POSITIONING SYSTEM AND STATION ADAPTED TO RECEIVE AND STORE AN UNMANNED AERIAL VEHICLE

    公开(公告)号:EP4438499A1

    公开(公告)日:2024-10-02

    申请号:EP23166064.8

    申请日:2023-03-31

    摘要: The invention pertains to the field of unmanned aircrafts, and more specifically to elements that enable storage, positioning and charging aircrafts upon their landing on the station. The invention discloses a positioning system comprising: a landing platform (1) and a charging arrangement (3). The system is characterized in that it comprises a positioning arrangement (2) capable to position an unmanned aircraft at a dedicated site on the landing platform (1). Positioning arrangement (2) comprises at least three beams (4) to enable positioning of the unmanned aircraft at a dedicated site on the landing platform (1), and guiding mechanisms capable to move the beams (4), where the charging arrangement (3) is attached to one beam (4) and has a connector (6) capable to be connected to the unmanned aircraft, preferably by means of a mechanic-electric connection. The invention also provides a station arranged for receiving and storage of an unmanned aircraft and comprising a positioning system.

    CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE
    4.
    发明公开

    公开(公告)号:EP4442573A1

    公开(公告)日:2024-10-09

    申请号:EP22901030.1

    申请日:2022-11-07

    申请人: DENSO CORPORATION

    IPC分类号: B64D27/24 B64C27/26 B64C39/02

    摘要: A flight control device performs flight control processing for causing an eVTOL to fly. The flight control device determines whether the eVTOL is on the ground in step S101 of the flight control processing. When the eVTOL is on the ground, the flight control device (40) acquires a temperature of a drive battery as a battery temperature (Tbt) in step S102. In step S103, the flight control device (40) determines whether the battery temperature (Tbt) is lower than a take-off permitting temperature (TA). When the battery temperature (Tbt) is lower than the take-off permitting temperature (TA), the flight control device (40) proceeds to step S104 to prohibit take-off of the eVTOL. Thereafter, the flight control device (40) performs the temperature raising control in step S105. In the temperature raising control, the temperature of the drive battery (31) is raised.