An aircraft (100) includes a gas turbine engine (108), an electric motor (110), and a propulsion device (112). The gas turbine engine (108) and the electric motor (110) are configured to provide a target cumulative output to the propulsion device (112). An electronic control unit (106) is configured to set the gas turbine engine (108) to a first engine mode to provide a first engine output to the propulsion device (112), set the electric motor (110) to a first motor mode to provide a first motor output to the propulsion device (112), a sum of the first engine output and the first motor output being within a predetermined range of the target cumulative output, and in response to a speed of the aircraft (100) reaching a target speed and the first engine output increasing to a second engine output, set the electric motor (110) to a second motor mode.
AIRCRAFTS, SYSTEMS, AND METHODS FOR PROVIDING CONSTANT TORQUE ON TAKEOFF
FLUGZEUGE, SYSTEME UND VERFAHREN ZUR BEREITSTELLUNG EINES KONSTANTEN DREHMOMENTS BEIM START
AÉRONEFS, SYSTÈMES ET PROCÉDÉS POUR FOURNIR UN COUPLE CONSTANT AU DÉCOLLAGE
28.02.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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