The present invention relates to an automatic landing system for a rotorcraft. More particularly, the present invention relates to an automatic landing system for a rotorcraft, capable of stably landing an aircraft using a tension control device when the aircraft including the rotorcraft lands on a ship. According to the present invention, the automatic landing system for a rotorcraft comprises: the aircraft; a plurality of wires provided on the aircraft, and one end of which is discharged toward the ground, and pulls the aircraft to the ground; and a tension adjusting device installed on the ground, and connected to one end of the wire as the one end of the wire is discharged toward the ground so as to adjust the tension of the wire.

    본 발명은 회전익 항공기 자동착륙 시스템에 관한 것으로, 더욱 자세하게는 회전익 항공기를 포함하는 비행체가 함정에 착륙할 때 장력조절장치를 이용하여 비행체를 안정적으로 착륙할 수 있는 회전익 항공기 자동착륙 시스템에 관한 것이다.


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    Titel :

    Rotary-wing Aircraft Automatic Landing System


    Weitere Titelangaben:

    회전익 항공기 자동착륙 시스템


    Beteiligte:
    YANG SOONYONG (Autor:in) / YANG CHANG DEOK (Autor:in)

    Erscheinungsdatum :

    04.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 / B66D Haspeln , CAPSTANS



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