An aircraft includes an airframe having an aircraft longitudinal axis and a main rotor system supported by the airframe. The main rotor system is rotatable about an axis of rotation. The airframe is tiltable relative to a ground surface to form a non-zero tilt angle between the aircraft longitudinal axis and the ground surface.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ENHANCED TAXI CONTROL FOR RIGID ROTORS


    Weitere Titelangaben:

    VERBESSERTE ROLLSTEUERUNG FÜR STARRE ROTOREN
    COMMANDE DE ROULAGE TAXI AMÉLIORÉE POUR DES ROTORS RIGIDES


    Beteiligte:

    Erscheinungsdatum :

    10.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ENHANCED TAXI CONTROL FOR RIGID ROTORS

    LAPPOS NICHOLAS D / THORNBERG CHRISTOPHER A | Europäisches Patentamt | 2019

    Freier Zugriff

    Enhanced taxi control for rigid rotors

    LAPPOS NICHOLAS D / THORNBERG CHRISTOPHER A | Europäisches Patentamt | 2020

    Freier Zugriff

    Simulations of Ducted and Coaxial Rotors for Air Taxi Operations

    Ventura Diaz, Patricia / Caracuel Rubio, Rafael / Yoon, Seokkwan | AIAA | 2019



    Control issues for rigid-in-plane helicopter rotors

    Latz, Amnon / Graham, Kenneth | AIAA | 1996