An air vehicle includes a flight computer, a fuselage, and two rotors mounted symmetrically with respect to the fuselage. Each of the two rotors includes a servo mechanism to tilt a respective rotor of the two rotors about two axes of the respective rotor. The flight computer is configured to send control parameters to each of the two rotors, the control parameters including a rotational speed, a first tilt angle about a first axis of the two axes of the respective rotor, and a second tilt angle about a second axis of the two axes of the respective rotor. A method for operating the air vehicle is also provided.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    System and method of operation of twin-tiltrotor helicopter



    Erscheinungsdatum :

    11.12.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



    SYSTEM AND METHOD OF OPERATION OF TWIN-TILTROTOR HELICOPTER

    ELFEKY MAHMOUD ABDELMAGID / ELSHAFEI MOUSTAFA | Europäisches Patentamt | 2017

    Freier Zugriff

    TWIN FUSELAGE TILTROTOR AIRCRAFT

    IVANS STEVEN R / ROE ROBERT | Europäisches Patentamt | 2023

    Freier Zugriff

    Twin fuselage tiltrotor aircraft

    IVANS STEVEN R / ROE ROBERT | Europäisches Patentamt | 2023

    Freier Zugriff