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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS


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

    Erscheinungsdatum :

    24.12.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS

    Europäisches Patentamt | 2021

    Freier Zugriff

    FORWARD SWEPT WING VTOL AIRCRAFT WITH EMBEDDED LIFT PROPULSORS

    WINSTON NEIL CLARK / WINSTON ROBERT ALLEN / FULLER CLARK WILLIAM et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Trimaran having outriggers with propulsors

    GEORGE RONALD | Europäisches Patentamt | 2015

    Freier Zugriff

    TRIMARAN HAVING OUTRIGGERS WITH PROPULSORS

    GEORGE RONALD A / ABORDO ADRIAN M | Europäisches Patentamt | 2015

    Freier Zugriff

    PROPULSORS

    JULLIAND LIONEL / GRALL THEO / BAERD HENRI et al. | Europäisches Patentamt | 2024

    Freier Zugriff