Systems and methods include providing an aircraft with a vertical stabilizer system having a vertical stabilizer operatively coupled to a tail boom, tail rotor gearbox, or other component of the aircraft at a forward attachment and an aft attachment. The vertical stabilizer is selectively rotatable to adjust an angle of attack of the vertical stabilizer with respect to a forward flight direction of the aircraft. The vertical stabilizer is rotatable between a forward flight position having a substantially small degree angle of attack and a hover or lateral movement position having a substantially ninety degree angle of attack.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vertical stabilizer


    Beteiligte:

    Erscheinungsdatum :

    2021-06-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    VERTICAL STABILIZER

    DUVAL SEBASTIEN / NOISEUX-BOUCHER GUILLAUME / ACEE AARON ALEXANDER | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT VERTICAL STABILIZER DESIGN

    LANIGAN BRENDAN P / O'NEIL JOSHUA R | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT VERTICAL STABILIZER DESIGN

    LANIGAN BRENDAN P / O'NEIL JOSHUA R | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft vertical stabilizer design

    LANIGAN BRENDAN P / O'NEIL JOSHUA R | Europäisches Patentamt | 2020

    Freier Zugriff

    Vertical stabilizer for ejection systems

    NICHOLAS KERSI CHARLES BHARUCHA / STEVEN HOLSTINE / CASEY ANDREW STRIBRNY | Europäisches Patentamt | 2024

    Freier Zugriff