A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS The present invention relates to an airplane capable of hyper-short / vertical takeoff and landing (hyper-STOL / VTOL) and having a positive tilt angle applied to the 5 horizontal propulsors (104A, 104B). A positive tilt angle may also be applied to the vertical propulsors (106A, 106B, 106A1, 106A2, 106B1, 106B2). This invention attempts to reduce pitch angle during hovering and vertical flight. Most Illustrative Diagram: FIG. 3


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    Title :

    A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS


    Contributors:

    Publication date :

    2020-12-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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