In a power supply system of an aircraft, when electric power is supplied from a power generation unit to a drive unit, the electric power is supplied from the power generation unit to the drive unit via a first power transmission path, and a voltage is applied to a second power transmission path by a fault detection circuit in a state in which the power generation unit and the drive unit are disconnected from the second power transmission path, and when the power generation unit is started, electric power of the fault detection circuit is supplied to the power generation unit in a state in which the power generation unit is connected to the second power transmission path.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    POWER SUPPLY SYSTEM OF AIRCRAFT


    Beteiligte:
    MITANI MANABU (Autor:in) / YOSHIDA MASATAKA (Autor:in)

    Erscheinungsdatum :

    31.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT POWER SUPPLY SYSTEM

    ZLEDENNYJ NIKOLAJ PAVLOVICH / FEDJAEV VIKTOR NIKOLAEVICH / PLIPLIN ANDREJ ALEKSANDROVICH et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT POWER SUPPLY SYSTEM

    ISMAGILOV FLYUR RASHITOVICH / VAVILOV VYACHESLAV EVGENEVICH / BEKUZIN VLADIMIR IGOREVICH et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft power supply system and associated aircraft

    AUROY ALEXANDRE / BARRACO THOMAS / SIGRIST ZOÉ | Europäisches Patentamt | 2025

    Freier Zugriff

    Electric power supply system for an aircraft, aircraft and airport power supply system

    BROMBACH JOHANNES / SCHULZ DETLEF | Europäisches Patentamt | 2016

    Freier Zugriff

    POWER SUPPLY SYSTEM OF AIRCRAFT

    MITANI MANABU / YOSHIDA MASATAKA | Europäisches Patentamt | 2023

    Freier Zugriff