Embodiments are directed to a rotorcraft comprising a body having a longitudinal axis, a wing coupled to the body, a single tiltrotor assembly pivotally coupled to the body, and the tiltrotor assembly configured to move between a position generally perpendicular to the longitudinal axis during a vertical flight mode and a position generally parallel to the longitudinal axis during a horizontal flight mode. The rotorcraft may further comprise an anti-torque system configured to counteract torque generated by the tiltrotor assembly during vertical flight. The rotorcraft may further comprise a center of gravity compensation system configured to manage a rotorcraft center of gravity during movement of the tiltrotor assembly between the vertical flight mode and the horizontal flight mode.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Centerline tiltrotor


    Beteiligte:

    Erscheinungsdatum :

    2022-01-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Centerline Tiltrotor

    STANNEY KEITH ALAN / IVANS STEVEN RAY / ROSS BRENT CHADWICK et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    TILTROTOR AIRCRAFT WITH CENTERLINE AND WING MOUNTED ENGINES

    KAREM ABRAHAM / PARCELL JOHN | Europäisches Patentamt | 2023

    Freier Zugriff

    TILTROTOR AIRCRAFT WITH CENTERLINE AND WING MOUNTED ENGINES

    KAREM ABRAHAM / PARCELL JOHN PAUL | Europäisches Patentamt | 2023

    Freier Zugriff

    Articulated tiltrotor

    IVANS STEVEN R / BENFIELD BERLIN B / ROSS BRENT C | Europäisches Patentamt | 2023

    Freier Zugriff

    Tiltrotor control

    ACHTTIEN BRENT RANDAL / TZENG CHYAU J | Europäisches Patentamt | 2022

    Freier Zugriff