An objective of the present invention is to provide a take-off and landing system for an aircraft that can safely implement take-off and landing of an aircraft excluding vertical propellers. According to the present invention, the take-off and landing system for an aircraft comprises: a base; and a deck configured to be capable of vertical take-off and landing with respect to the base and equipped with a docking device capable of docking and undocking with a landing gear of the aircraft.

    본 발명은 베이스; 상기 베이스에 대해 수직 이착륙 가능하게 구성되고, 비행체의 랜딩기어와 도킹 및 언도킹할 수 있는 도킹장치를 구비한 데크를 포함하여 구성된다.


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    Titel :

    AIRCRAFT TAKE-OFF AND LANDING SYSTEM


    Weitere Titelangaben:

    비행체의 이착륙 시스템


    Beteiligte:
    NAM YONG HYUN (Autor:in) / YIM CHUNG SIK (Autor:in) / CHOI JAE YOUNG (Autor:in) / JUNG SANG HYUN (Autor:in) / HAN SEUNG SIK (Autor:in) / LEE DAE HEE (Autor:in) / LEE JAE SEUNG (Autor:in) / CHO KYU HOON (Autor:in)

    Erscheinungsdatum :

    2022-07-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    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 / F16F SPRINGS , Federn