The method involves providing a rotor (3) with a set of blades (3'), and maintaining aerodynamic angle of incidence of a rotary wing aircraft i.e. helicopter, equal to a reference angle of incidence by automatically operating a collective pitch of the set of blades. The reference angle of incidence is equal to current aerodynamic incidence of the aircraft at the time of commitment of a mode of assisted piloting of the aircraft. Value of the reference angle of incidence is modified. An independent claim is also included for a device for automatic piloting of a rotary wing aircraft.


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    Title :

    PROCEDE DE PILOTAGE AUTOMATIQUE D'UN AERONEF A VOILURE TOURNANTE COMPRENANT AU MOINS UNE HELICE PROPULSIVE, DISPOSITIF DE PILOTAGE AUTOMATIQUE ET AERONEF ASSOCIES


    Additional title:

    Method for automatic piloting of a rotary wing aircraft comprising at least one thruster propeller, associated automatic piloting device and aircraft
    Selbststeuerungsverfahren eines Drehflügelflugzeugs, das mindestens einen Druckpropeller umfasst, entsprechende Autopilot und Flugzeug


    Contributors:
    EGLIN PAUL (author)

    Publication date :

    2017-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT







    DISPOSITIF DE PILOTAGE AUTOMATIQUE D'UN AERONEF A VOILURE TOURNANTE ET AERONEF A VOILURE TOURNANTE COMPRENANT UN TEL DISPOSITIF

    COLONNA FRANCOIS / THOUVENOT GILLES / AUGER ALAIN | European Patent Office | 2019

    Free access