  H04B7/18504

    Abstract: Methods and systems for determining trajectories for vehicles of a fleet of vehicles are provided. In one example, a method comprises receiving an initial location of one or more vehicles, and receiving a sequence of coverage requirements for a region and an associated period of time. The region may be divided into a plurality of landmarks and the period of time may be divided into a plurality of phases. The method also comprises determining for each of one or more phases and at least one respective landmark, a set of starting landmarks from which a vehicle could reach the respective landmark during the phase. The method further comprises determining which respective landmark that the vehicle should travel to during the one or more phases based on the sequence of coverage requirements and the set of starting landmarks for the one or more phases and the at least one respective landmark.

    Abstract translation: 提供了用于确定车队车辆轨迹的方法和系统。 在一个示例中，一种方法包括接收一个或多个车辆的初始位置，以及接收一个区域和相关时间段的覆盖要求序列。 该区域可以被划分为多个地标，并且该时间段可以被分成多个阶段。 该方法还包括确定一个或多个相位中的每一个以及至少一个相应的标记，一组起始地标，在该阶段期间车辆可从该起始地标到达相应的地标。 所述方法还包括基于所述一个或多个相位和所述至少一个相应地标的覆盖要求序列和所述一组起始地标来确定所述车辆在所述一个或多个阶段期间应该行进到哪个相应的标记。

    AIRSHIP WITH A CONTROLLED VARIABLE PROFILE
    78.
    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
    79.
    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。

    Lighter-than-air vertical load lifting system
    80.
    发明授权
    Lighter-than-air vertical load lifting system 有权
    轻型立式起重系统

    公开(公告)号：US08141814B2

    公开(公告)日：2012-03-27

    申请号：US11945047

    申请日：2007-11-26

    Applicant: Richard L. Kulesha

    Inventor： Richard L. Kulesha

    IPC: B64B1/34

    CPC classification number: B64B1/06 ,  B64B1/08 ,  B64C2201/022

    Abstract: An aerial load lifting system features a non-rigid or blimp-type dirigible providing a lighter-than-air envelope that is placed within a structural shell. The system is designed so that the envelope provides essentially neutral buoyancy for the structure, leaving only the cargo weight to be lifted by the rotors. The structural shell supports the engine, fuel tank, rotors, and transmission system that power the lift and vectoring of the aircraft, in addition to supporting the cargo load. The structural shell transfers the weight of the load directly to the location of the rotors, thus avoiding stress on the envelope.

    Abstract translation: 一种空中负载提升系统具有非刚性或微型飞行器，提供放置在结构外壳内的轻于空气的封套。 该系统的设计使得外壳为结构提供基本上中性的浮力，只留下货物由转子提升。 结构外壳还支持发动机，燃油箱，转子和传动系统，以支持飞机的起重和矢量化，以及支撑货物载荷。 结构外壳将负载的重量直接转移到转子的位置，从而避免了信封上的压力。

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