An air intake unit for an engine of an aircraft; the intake unit has: a tubular housing; a first inlet opening which is obtained through an outer wall of the tubular housing and through which external air can be taken in; an air filter which engages the first inlet opening; a second inlet opening which is obtained through the outer wall of the tubular housing and through which external air can be taken in; a shutter device which is coupled to the second inlet opening and is movable between a closed position, in which it closes the second inlet opening, and an open position, in which it sets the passage through the second inlet opening free; and an actuator, which moves the shutter device.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE


    Weitere Titelangaben:

    LUFTEINLASSEINHEIT FÜR EINE FLUGZEUGMASCHINE
    UNITÉ D'ENTRÉE D'AIR POUR MOTEUR D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    24.03.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Air intake unit for an aircraft engine

    BERGAMI GAETANO | Europäisches Patentamt | 2022

    Freier Zugriff

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE

    BERGAMI GAETANO | Europäisches Patentamt | 2021

    Freier Zugriff

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE

    BERGAMI GAETANO | Europäisches Patentamt | 2018

    Freier Zugriff

    AIR INTAKE UNIT FOR AN ENGINE OF AN AIRCRAFT

    BERGAMI GAETANO | Europäisches Patentamt | 2019

    Freier Zugriff

    INTAKE FOR ENGINE OF AIRCRAFT

    JUDAS MICHAEL / BICHLER BARHOLOMAUS | Europäisches Patentamt | 2018

    Freier Zugriff