A load fluctuation detection unit that detects a load fluctuation of an aircraft, and an operating point control unit that controls a power operating point defined by a torque and rotation speed based on a flight state. The operating point control unit sets a target power operating point (62) for coping with a load with respect to an initial power operating point (61) in an operating point map (40) when the load has fluctuated. The operating point control unit moves the power operating point from the initial power operating point (61) on a first operating line (41) to the target power operating point (62) on a second operating line (42), to a return power operating point (63) on the first operating line (41) while keeping a torque T constant, and then to the initial power operating point (61) along the first operating line (41).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft propulsion system


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

    Erscheinungsdatum :

    2024-07-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    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