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    ENSEMBLE POUR AÉRONEF COMPORTANT UN CHÂSSIS ET UN MODULE DE VISION D'UN SYSTÈME DE VISION EN VOL AMÉLIORÉE
    3.
    发明公开
    ENSEMBLE POUR AÉRONEF COMPORTANT UN CHÂSSIS ET UN MODULE DE VISION D'UN SYSTÈME DE VISION EN VOL AMÉLIORÉE 审中-公开

    公开(公告)号：EP4310008A1

    公开(公告)日：2024-01-24

    申请号：EP23185012.4

    申请日：2023-07-12

    申请人： AIRBUS OPERATIONS

    发明人： BERTRAND, Sébastien

    IPC分类号： B64D47/00

    摘要： L'invention concerne un ensemble (200) pour aéronef comportant un module de vision (152) avec une base (156) et un châssis (160) comportant une première poutre (162) fixée à la base (156) par quatre moyens de fixation (50a), une deuxième poutre (164) fixée à la première poutre (162) par quatre moyens de fixation (50b), et deux troisièmes poutres (166a-b) fixées à la structure (168) de l'aéronef et entre lesquelles la deuxième poutre (164) est fixée par deux troisièmes moyens de fixation (50c), où chaque moyen de fixation (50a-c) prend la forme d'un système à deux bagues excentriques mobiles en rotation l'une par rapport à l'autre autour d'axes de rotation parallèles.
    Avec un tel arrangement, les moyens de fixation permettent le réglage du châssis, le transfert des charges selon toutes les directions, et le verrouillage des positions.

    CONTROL DEVICE, PROGRAM, SYSTEM, AND CONTROL METHOD
    4.
    发明公开
    CONTROL DEVICE, PROGRAM, SYSTEM, AND CONTROL METHOD 审中-公开

    公开(公告)号：EP4279381A1

    公开(公告)日：2023-11-22

    申请号：EP21919749.8

    申请日：2021-12-27

    申请人： HAPSMobile Inc.

    发明人： NAKAZAWA Eiji

    IPC分类号： B64C39/02 ,  B64D47/00 ,  H04W16/18 ,  H04W16/26 ,  H04W16/28 ,  H04W24/04 ,  H04W76/10

    摘要： Provided is a control device including: a flight vehicle position information acquisition unit which acquires service flight vehicle position information indicating positions of a plurality of service flight vehicles, each of which functions as a stratosphere platform and is mounted with a communication device which forms a wireless communication area by emitting a beam and provides a wireless communication service to a user terminal in the wireless communication area; an arrangement determination unit which determines arrangement of a relay flight vehicle which relays communication of one service flight vehicle among the plurality of service flight vehicles on a basis of a predetermined condition and the service flight vehicle position information; and a flight vehicle control unit which controls the relay flight vehicle to move according to the arrangement determined by the arrangement determination unit and establish wireless communication connection with the one service flight vehicle.

    MECHANISMS FOR LOWERING A PAYLOAD TO THE GROUND FROM A UAV
    6.
    发明公开
    MECHANISMS FOR LOWERING A PAYLOAD TO THE GROUND FROM A UAV 审中-公开

    公开(公告)号：EP4134305A1

    公开(公告)日：2023-02-15

    申请号：EP22190713.2

    申请日：2014-08-25

    申请人： Wing Aviation LLC

    发明人： Patrick, William Graham ,  Burgess, James Ryan ,  Andrew, Conrad

    IPC分类号： B64C39/02 ,  B64D1/02 ,  B64D47/00 ,  B64D1/12 ,  B64D1/22

    摘要： Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housing, a payload, a line-deployment mechanism coupled to the housing and a line, and a payload-release mechanism that couples the line to the payload, wherein the payload-release mechanism is configured to release the payload from the line. The UAV may further include a control system configured to determine that the UAV is located at or near a delivery location and responsively: operate the line-deployment mechanism according to a variable deployment-rate profile to lower the payload to or near to the ground, determine that the payload is touching or is within a threshold distance from the ground, and responsively operate the payload-release mechanism to release the payload from the line.