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.
PROCEDE DE PILOTAGE AUTOMATIQUE D'UN AERONEF A VOILURE TOURNANTE COMPRENANT AU MOINS UNE HELICE PROPULSIVE, DISPOSITIF DE PILOTAGE AUTOMATIQUE ET AERONEF ASSOCIES
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
2017-11-08
Patent
Elektronische Ressource
Französisch
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