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).


    Access

    Download


    Export, share and cite



    Title :

    AIR INTAKE UNIT FOR AN ENGINE OF AN AIRCRAFT


    Additional title:

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


    Contributors:

    Publication date :

    2019-09-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Air intake unit for an aircraft engine

    BERGAMI GAETANO | European Patent Office | 2022

    Free access

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE

    BERGAMI GAETANO | European Patent Office | 2021

    Free access

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE

    BERGAMI GAETANO | European Patent Office | 2021

    Free access

    AIR INTAKE UNIT FOR AN AIRCRAFT ENGINE

    BERGAMI GAETANO | European Patent Office | 2018

    Free access

    INTAKE FOR ENGINE OF AIRCRAFT

    JUDAS MICHAEL / BICHLER BARHOLOMAUS | European Patent Office | 2018

    Free access