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    SOLARKONZENTRATOR FÜR HOCHFLIEGENDE LEICHTBAUSTRUKTUR
    12.
    发明申请
    SOLARKONZENTRATOR FÜR HOCHFLIEGENDE LEICHTBAUSTRUKTUR 审中-公开
    太阳能聚光飙升结构轻巧

    公开(公告)号：WO2016034667A1

    公开(公告)日：2016-03-10

    申请号：PCT/EP2015/070129

    申请日：2015-09-03

    Applicant: AIRBUS DEFENCE AND SPACE GMBH

    Inventor： STEINWANDEL, Jürgen ,  STÜCKL, Stefan ,  STUHLBERGER, Johannes

    IPC: H01L31/054 ,  H01L31/0216

    CPC classification number: H01L31/0547 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/125 ,  B64D2211/00 ,  H01L31/02168 ,  Y02E10/52

    Abstract: Die Erfindung betrifft eine Vorrichtung 10 zur Versorgung einer hochfliegenden Leichtbaustruktur 60, insbesondere eines Stratosphären- oder Mesosphärenfluggeräts, mit elektrischer Energie unter Verwendung mindestens einer Solarzelle 48. Erfindungsgemäß ist mindestens ein Strahlungskollektor 12 zum Auffangen von Sonnenstrahlung 20 vorgesehen und der mindestens eine Strahlungskollektor 12 ist über mindestens ein Faserbündel 14 optisch mit mindestens einem Strahlungsemitter 16 verbunden, wobei die mindestens eine Solarzelle 48 zur Erzeugung von elektrischer Energie durch den mindestens einen Strahlungsemitter 16 mit der von dem mindestens einen Strahlungskollektor 12 aufgefangenen und durch das mindestens eine Faserbündel 14 weitergeleiteten Sonnenstrahlung 20 bestrahlbar ist. Dadurch, dass die Sonnenstrahlung 20 an einem Ort aufgefangen und an einem hiervon verschiedenen Ort in elektrische Energie konvertiert wird, lassen sich aerodynamische sowie strukturmechanische Vorteile erzielen, die unteren anderem eine signifikante Gewichtsreduktion einer mit der Vorrichtung 10 ausgestatteten hochfliegenden Leichtbaustruktur ermöglichen. Darüber hinaus hat die Erfindung eine hochfliegende Leichtbaustruktur 60 zum Gegenstand.

    Abstract translation: 本发明使用至少一个太阳能电池48涉及的装置10用于供应高飞扬轻质结构60，尤其是同温层或Mesosphärenfluggeräts，与电能根据本发明，提供了一种用于收集太阳辐射20和所述至少一个辐射收集器12经由连接的至少一个辐射收集器12 至少一个纤维束14被光学地与至少一个辐射发射器16，其中，由所述至少一个辐射发射器16中的至少一个太阳能电池48，用于电能的产生捕获的和通过所述至少一个纤维束14的太阳辐射转发到的至少一个辐射收集器12的连接20被照射 ， 特征在于，所述太阳辐射20被收集在一个地方，在电力转换为不同从其地方，可以实现空气动力和结构的机械优点，使下外，一个显著轻量化的装备有装置10的高飞行结构轻巧。 此外，本发明具有轻便的高空飞行的结构60的对象。

    공중에 떠 다니는 무인 정보 수집과 송신하는 방법 및 그 시스템
    13.
    发明申请
    공중에 떠 다니는 무인 정보 수집과 송신하는 방법 및 그 시스템 审中-公开
    无人机收集和信息传输的方法和系统

    公开(公告)号：WO2013032078A1

    公开(公告)日：2013-03-07

    申请号：PCT/KR2012/001232

    申请日：2012-02-19

    Applicant: 김준규

    Inventor： 김준규

    IPC: B64C39/02 ,  B64D47/00 ,  B64C29/00

    CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/125 ,  B64C2201/127

    Abstract: 본 발명은 비행을 통해 정보를 수집, 송신하는 방법 및 시스템에 관한 것으로, 공기모음추진체로 무인 비행을 하고, 설정된 경로와 지점으로 공기모음캡과 공기모음케이스로 일정고도에서 최저속도로 하강 이동하며, 센서들로부터 수집된 정보를 지상 정보수집처리체에 송신하여 기록, 저장 및 활용하는 기술에 관한 것이다.

    Abstract translation: 本发明涉及飞行中无人机载体收集和传输信息的方法和系统，以及使用空气收集体执行无人驾驶的技术，其以预定的高度以优化的速度在设定的路线和位置 使用集气罩和空气收集箱，并将收集的信息从传感器发送到地面上的信息收集/处理机构，以记录，存储和利用信息。

    SYSTEMS AND METHODS OF MEASURING AND ANALYSING WEATHER
    14.
    发明申请
    SYSTEMS AND METHODS OF MEASURING AND ANALYSING WEATHER 审中-公开
    测量和分析天气的系统和方法

    公开(公告)号：WO2017199237A1

    公开(公告)日：2017-11-23

    申请号：PCT/IL2017/050530

    申请日：2017-05-14

    Applicant: ISRAEL AEROSPACE INDUSTRIES LTD.

    Inventor： DEKEL, Guy ,  ZIVAN, Lior

    IPC: B64D17/00 ,  G05D1/00 ,  G06F19/00

    CPC classification number: B64D45/00 ,  B64C13/16 ,  B64C31/036 ,  B64C39/024 ,  B64C2201/107 ,  B64C2201/125 ,  B64D17/025 ,  B64D17/34 ,  B64D43/00 ,  G01W1/08 ,  G05D1/105

    Abstract: A system for the measurement of weather comprises a sensor configured to sense data comprising data indicative of the geometrical configuration of a flexible airfoil of an air vehicle, and a controller configured to extract data indicative of the geometrical configuration of the airfoil in operation from the sensed data, and determine characteristics of local weather based at least on said extracted data. A system for the measurement of weather comprises a load sensor mounted on a suspension line attached to a flexible airfoil of an air vehicle, for measuring the load of the suspension line, and a controller configured to determine characteristics of local weather based at least on the load measured on the suspension line of the air vehicle in operation. A weather database comprises information on a correlation between data indicative of the nature of the ground at a plurality of locations and characteristics of the local weather at these locations.

    Abstract translation: 用于天气测量的系统包括配置成感测数据的传感器，所述数据包括指示飞行器的柔性翼型的几何配置的数据，以及控制器，配置成提取指示所述几何配置 从所感测的数据开始操作机翼，并且至少基于所述提取的数据确定本地天气的特性。 用于测量天气的系统包括安装在悬挂线上的负载传感器，悬挂线连接到飞行器的柔性翼型，用于测量悬挂线的负载，以及控制器，配置为至少基于 在运行中的飞行器的悬挂线上测量的载荷。 天气数据库包括关于指示多个位置处的地面性质的数据与这些位置处的当地天气的特性之间的相关性的信息。

    TRAILER FOR AUTONOMOUS VEHICLE
    15.
    发明申请
    TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
    自动车辆拖车

    公开(公告)号：WO2015038697A3

    公开(公告)日：2015-10-29

    申请号：PCT/US2014055075

    申请日：2014-09-11

    Applicant: SILICIS TECHNOLOGIES INC

    Inventor： STIGLER MICHAEL J ,  SETAR NICHOLAS JAMES

    IPC: B64F1/12

    CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    Abstract translation: 所公开的实施例包括用于由命令和控制接口控制的自主车辆的拖车。 拖车包括拖车主体，其构造成将自主车辆保持在未部署的构造中。 拖车还以部署的配置锚定自主车辆。 提供了系绳，其具有联接到拖车主体的第一端和被配置为联接到自主车辆的第二端。 使用绞盘来调节系绳的长度以在未部署的配置和部署配置之间移动自主车辆。 此外，通信系统与命令和控制界面以及自主车辆进行通信，以控制自动车辆在未部署配置和部署配置之间的移动。

    Air pollutants monitoring by a continuous process in real time and at different altitudes
    18.
    发明公开
    Air pollutants monitoring by a continuous process in real time and at different altitudes 审中-公开
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    公开(公告)号：EP2327626A1

    公开(公告)日：2011-06-01

    申请号：EP10192814.1

    申请日：2010-11-26

    Applicant: Universita' Degli Studi di Napoli Parthenope

    Inventor： Lega, Massimiliano ,  Napoli, Rodolfo

    IPC: B64C39/02 ,  G01W1/08

    CPC classification number: B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/125 ,  B64C2201/146 ,  G01W1/08

    Abstract: The present invention relates to a process for continuously monitoring, in real time and at different altitudes, airborne pollutants.
    In particular, by using a multi-rotor flying platform, a fluid dynamic conveyance system, a specific sensor and a remote transmission system for transmitting the collected data, it is possible to monitor the presence, and possibly also the concentration, of airborne pollutants along vertical transepts and/or spatial trajectories. The process is implemented by coupling single elements, appropriately built and integrated, according to a predefined sequence and by imposing a certain operational procedure. In particular, it must be pointed out that:
    - the multi-rotor platform has no humans aboard and is controlled remotely, although it includes an on-board automatic flight stabilization system and a system for stopping the flight in the event of failures and/or malfunctions.
    - the fluid dynamic conveyance system consists of a truncated-cone element arranged in the upper part of the platform and securely anchored thereto; more in detail, the length of this element is such that it allows the monitored air to be taken partly outside the interference field of the rotors, and the flow inlet and outlet areas are so arranged as to allow the air to flow without any hindrance.
    - the airborne pollutant sensor is located in the upper part of the platform, at the base of the fluid dynamic conveyance system, and its sensitive part is immersed in the outgoing flow.
    The platform, assembled with the fluid dynamic conveyance system, a specific sensor and a system for remotely transmitting the collected data, is flown along vertical trajectories where stop points are imposed at different altitudes and repositioning shifts are made by means of translational movements. The vertical transepts are obtained by imposing paths that follow lines orthogonal to the ground plane and with one vertex lying therein.

    Abstract translation: 本发明涉及一种在实时和不同高度连续监测空气污染物的方法。 特别地，通过使用多转子飞行平台，流体动力传递系统，特定传感器和用于传送收集的数据的远程传输系统，可以监测沿着空气传播的污染物的存在和可能的浓度 垂直方向和/或空间轨迹。 该过程通过根据预定义的顺序并且通过施加一定的操作过程来耦合单个元件，适当地构建和集成来实现。 特别地，必须指出的是：多转子平台没有人类并且被远程控制，尽管它包括车载自动飞行稳定系统和在发生故障时停止飞行的系统和/ 或故障。 - 流体动力输送系统由设置在平台上部并牢固锚固的截头圆锥元件组成; 更详细地，该元件的长度使得其允许被监视的空气部分地在转子的干涉场之外，并且流入口和出口区域被布置成允许空气流动而没有任何障碍。 - 空气污染物传感器位于平台的上部，位于流体动力输送系统的底部，其敏感部分浸入流出中。 与流体动力输送系统组装的平台，用于远程传送收集的数据的特定传感器和系统沿着垂直轨迹飞行，在不同高度处施加停止点，并且通过平移运动进行重新定位位移。 通过施加跟随垂直于接地平面的线并且一个顶点位于其中的路径来获得垂直接通。

    ARTIFICIAL INTELLIGENCE-DRIVEN CARBON DIOXIDE SEQUESTRATION IN THE ATMOSPHERE
    19.
    发明公开
    ARTIFICIAL INTELLIGENCE-DRIVEN CARBON DIOXIDE SEQUESTRATION IN THE ATMOSPHERE 审中-公开

    公开(公告)号：US20230375746A1

    公开(公告)日：2023-11-23

    申请号：US17749400

    申请日：2022-05-20

    Applicant: Kyndryl, Inc.

    Inventor： Mauro Marzorati ,  Jeremy R. Fox ,  Sarbajit K. Rakshit ,  Ruben Luengas de la Fuente

    IPC: G01W1/18 ,  G08G5/00 ,  B64C39/02

    CPC classification number: G01W1/18 ,  G08G5/003 ,  B64C39/024 ,  B64C2201/125

    Abstract: Aspects of the present disclosure relate generally to reduction in environmental pollution and, more particularly, to systems and method of carbon dioxide (CO2) sequestration in the atmosphere. For example, a computer-implemented method includes receiving, by a computing device, locations of an atmospheric pollutant; determining, by a computing device, a location of a target area of the atmospheric pollutant for sequestration; determining, by the computing device, positioning and flight path data for airborne sequestration devices to sequester the atmospheric pollutant at the location of the target area of the atmospheric pollutant; and deploying, by the computing device, the airborne sequestration devices with reagent according to the positioning and the flight path data to sequester the atmospheric pollutant at the location of the target area of the atmospheric pollutant.

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