A propulsor (101) for an aircraft is shown. The propulsor comprises a propulsive fan (106), and an electric machine (108) configured to drive the propulsive fan. The electric machine has a casing containing electrical and electromechanical components, a shaft which extends outside of the casing and which is connected to the propulsive fan, and a seal to seal the casing around the shaft. A pressurisation system pressurises the casing above an external pressure to prevent electrical breakdown within gas in the casing of the electric machine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PREVENTING ELECTRICAL BREAKDOWN


    Beteiligte:
    RAZAK AHMED MY (Autor:in) / CHONG ELLIS FH (Autor:in)

    Erscheinungsdatum :

    29.11.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    PREVENTING ELECTRICAL BREAKDOWN

    RAZAK AHMED MY | Europäisches Patentamt | 2018

    Freier Zugriff

    PREVENTING ELECTRICAL BREAKDOWN

    RAZAK AHMED / CHONG ELLIS | Europäisches Patentamt | 2018

    Freier Zugriff

    Preventing electrical breakdown

    RAZAK AHMED MY | Europäisches Patentamt | 2023

    Freier Zugriff

    Preventing electrical breakdown

    RAZAK AHMED M Y | Europäisches Patentamt | 2022

    Freier Zugriff

    PREVENTING ELECTRICAL BREAKDOWN

    RAZAK AHMED | Europäisches Patentamt | 2020

    Freier Zugriff