An assembly is provided for an aircraft propulsion system (20). This assembly includes a nacelle inner structure (42) that extends axially along and circumferentially about an axial centerline (30). The nacelle inner structure (42) includes an internal compartment (68) and a cowl (76). The internal compartment (68) is configured to house a core of a gas turbine engine (22). The cowl (76) is configured to form an outer radial periphery of the internal compartment (68). An aft end portion (80) of the cowl (76) is also configured to form an outer radial periphery of a compartment exhaust (70) to the internal compartment (68). The aft end portion (80) of the cowl (76) includes a plurality of axial fingers (84) arranged circumferentially about the axial centerline (30) in an array.


    Access

    Download


    Export, share and cite



    Title :

    PASSIVE INTERNAL COMPARTMENT EXHAUST FOR AN AIRCRAFT PROPULSION SYSTEM


    Additional title:

    PASSIVE INNENRAUMABSAUGUNG FÜR EIN FLUGZEUGANTRIEBSSYSTEM
    ÉCHAPPEMENT DE COMPARTIMENT INTERNE PASSIF POUR SYSTÈME DE PROPULSION D'AÉRONEF


    Contributors:

    Publication date :

    2022-11-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Passive internal compartment exhaust for an aircraft propulsion system

    SHERMAN BRIAN A | European Patent Office | 2023

    Free access

    PASSIVE INTERNAL COMPARTMENT EXHAUST FOR AN AIRCRAFT PROPULSION SYSTEM

    SHERMAN BRIAN A | European Patent Office | 2021

    Free access



    THRUST VECTORING EXHAUST NOZZLE FOR AIRCRAFT PROPULSION SYSTEM

    HANRAHAN PAUL R / BOCHAR ROXANNE M | European Patent Office | 2023

    Free access