METHODS AND SYSTEMS FOR DETERMINING FLEET TRAJECTORIES TO SATISFY A SEQUENCE OF COVERAGE REQUIREMENTS
    53.
    发明公开
    METHODS AND SYSTEMS FOR DETERMINING FLEET TRAJECTORIES TO SATISFY A SEQUENCE OF COVERAGE REQUIREMENTS 审中-公开
    FOR运动轨迹的检测方法和系统,以满足覆盖要求的序列

    公开(公告)号:EP2939372A4

    公开(公告)日:2016-08-24

    申请号:EP13869702

    申请日:2013-11-21

    Applicant: GOOGLE INC

    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: 提供了对车队的车辆确定性采矿轨迹的方法和系统。 在一个实施例中,一种方法包括:接收在一个或多个车辆的初始位置,以及接收的覆盖要求的序列为一个区域和时间相关联的时间段。 的区域可以被划分成路标的多元性和所述时间段可被划分成相的复数。 因此,该方法包括用于每个一个或多个相以及至少一个界标respectivement,一组开始从车辆中的相位可能到达respectivement界标的地标确定性挖掘。 该方法还包括确定挖掘其中respectivement里程碑意义的基础上,覆盖要求的顺序和设定开始的一个或多个阶段的地标和至少一个respectivement里程碑意义的一个或多个阶段中没有车辆shoulderstand出行。

    DRONE HAUTE ALTITUDE
    55.
    发明公开
    DRONE HAUTE ALTITUDE 有权
    DROHNEFÜRGROSSEHÖHEN

    公开(公告)号:EP2996937A1

    公开(公告)日:2016-03-23

    申请号:EP14732257.2

    申请日:2014-05-09

    Applicant: Ridengineering

    Inventor: JONIOT, Jacques

    Abstract: The invention relates to a drone comprising: two contra-rotating annular propellers (2, 4) defining a plane therebetween which is referred to as an equatorial plane and is assumed to be horizontal, means for driving the propellers, a load arranged below the equatorial plane, and means (20) for moving the load relative to the equatorial plane, an enclosure referred to as an upper enclosure (6) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially above the equatorial plane, and an enclosure referred to as a lower enclosure (8) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially below the equatorial plane, the load being placed inside the lower enclosure (8).

    Abstract translation: 无人机技术领域本发明涉及一种无人机,包括:两个反向转动的环形螺旋桨(2,4),在其间限定一个平面,被称为赤道平面,并被假设为水平的,用于驱动螺旋桨的装置,设置在赤道 平面和用于相对于赤道平面移动负载的装置(20),被称为上部外壳(6)的外壳,其填充有密度小于1且基本上位于赤道平面上方的气体或气体混合物 ,以及被称为下部外壳(8)的外壳,其中填充有密度小于1且基本上位于赤道平面下方的气体或气体混合物,负载被放置在下部外壳内。

    Fire control process and device
    56.
    发明公开
    Fire control process and device 审中-公开
    Brandbekämpfungsverfahrenund Vorrichtung

    公开(公告)号:EP2860110A1

    公开(公告)日:2015-04-15

    申请号:EP13188262.3

    申请日:2013-10-11

    Inventor: Ghio, Marco

    Abstract: A fire (1 a) control device(1) is provided comprising at least one aerostat (10) comprising a casing (11) defining an air chamber (11a) suitable to contain a gas lighter than air, a tank (12) defining a collection space (12a) for extinguisher fluid (10a), an identification device (13) suitable to identify when the aerostat (10) is above the fire (1 a) and a valve (14) suitable to permit dropping of the extinguisher fluid (10a) when said at least one aerostat (10) finds itself above said fire (1a).

    Abstract translation: 提供了一种火(1a)控制装置(1),包括至少一个空气净化器(10),其包括限定适于容纳比空气轻的气体的空气室(11a)的壳体(11),限定 用于灭火器流体(10a)的收集空间(12a),适于识别空气处理器(10)何时高于火焰(1a)的识别装置(13)和适于允许灭火器流体滴落的阀(14) 10a)当所述至少一个空气净化器(10)发现自身位于所述火(1a)上方时。

    AÉROSTAT DIRIGEABLE À PROFIL VARIABLE COMMANDÉ
    57.
    发明公开
    AÉROSTAT DIRIGEABLE À PROFIL VARIABLE COMMANDÉ 有权
    飞机,轻于空气中的装置,用于改变外壳的形状

    公开(公告)号:EP2686237A1

    公开(公告)日:2014-01-22

    申请号:EP12711224.1

    申请日:2012-03-07

    Applicant: Voliris

    Inventor: BERNARD, Alain

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

    Abstract: The invention relates to an airship (1) comprising a flexible envelope (2) having at least one adjustment region (4) provided with two longitudinal adjustment elements (5, 6) 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 (5, 6) being connected to each other by a group comprising a plurality of cables (7, 7', 8, 8', 9, 9') crossing the inner space (3) of the envelope, each of the cables (7, 7', 8, 8', 9, 9') cooperating with a plurality of tightening points (10) provided along each longitudinal element. The cables are connected to at least one tightening module (20) that can exert a tightening or loosening action on the cables and thereby bring the longitudinal adjustment elements (20) closer together or move them further away.

    Abstract translation: 本发明涉及在飞艇,其包括具有设置有最大疏远位置和最小疏远位置之间安装在对立和移动在相对于彼此的两个纵向调节元件的至少一个调节区的柔性封套,所述两个纵向调节元件被连接 海誓山盟由一组包括电缆交叉的包络线的内部空间的复数,每根电缆与沿着每个纵向构件提供多个或紧固点协作。 该电缆连接到至少一个紧固模块也能对电缆的紧固或松开的动作,并由此带来的纵向调节元件靠近在一起或furtheraway移动它们。

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