The present invention discloses a high-speed take-off and landing anti-falling airplane. The airplane includes an fuselage, wing mechanisms are provided on the fuselage, each wing mechanism includes a main wing, an invisible wing, a slow descent wing, a layer wing, an empennage, a slow descent wing adjusting mechanism, an invisible wing adjusting mechanism and a layer wing adjusting mechanism, the layer wings are provided on the upper side and the lower side of each main wing respectively, and the layer wing adjusting mechanisms are provided on the inner sides of the layer wings; the front end of the layer wing adjusting mechanism is fixedly connected with the inner side of the layer wing; according to the high-speed take-off and landing anti-falling airplane, the take-off speed and safety are improved, and fuel consumption is reduced.


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    Titel :

    HIGH-SPEED TAKE-OFF AND LANDING ANTI-FALLING AIRPLANE


    Beteiligte:
    MU ZHICHANG (Autor:in)

    Erscheinungsdatum :

    2021-06-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



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