An aircraft propulsion unit comprising a motor, a system for supplying fuel to the motor, a fairing inside which the motor and at least part of the fuel supplying system are positioned, and at least one pressure relief device configured to establish communication between the inner and outer zones of the fairing when the pressure in the inner zone is greater than or equal to a given threshold or when a leak is detected. Also an aircraft comprising at least one such propulsion unit.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT PROPULSION UNIT COMPRISING AT LEAST ONE PRESSURE RELIEF DEVICE AND AIRCRAFT HAVING AT LEAST ONE SUCH PROPULSION UNIT


    Beteiligte:
    CZAPLA LIONEL (Autor:in) / PISSAVIN ALEXIS (Autor:in)

    Erscheinungsdatum :

    22.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit

    CZAPRA LIONEL / PISAVIN ALEXEY | Europäisches Patentamt | 2024

    Freier Zugriff

    ELECTRIC PROPULSION UNIT COMPRISING AT LEAST TWO INDEPENDENT SUPPORTS, AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT

    FUKASAKU KOTARO / AMARGIER RÉMI / CZAPLA LIONEL et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft propulsion assembly and aircraft comprising at least one such propulsion assembly

    REYNAUD ERIC / DEFORET THOMAS / KALETTA MICHAEL et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Propulsion device and aircraft comprising at least one such propulsion device

    BERJOT MICHAEL / LANCIAUX R ¨ / MI et al. | Europäisches Patentamt | 2025

    Freier Zugriff