An aircraft propulsion system capable of improving power generation efficiency is provided. When a flight state of an aircraft is a first state after a plurality of engines operate and the aircraft takes off, the aircraft propulsion system causes at least one engine among the plurality of engines to be stopped, causes another engine, which has not been stopped, to be operated in an operating range in which the other engine is able to operate efficiently, and causes a generator corresponding to the other engine to output power.


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    Titel :

    AIRCRAFT PROPULSION SYSTEM


    Beteiligte:
    KITA AKINORI (Autor:in) / MATSUMOTO TAKESHI (Autor:in) / TSUTSUMI DAIKO (Autor:in)

    Erscheinungsdatum :

    2022-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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