The aircraft has a pivoting motor for swinging a moving part carrying a rear rotor (10) from a fixed position (POS1) to another position in a reversible manner so that the aircraft passes from an operating mode to another operating mode during which propulsion of the aircraft is assured by the rear rotor. An inclination unit inclines a mast in an anteroposterior longitudinal plane toward a rear end (4'') of the aircraft in a reversible manner so that the aircraft passes from the latter mode toward a third operating mode during which propulsion of the aircraft is assured only by the rear rotor. An independent claim is also included for a method for piloting an aircraft.


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    Title :

    Aéronef muni d'un rotor arrière basculant, et procédé associé


    Additional title:

    Aircraft provided with a tilting rear rotor and associated method
    Luftfahrzeug, das mit einem rückseitigen Kipprotor ausgestattet ist, und entsprechendes Verfahren


    Contributors:

    Publication date :

    2016-03-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge





    MANCHON DE PALE DE ROTOR D'UN AERONEF MUNI D'UNE PROTUBERANCE EN ZONE ARRIERE ET ROTOR MUNI D'UN TEL MANCHON

    DESVIGNE DAMIEN / ALFANO DAVID | European Patent Office | 2018

    Free access