A vertical/horizontal flight fixed-nozzle fixed wing aircraft is characterized in that a nozzle backward blows gas from the leading edge of the upper aerofoil of a pinion to realize pinion lift augmentation, and the ejector action increasing gas flow downwash of gas flow is deflected through the lower aerofoil of a proximal limb and then flows toward the ground to make the proximal limb lift augmentation of the pneumatic layout, so the fluid supercharging ratio is small, the flow is large, and fuel oil is saved.


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    Titel :

    Vertical/horizontal flight fixed-nozzle fixed wing aircraft


    Beteiligte:
    REN JUN (Autor:in)

    Erscheinungsdatum :

    2016-02-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge