An aircraft propulsion system capable of improving the restartability of an engine is provided. An aircraft propulsion system includes: a plurality of engines (60-1 and 60-2); an electric generator connected to engine shafts (63-1 and 63-2); a plurality of electric motors; a plurality of rotors; and a controller (100) which controls an operation state of the plurality of engines (60-1 and 60-2). The controller (100) causes a part of the plurality of engines (60-1 and 60-2) to operate while stopping the remaining engine when a flight state is in a first state. The plurality of engines (60-1 and 60-2) include circulators (65-1 and 65-2). A plurality of communication pipes (68 and 69) which communicate the circulator (65-1) in the first engine (60-1) among the plurality of engines (60-1 and 60-2) with the circulator (65-2) in the second engine (60-2) are provided.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft propulsion system


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

    Erscheinungsdatum :

    2023-09-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft propulsion system

    MATSUMOTO TAKESHI / KITA AKINORI | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    ERYILMAZ IBRAHIM | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    FAMULARO DOUGLAS / TURALBA JOSE ANTONIO | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    LI HONGLIANG / KANG YUANLI / HUI YANNIAN | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    HARWOOD RICHARD / MENON KALYANI G / PALMER JOSEPH et al. | Europäisches Patentamt | 2021

    Freier Zugriff