An aircraft propulsion system capable of improving power generation efficiency is provided. When a flight state of an aircraft (10) is a first state after a plurality of engines (60-1, 60-2) operate and the aircraft takes off, the aircraft propulsion system causes at least one engine among the plurality of engines (60-1, 60-2) 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 :

    MULTICOPTER WITH PROPULSION SYSTEM


    Weitere Titelangaben:

    MULTIKOPTER MIT ANTRIEBSSYSTEM
    MULTICOPTÈRE AVEC SYSTÈME DE PROPULSION


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

    Erscheinungsdatum :

    2023-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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