A landing facility that enables flight vehicles to land safely even in strong winds. The landing system of the invention includes a first area for landing a flight vehicle, a windbreak part having a predetermined height and cover part at least a portion of the perimeter of the first area, and a second area located away from the windbreak part, where the flight vehicle descends to a predetermined flight altitude. The flight altitude is lower than the predetermined height of the windbreak part. The second area is an area selected from a plurality of permitted areas where vertical descent is permitted. A portion of the windbreak part comprises a net.


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    Titel :

    Landing facility, landing method


    Beteiligte:
    SUZUKI YOICHI (Autor:in)

    Erscheinungsdatum :

    28.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64U



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