An air intake unit (3) for an engine of an aircraft (1); the intake unit (3) has: a tubular housing (4); a first inlet opening (7) which is obtained through an outer wall (6) of the tubular housing (4) and through which external air can be taken in; an air filter (8) which engages the first inlet opening (7); a second inlet opening (9) which is obtained through the outer wall (6) of the tubular housing (4) and through which external air can be taken in; a shutter device (10) which is coupled to the second inlet opening (9) and is movable between a closed position, in which it closes the second inlet opening (9), and an open position, in which it sets the passage through the second inlet opening (9) free; and an actuator (11), which moves the shutter device (10).


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    Titel :

    AIR INTAKE UNIT FOR AN ENGINE OF AN AIRCRAFT


    Weitere Titelangaben:

    LUFTEINLASSEINHEIT FÜR EINEN MOTOR EINES FLUGZEUGES
    UNITÉ D'ADMISSION D'AIR POUR UN MOTEUR D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    11.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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