An aircraft propulsion system capable of reducing a rotational load of an engine shaft is provided. An aircraft propulsion system includes a plurality of engines (60-1 and 60-2) and a controller (100). When a flight state is a first state, the controller (100) causes some of the plurality of engines (60-1 and 60-2) to operate while stopping the remaining engine. At least one engine (60-1) of the plurality of engines (60-1 and 60-2) includes a bleed air hole (71-1), a bleed air pipe (72-1), and a bleed air valve (73-1). When causing the engine (60-2) which has stopped to start up again, the controller (100) opens a bleed air valve (73-1) in the engine (60-1) which is in operation and supplies compressed air of the compressor (62-1) to the compression chamber (64-2) of the engine (60-2) which has stopped.


    Zugriff

    Download


    Exportieren, teilen und zitieren



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



    AIRCRAFT PROPULSION SYSTEM

    ERYILMAZ IBRAHIM | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft propulsion system

    HARWOOD RICHARD / MENON KALYANI G / PALMER JOSEPH et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft propulsion system

    SONNETTE PIERRE-JULIEN / RENOTTE ALEXIS / LINCK BENOIT | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    TASKER RICHARD V / RIX ANDREW I J | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM

    OTA AKIRA | Europäisches Patentamt | 2022

    Freier Zugriff