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.

    本发明涉及一种能够超短距/垂直起飞和着陆(hyper‑STOL/VTOL)并且具有向水平推进器(104A,104B)施加的正倾角的飞机。正倾角也可以施加到垂直推进器(106A、106B、106A1、106A2、106B1、106B2)。本发明试图减小悬停和垂直飞行期间的俯仰角。


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    Titel :

    Airplane capable of hyper-short / vertical takeoff and landing


    Weitere Titelangaben:

    具有倾斜推进器的垂直起飞和着陆能力飞机


    Beteiligte:
    POH CHUNG-KIAK (Autor:in) / POH CHUNG-HOW (Autor:in)

    Erscheinungsdatum :

    2021-09-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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