We disclose a method of operating an aircraft with multiple actuators, such as propulsion units, preferably electrically powered propulsion units, comprising:i) monitoring an operational state of said multiple actuators;ii) when detecting a malfunctioning or failure of any one of said actuators, indicating said malfunctioning or failure to a pilot in command (2b) of the aircraft;iii) controlling a human machine interface (2ab) of the aircraft to display and enable a limited choice of possible operating measures in connection with said malfunctioning or failure to the pilot in command (2b); andiv) programming at least one control element (2ae) in association with said one actuator to perform said measures when actuated by the pilot in command (2b).
AIRCRAFT OPERATING METHOD, AIRCRAFT CONTROL PANEL ARCHITECTURE, AND AIRCRAFT
FLUGZEUGBETRIEBSVERFAHREN, FLUGZEUGSTEUERPANEELARCHITEKTUR UND FLUGZEUG
PROCÉDÉ DE FONCTIONNEMENT D'AÉRONEF, ARCHITECTURE DE PANNEAU DE COMMANDE D'AÉRONEF ET AÉRONEF
2024-03-06
Patent
Electronic Resource
English
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